US20180117981A1 - Vehicle Capable of Multiple Varieties of Locomotion - Google Patents
Vehicle Capable of Multiple Varieties of Locomotion Download PDFInfo
- Publication number
- US20180117981A1 US20180117981A1 US15/794,931 US201715794931A US2018117981A1 US 20180117981 A1 US20180117981 A1 US 20180117981A1 US 201715794931 A US201715794931 A US 201715794931A US 2018117981 A1 US2018117981 A1 US 2018117981A1
- Authority
- US
- United States
- Prior art keywords
- vehicle
- tracks
- ground
- blades
- track
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 230000033001 locomotion Effects 0.000 title claims abstract description 27
- 230000007246 mechanism Effects 0.000 claims description 15
- 230000005484 gravity Effects 0.000 claims description 12
- 238000013507 mapping Methods 0.000 claims description 12
- 238000013461 design Methods 0.000 claims description 7
- 230000000007 visual effect Effects 0.000 claims description 7
- 238000001514 detection method Methods 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 6
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 6
- 230000001141 propulsive effect Effects 0.000 claims description 4
- 239000002131 composite material Substances 0.000 claims description 2
- 238000012937 correction Methods 0.000 claims description 2
- 230000007613 environmental effect Effects 0.000 claims description 2
- 238000005286 illumination Methods 0.000 claims description 2
- 238000012800 visualization Methods 0.000 claims description 2
- 230000009466 transformation Effects 0.000 claims 1
- 238000000034 method Methods 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 239000000725 suspension Substances 0.000 description 3
- 235000009508 confectionery Nutrition 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000001953 sensory effect Effects 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 240000005561 Musa balbisiana Species 0.000 description 1
- 235000018290 Musa x paradisiaca Nutrition 0.000 description 1
- 230000003466 anti-cipated effect Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005672 electromagnetic field Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- PWPJGUXAGUPAHP-UHFFFAOYSA-N lufenuron Chemical compound C1=C(Cl)C(OC(F)(F)C(C(F)(F)F)F)=CC(Cl)=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F PWPJGUXAGUPAHP-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000003032 molecular docking Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 235000013550 pizza Nutrition 0.000 description 1
- 150000003071 polychlorinated biphenyls Chemical class 0.000 description 1
- 238000005381 potential energy Methods 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F3/00—Amphibious vehicles, i.e. vehicles capable of travelling both on land and on water; Land vehicles capable of travelling under water
- B60F3/0007—Arrangement of propulsion or steering means on amphibious vehicles
- B60F3/0015—Arrangement of propulsion or steering means on amphibious vehicles comprising tracks specially adapted therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F3/00—Amphibious vehicles, i.e. vehicles capable of travelling both on land and on water; Land vehicles capable of travelling under water
- B60F3/003—Parts or details of the vehicle structure; vehicle arrangements not otherwise provided for
- B60F3/0038—Flotation, updrift or stability devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F3/00—Amphibious vehicles, i.e. vehicles capable of travelling both on land and on water; Land vehicles capable of travelling under water
- B60F3/0061—Amphibious vehicles specially adapted for particular purposes or of a particular type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/003—Off the road or amphibian vehicles adaptable for air or space transport
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D55/00—Endless track vehicles
- B62D55/02—Endless track vehicles with tracks and additional ground wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D55/00—Endless track vehicles
- B62D55/08—Endless track units; Parts thereof
- B62D55/12—Arrangement, location, or adaptation of driving sprockets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D55/00—Endless track vehicles
- B62D55/08—Endless track units; Parts thereof
- B62D55/30—Track-tensioning means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D57/00—Vehicles characterised by having other propulsion or other ground- engaging means than wheels or endless track, alone or in addition to wheels or endless track
- B62D57/04—Vehicles characterised by having other propulsion or other ground- engaging means than wheels or endless track, alone or in addition to wheels or endless track having other than ground-engaging propulsion means, e.g. having propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/38—Alighting gear characterised by elements which contact the ground or similar surface endless-track type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/007—Helicopter portable landing pads
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/70—Convertible aircraft, e.g. convertible into land vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/30—Supply or distribution of electrical power
- B64U50/31—Supply or distribution of electrical power generated by photovoltaics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
- B64U60/50—Undercarriages with landing legs
- B64U60/55—Undercarriages with landing legs the legs being also used as ground propulsion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/86—Land vehicles
-
- B64C2201/042—
-
- B64C2201/108—
-
- B64C2201/128—
-
- B64C2201/141—
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/60—UAVs specially adapted for particular uses or applications for transporting passengers; for transporting goods other than weapons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/10—UAVs characterised by their flight controls autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/84—Waterborne vehicles
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Definitions
- the present invention relates generally to a vehicle capable of multiple varieties of locomotion. More specifically, the present invention relates to a vehicle that is capable of utilizing different methods of movement by rotating its propellers to accommodate air, ground, or water locomotion.
- Quadrotors and hex rotors have revolutionized a variety of applications, including toys, the delivery of goods, or the delivery of devices and information in the battlefield. Although the ability to fly allows such devices to reach locations that are inaccessible to ground vehicles, there are locations where ground vehicles are still best suited for a given task.
- a policeman involved in a hostage situation may like to have a flying vehicle capable of traversing an open doorway; however, he may then prefer to possess a ground vehicle for traversing the indoors of the building in search of the suspect.
- a combination between air and ground vehicles would be better suited for this mission.
- such a vehicle would be able to provide a significantly longer work time, since the ground vehicle consumes significantly less energy than the quadrotor. Similar levels of efficiency can be found with a quadrotor that becomes an air-boat.
- An autonomous vehicle is a vehicle that is capable of sensing its environment and navigating without human input.
- Autonomous vehicles can detect surroundings using a variety of techniques such as radar, LIDAR, GPS, odometry, and computer vision.
- Advanced control systems interpret sensory information to identify appropriate navigation paths, as well as obstacles and relevant signage.
- Autonomous vehicles have control systems that are capable of analyzing sensory data to distinguish between different objects and obstacles, which is very useful in planning a path to the desired destination.
- Connected vehicles are vehicles that use any of a number of different communication technologies to communicate with the driver, other cars on the road (vehicle-to-vehicle [V2V]), roadside infrastructure (vehicle-to-infrastructure [V2I]), and the “Cloud.” This technology can be used to not only improve vehicle safety, but also to improve vehicle efficiency and commute times.
- V2V vehicle-to-vehicle
- V2I vehicle-to-infrastructure
- Continuous track also called tank tread or caterpillar track, is a system of vehicle propulsion in which a continuous band of treads or track plates is driven by two or more wheels.
- GPS Global Positioning System
- the GPS Global Positioning System
- the GPS is a “constellation” of approximately 30 well-spaced satellites that orbit the Earth and make it possible for people with ground receivers to pinpoint their geographic location.
- the location accuracy is anywhere from 100 to 10 meters for most equipment. Accuracy can be pinpointed to within one (1) meter with special military-approved equipment. GPS equipment is widely used in science and has now become sufficiently low-cost so that almost anyone can own a GPS receiver.
- Hot swapping and hot plugging are terms used to describe the functions of replacing computer system components without shutting down the system. More specifically, hot swapping describes replacing components without significant interruption to the system, while hot plugging describes the addition of components that would expand the system without significant interruption to the operation of the system.
- hot swapping describes replacing components without significant interruption to the system
- hot plugging describes the addition of components that would expand the system without significant interruption to the operation of the system.
- An inertial measurement unit is an electronic device that measures and reports a body's specific force, angular rate, and sometimes the magnetic field surrounding the body, using a combination of accelerometers and gyroscopes, sometimes also magnetometers.
- IMUs are typically used to maneuver aircraft, including unmanned aerial vehicles (UAVs), among many others, and spacecraft, including satellites and landers. Recent developments allow for the production of IMU-enabled GPS devices.
- UAVs unmanned aerial vehicles
- satellites and landers including satellites and landers. Recent developments allow for the production of IMU-enabled GPS devices.
- An IMU allows a GPS receiver to work when GPS-signals are unavailable, such as in tunnels, inside buildings, or when electronic interference is present.
- a wireless IMU is known as a WIMU.
- Lidar (also called LIDAR, LiDAR, and LADAR) is a surveying method that measures distance to a target by illuminating that target with a laser light.
- LIDAR sometimes considered an acronym of Light Detection And Ranging, (sometimes Light Imaging, Detection, And Ranging)
- LADAR Light Imaging, Detection, And Ranging
- Lidar is popularly used to make high-resolution maps, with applications in geodesy, geomatics, archaeology, geography, geology, geomorphology, seismology, forestry, atmospheric physics, laser guidance, airborne laser swath mapping (ALSM), and laser altimetry.
- Lidar sometimes is called laser scanning and 3D scanning, with terrestrial, airborne, and mobile applications.
- Radar is an acronym for “radio detection and ranging.”
- a radar system usually operates in the ultra-high-frequency (UHF) or microwave part of the radio-frequency (RF) spectrum, and is used to detect the position and/or movement of objects.
- UHF ultra-high-frequency
- RF radio-frequency
- Radar can track storm systems, because precipitation reflects electromagnetic fields at certain frequencies. Radar can also render precise maps. Radar systems are widely used in air-traffic control, aircraft navigation, and marine navigation.
- UAV unmanned aerial vehicle
- UAS unmanned aircraft system
- the flight of UAVs may operate with various degrees of autonomy: either under remote control by a human operator, or fully or intermittently autonomously, by onboard computers.
- UGV unmanned ground vehicle
- the present invention is a vehicle capable of multiple varieties of locomotion comprising: a main body; a plurality of motors and blades providing flying capability; each motor being associated with and powering a blade assembly; two legs extending from opposing sides of the main body creating a ground propulsion system.
- the ground propulsion system comprised of two legs; the each leg connected to a track body at the opposing leg end connected to the main body; each track body comprised of a plurality of drive gears; each track body connected to and retaining a track providing ground propulsion; and the vehicle of the present invention can either drive or fly based on its base structure, in additional to carrying a payload.
- the payload is carried below the main body of the vehicle and between the tracks or running gear, the center of gravity is critical.
- the tracks are able to rotate up into a fly/flight mode to protect the blades during flight.
- the main body shell is supported by the tracks and their gearing.
- the batteries powering the electric motors are located under the main body as well for reducing the center of gravity.
- the vehicle When in flight mode, the vehicle has the tracks rotated up to protect the blades and the battery and payload, if so equipped, hang below the main body shell, tracks, electric motors, and blades.
- the motors of the vehicle of the present invention are servo based. The use of a servo allows the motor to be placed at any angle, not a limited amount of set positions/angles.
- FIG. 1 is a side view of a single blade vehicle of the present invention.
- FIG. 2 is a front view of a single blade vehicle of the present invention.
- FIG. 3 is a side view of a double blade vehicle of the present invention.
- FIG. 4 is a front view of a double blade vehicle of the present invention.
- the present invention is a vehicle capable of multiple varieties of locomotion, those being a drive mode and a fly mode.
- the vehicle of the present invention can either drive or fly based on its base structure, in additional to carrying a payload 102 .
- the center of gravity is critical.
- the payload 102 is secured to the main body 101 and hangs underneath it, contributing to a lower center of gravity.
- the tradeoff is that the larger the payload 102 , due to its location, results in a loss of ground clearance when in the drive mode.
- the tracks 103 are able to rotate up into a fly/flight mode to protect the blades 104 during flight.
- the main body shell 105 is supported by the tracks and their gearing 103 . This results in a vehicle that has a larger ground clearance compared to others currently being developed.
- the batteries 106 powering the electric motors 107 and 108 are located under the main body 101 as well for reducing the center of gravity.
- the batteries 106 and the payload 102 represent the most significant components that contribute to the overall weight of the vehicle.
- the vehicle When in flight mode, the vehicle has the tracks 103 rotated up to protect the blades 104 and the battery 106 and payload 102 , if so equipped, hang below the main body shell 105 , tracks 103 , electric motors 107 and 108 , and blades 1047 .
- the lower (z plane) and centrally located (with respect to the x and y planes) the center of gravity is, it acts like a pendulum and keeps the vehicle stable in various conditions.
- Another advantage of the tracks 103 being rotated up is that this movement enables a 360 degree view off a bottom mounted camera, when a camera is the payload 102 .
- the motors 107 and 108 of the vehicle of the present invention are servo based. Typically, in a vehicle capable of multiple varieties of locomotion, the motor must be in one of only two fixed positions. In the present invention, the use of a servo 111 allows the motors 107 and 108 to be placed at any angle, not a limited amount of set positions/angles.
- the vehicle can carry an unmanned air vehicle (UAV) or an unmanned ground vehicle (UGV).
- UAV unmanned air vehicle
- UGV unmanned ground vehicle
- the vehicle can fly and drive, and also deliver an additional UAV or UGV to a location by air, land, water, or any combination thereof.
- the vehicle of the present invention can be built to have the same functionality in various degrees of durability by altering the materials and size and strength of its component parts. This means the vehicle can range in size/weight from 120 to 5 pounds, but retain the same functionality and various payload capacities ranging from delivering batteries to containers.
- the combined UAV and UGV functionality also allows the vehicle to operate as a multi-vehicle system, where the vehicle can travel and land, then allow the UAV or UGV to carry out its function, which could be anything from delivering a secondary payload by air or ground to a secondary location. For example, a pizza or package delivery could be completed where the vehicle flies to a street or intersection, and then the UAV or UGV delivers the package to a specific location at that street or intersection, in a multi-step, multi-vehicle situation.
- the vehicle of the present invention is comprised of a plurality of sensors including LADAR in both single line and multiple line embodiments 112 .
- the vehicle can use the LADAR 112 to provide mapping and obstacle detection.
- the vehicle would be in fly mode using a single line LADAR to provide obstacle detection and two-dimensional mapping.
- a front facing LADAR provides horizontal line information while a rear sensor provides vertical line information.
- mapping occurs during normal flight or ground exercises. When the sensors wobble accuracy is diminished and mapping can become blurred.
- the vehicle uses its sensors to provide mapping in the direction it is moving or to its front, while using Ladar to detect the ground so that a correction can be made as the vehicle is in motion.
- the present invention can be equipped with ranging radios.
- Ranging radios can be used to measure the distance between the vehicle and other objects in its environment. In some situations, this can be used to monitor and maintain a specific distance between the vehicle and a walker/pedestrian or another vehicle.
- a plurality of ranging radios can be placed on each of the four corners of another vehicle, which could be stationary or in motion itself.
- the four ranging radios then provide corner information to the vehicle so that the vehicle can land on it.
- the present invention using ranging radios, can place the vehicle not just in the area of another vehicle, person, or combination thereof, but it can follow that target based on the information provided to it by the ranging radios. Additionally, multiple vehicles, each equipped with their own ranging radio can find each other using the ranging radios and then communicate with each other.
- the one or more vehicles can maintain complete functionality using only the sensors it is carrying and any additional information received from ranging radios detectable to it.
- the need for a GPS signal or any GPS information is removed and the vehicles will still be able to determine and know their location(s).
- a software method has been developed to control and use the information in the proper manner.
- the vehicle of the present invention can be used to gather visual information in a live stream format to be combined with model data for viewing by an operator or other interested parties at one or more remote locations from the vehicle.
- the vehicle is equipped with a single line sensor for mapping and the vehicle is rotated around the environment for continuous, real-time mapping.
- This data and information would be very difficult for an operator or other interested party to view.
- the information would make orientation of the vehicle and subsequent control and maneuverability very difficult as location and orientation based on a such information would be difficult to remember and control of direction and location quickly lost or confused by the operator. Equally, any third party viewer would have the same orientation issues with respect to the information.
- the blades are used in fly mode, but could also be used in a drive mode if the vehicle where on ice, water, or in another situation where additional ground propulsive force or propulsive ground force, not coming from the tracks or in combination with the tracks is desired.
- the present invention improves upon these prior art devices by using the servo which allows any angle of adjust compared to the prior art devices that used fixed positions of adjustment. Additionally, the present invention has a second hinge 116 to control and raise the tracks of the ground propulsion mechanism 115 to any desired angle.
- the vehicle is equipped with a double bladed design where the more common, single blades 104 of a drone or similar vehicle are replaced/supplemented with a double blade 117 and 118 .
- the second blade 117 and 118 located on the bottom side of the electric motors 107 and 108 are driving the pair of bottom/lower/second blades 117 and 118 and the corresponding top/upper blade 104 is located on the top side.
- Suspension solutions include a leaf spring design and a shock/damper design.
- the vehicle of the present invention is used in combination with a cradle that provides a means of securing it to another vehicle or stationary position as well as providing charging capability.
- Landing a vehicle such as a drone or one with capable of a variety of locomotions can be very difficult. Landing a flying vehicle is very difficult and often results in hard landings, or imperfect landings that can damage the vehicle or landing platform.
- a landing platform designed in the shape of a triangle or pyramid in the three dimensional shape/sense providers a larger margin for landing error, resulting in a larger sweet spot for a successful landing. This is due to the mechanical nature of the shape, which when combine with the legs and tracks of the present invention results in a self-correcting mechanical advantage once contact is made.
- the legs Upon contact between the tracks/legs portion of the vehicle and a pyramid shaped cradle or docking station, the legs, angled in an inverted triangle/pyramid shape engage the pyramid shape of the cradle and, following the laws of physics, will pull themselves into each other and settle into a position of having the lowest potential energy, which is that of an inverted triangle secured between the sides of two adjacent triangles, which is a particularly stable position.
- the angle of the legs/cradle is in a range of zero to 10 degree and optimally about 5 degrees.
- the legs are moved at an angle, to a mechanically more stable location then simply straight up and down and parallel to each other.
- the cradle and legs make contact.
- the rails of the cradle guide the tracks into a track slot.
- a charging mechanism then makes contact with a charging port on the vehicle.
- a closing pin can flip to lock and secure the tracks and/or legs into place against the cradle.
- the closing pin can also be equipped with a charging connection. If an imperfect landing occurs, an operator an use the tracks to drive the vehicle forward or backward until the tracks fall into the track retaining slots.
- the noise characteristic of the vehicle can be drastically affected by the selection of blades based on their size, pitch, and other factors.
- Each motor gives off a wave, which is in the spectrum for being heard by the human ear.
- the motors In order to avoid a vehicle that generates a standing wave, that can be continuously be heard, the motors must not run in sync or at the same RPM or at a multiple which can also create a standing or amplified wave.
- the motors need to be selected for RPM efficiency and arranged in a manner so that they are operated at their most efficient RPM, while not combining to create a standing wave.
- Blade angle of the vehicle of the present invention should not be horizontal as it provides for better control during landing.
- the present invention uses a linkage 129 that, when in flight, puts the blades 104 and 121 - 124 in a flat position for increased efficiency and control during flight modality. During landing, the same linkage 129 is used to place the blades 104 and 121 - 124 in a non-flat position, resulting in better control and handling characteristics.
- the angle of the blades on a drone or vehicle like that of the present invention are different for performance or landing.
- the present invention provides a means for the angel of the blades 104 and 121 - 124 to be changes based on a plurality of modalities, two of them being landing and performance/efficiency. This angle changed is done by adjusting the length of the linkage 129 .
- a single track 103 is replaced by a two or three track 136 embodiment where each segment of the track frame 103 has its own associated and corresponding track. This would eliminate the concave bend 130 in the single track embodiment.
- the vehicle of the present invention can incorporate solar panels to charge onboard batteries 1006 or provide energy directly to the components.
- the present invention uses hot swappable batteries 106 .
- the inventors use their own propriety electronics and PCBs to enable this feature with the vehicle.
- the linkage or legs 120 of the ground transportation mechanics 115 are not straight, but banana shaped to increase payload size.
- the four bar linkage 132 used minimizes parts and enables various angles to be used rather than fixed angles.
- the linkage 132 pulls into a hard stop 133 .
- a bar is used as the hard stop 133 making the vehicle more rigid.
- a loop 134 is used in fly mode to hard stop against the linkage 132 tube's circumference. This set of hard stops 133 and 134 reduces play in both the fly and drive modes. Without the hard stops 133 and 134 , the motors 125 - 128 would wiggle or vibrate, negatively impacting control. The motors 125 - 128 must be rigidly for control purposes.
- the vehicle can hold a position by using a camera as the payload looking down on an object or feature and holding a position with respect to the object or feature.
- a light can also be provided to light the object or feature in which the camera is fixed on and the vehicle is holding its position on.
- An alternative is to use infrared (IR) illumination to located, look down on, and hold position.
- IR infrared
- auto takeoff and landing controls the movement of the legs/arms of the ground propulsion mechanism based on an acoustic sensor, single line LADAR, or an inertial measurement unit (IMU).
- acoustic sensor single line LADAR
- IMU inertial measurement unit
- a single remote is used to control the vehicle in both ground and fly modes.
- a ranging radio in the controller allows the vehicle to follow the operator, any other object with a ranging radio, or return home in a non-GPS environment.
- variable pitch blades 104 and 121 - 124 the motors can be run at the correct RPM for their efficiency or operating range by changing pitch for performance or hovering to optimize energy consumption for performance, hovering, or in response to operating conditions. This can be done in configurations with one motor or two motors, but not with four motors.
- crisscross blades are linked which allows for larger blades before they collide. This is not possible on multi-rotor designs. With respect to current blade sizes, this embodiment, using the mechanical connection, allows massive blade sizes to be used.
- Track motors have decoders to provide wheel geometry.
- the vehicle of the present invention will operate in both drive and fly modes autonomously.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Remote Sensing (AREA)
- Motorcycle And Bicycle Frame (AREA)
Abstract
Description
- This application claims priority from U.S. Patent Application Ser. 62/413,474, entitled “Vehicle Capable of Multiple Varieties of Locomotion”, filed on 27 Oct. 2016.
- This application is related to U.S. patent application Ser. No. 14/928,648, entitled “Vehicle Capable of Multiple Varieties of Locomotion”, filed on 30 Oct. 2015, claiming priority from U.S. Patent Application Ser. 62/072,811.
- U.S. patent application Ser. No. 14/928,648 is a non-provisional of U.S. Patent Application Ser. 62/072,811, entitled “Vehicle Capable of Multiple Varieties of Locomotion”, filed on 30 Oct. 2014.
- Not Applicable
- Not Applicable
- The present invention relates generally to a vehicle capable of multiple varieties of locomotion. More specifically, the present invention relates to a vehicle that is capable of utilizing different methods of movement by rotating its propellers to accommodate air, ground, or water locomotion.
- Quadrotors and hex rotors have revolutionized a variety of applications, including toys, the delivery of goods, or the delivery of devices and information in the battlefield. Although the ability to fly allows such devices to reach locations that are inaccessible to ground vehicles, there are locations where ground vehicles are still best suited for a given task.
- For example, a policeman involved in a hostage situation may like to have a flying vehicle capable of traversing an open doorway; however, he may then prefer to possess a ground vehicle for traversing the indoors of the building in search of the suspect. A combination between air and ground vehicles would be better suited for this mission. In particular, such a vehicle would be able to provide a significantly longer work time, since the ground vehicle consumes significantly less energy than the quadrotor. Similar levels of efficiency can be found with a quadrotor that becomes an air-boat. In the next section, we will present different embodiments of the invention.
- An autonomous vehicle (driverless car, self-driving car, robotic car, and robotic drone) is a vehicle that is capable of sensing its environment and navigating without human input. Autonomous vehicles can detect surroundings using a variety of techniques such as radar, LIDAR, GPS, odometry, and computer vision. Advanced control systems interpret sensory information to identify appropriate navigation paths, as well as obstacles and relevant signage. Autonomous vehicles have control systems that are capable of analyzing sensory data to distinguish between different objects and obstacles, which is very useful in planning a path to the desired destination.
- Connected vehicles are vehicles that use any of a number of different communication technologies to communicate with the driver, other cars on the road (vehicle-to-vehicle [V2V]), roadside infrastructure (vehicle-to-infrastructure [V2I]), and the “Cloud.” This technology can be used to not only improve vehicle safety, but also to improve vehicle efficiency and commute times.
- Continuous track, also called tank tread or caterpillar track, is a system of vehicle propulsion in which a continuous band of treads or track plates is driven by two or more wheels.
- The GPS (Global Positioning System) is a “constellation” of approximately 30 well-spaced satellites that orbit the Earth and make it possible for people with ground receivers to pinpoint their geographic location. The location accuracy is anywhere from 100 to 10 meters for most equipment. Accuracy can be pinpointed to within one (1) meter with special military-approved equipment. GPS equipment is widely used in science and has now become sufficiently low-cost so that almost anyone can own a GPS receiver.
- Hot swapping and hot plugging are terms used to describe the functions of replacing computer system components without shutting down the system. More specifically, hot swapping describes replacing components without significant interruption to the system, while hot plugging describes the addition of components that would expand the system without significant interruption to the operation of the system. Once the appropriate software is installed on the computer, a user can plug and unplug the component without rebooting. A well-known example of this functionality is the Universal Serial Bus (USB) that allows users to add or remove peripheral components such as a mouse, keyboard, or printer.
- An inertial measurement unit (IMU) is an electronic device that measures and reports a body's specific force, angular rate, and sometimes the magnetic field surrounding the body, using a combination of accelerometers and gyroscopes, sometimes also magnetometers. IMUs are typically used to maneuver aircraft, including unmanned aerial vehicles (UAVs), among many others, and spacecraft, including satellites and landers. Recent developments allow for the production of IMU-enabled GPS devices. An IMU allows a GPS receiver to work when GPS-signals are unavailable, such as in tunnels, inside buildings, or when electronic interference is present. A wireless IMU is known as a WIMU.
- Lidar (also called LIDAR, LiDAR, and LADAR) is a surveying method that measures distance to a target by illuminating that target with a laser light. The name LIDAR, sometimes considered an acronym of Light Detection And Ranging, (sometimes Light Imaging, Detection, And Ranging), was originally a portmanteau of light and radar. Lidar is popularly used to make high-resolution maps, with applications in geodesy, geomatics, archaeology, geography, geology, geomorphology, seismology, forestry, atmospheric physics, laser guidance, airborne laser swath mapping (ALSM), and laser altimetry. Lidar sometimes is called laser scanning and 3D scanning, with terrestrial, airborne, and mobile applications.
- Payload is the carrying capacity of an aircraft or launch vehicle, usually measured in terms of weight. Depending on the nature of the flight or mission, the payload of a vehicle may include cargo, passengers, flight crew, munitions, scientific instruments or experiments, or other equipment. Extra fuel, when optionally carried, is also considered part of the payload. In a commercial context (i.e., an airline or air freight carrier), payload may refer only to revenue-generating cargo or paying passengers. There is a natural trade-off between the payload and the range of an aircraft.
- Radar is an acronym for “radio detection and ranging.” A radar system usually operates in the ultra-high-frequency (UHF) or microwave part of the radio-frequency (RF) spectrum, and is used to detect the position and/or movement of objects. Radar can track storm systems, because precipitation reflects electromagnetic fields at certain frequencies. Radar can also render precise maps. Radar systems are widely used in air-traffic control, aircraft navigation, and marine navigation.
- An unmanned aerial vehicle (UAV), commonly known as a drone, as an unmanned aircraft system (UAS), or by several other names, is an aircraft without a human pilot aboard. The flight of UAVs may operate with various degrees of autonomy: either under remote control by a human operator, or fully or intermittently autonomously, by onboard computers.
- An unmanned ground vehicle (UGV) is a vehicle that operates while in contact with the ground and without an onboard human presence. UGVs can be used for many applications where it may be inconvenient, dangerous, or impossible to have a human operator present.
- Table with element number corresponding to figures in non-provisional filing and part/element name.
- The present invention is a vehicle capable of multiple varieties of locomotion comprising: a main body; a plurality of motors and blades providing flying capability; each motor being associated with and powering a blade assembly; two legs extending from opposing sides of the main body creating a ground propulsion system. The ground propulsion system comprised of two legs; the each leg connected to a track body at the opposing leg end connected to the main body; each track body comprised of a plurality of drive gears; each track body connected to and retaining a track providing ground propulsion; and the vehicle of the present invention can either drive or fly based on its base structure, in additional to carrying a payload.
- The payload is carried below the main body of the vehicle and between the tracks or running gear, the center of gravity is critical. When the vehicle is in flight, the tracks are able to rotate up into a fly/flight mode to protect the blades during flight. The main body shell is supported by the tracks and their gearing. The batteries powering the electric motors are located under the main body as well for reducing the center of gravity.
- When in flight mode, the vehicle has the tracks rotated up to protect the blades and the battery and payload, if so equipped, hang below the main body shell, tracks, electric motors, and blades. The motors of the vehicle of the present invention are servo based. The use of a servo allows the motor to be placed at any angle, not a limited amount of set positions/angles.
- The accompanying drawings, which are incorporated herein a form a part of the specification, illustrate the present invention and, together with the description, further serve to explain the principles of the invention and to enable a person skilled in the pertinent art to make and use the invention.
-
FIG. 1 is a side view of a single blade vehicle of the present invention. -
FIG. 2 is a front view of a single blade vehicle of the present invention. -
FIG. 3 is a side view of a double blade vehicle of the present invention. -
FIG. 4 is a front view of a double blade vehicle of the present invention. - In the following detailed description of the invention of exemplary embodiments of the invention, reference is made to the accompanying drawings (where like numbers represent like elements), which form a part hereof, and in which is shown by way of illustration specific exemplary embodiments in which the invention may be practiced. These embodiments are described in sufficient detail to enable those skilled in the art to practice the invention, but other embodiments may be utilized and logical, mechanical, electrical, and other changes may be made without departing from the scope of the present invention. The following detailed description is, therefore, not to be taken in a limiting sense, and the scope of the present invention is defined only by the appended claims.
- In the following description, numerous specific details are set forth to provide a thorough understanding of the invention. However, it is understood that the invention may be practiced without these specific details. In other instances, well-known structures and techniques known to one of ordinary skill in the art have not been shown in detail in order not to obscure the invention. Referring to the figures, it is possible to see the various major elements constituting the apparatus of the present invention.
- Now referring to the Figures, the present invention and various embodiments are illustrated. The present invention is a vehicle capable of multiple varieties of locomotion, those being a drive mode and a fly mode. The vehicle of the present invention can either drive or fly based on its base structure, in additional to carrying a
payload 102. - With respect to the
payload 102, which is carried below the main body of thevehicle 101 and between the tracks or runninggear 103, the center of gravity is critical. With respect toFIGS. 2 and 3 , thepayload 102 is secured to themain body 101 and hangs underneath it, contributing to a lower center of gravity. The lower the center of gravity can be made, the more stable the vehicle will be in and during the flight mode. The tradeoff is that the larger thepayload 102, due to its location, results in a loss of ground clearance when in the drive mode. - When the vehicle is in flight, the
tracks 103 are able to rotate up into a fly/flight mode to protect theblades 104 during flight. - The
main body shell 105 is supported by the tracks and theirgearing 103. This results in a vehicle that has a larger ground clearance compared to others currently being developed. - The
batteries 106 powering theelectric motors main body 101 as well for reducing the center of gravity. Thebatteries 106 and thepayload 102 represent the most significant components that contribute to the overall weight of the vehicle. - When in flight mode, the vehicle has the
tracks 103 rotated up to protect theblades 104 and thebattery 106 andpayload 102, if so equipped, hang below themain body shell 105,tracks 103,electric motors - Another advantage of the
tracks 103 being rotated up is that this movement enables a 360 degree view off a bottom mounted camera, when a camera is thepayload 102. - Additionally, in flight mode, all weight is moved above the
head 109 at the top joint 110, while the weight of thebatteries 106 and anypayload 102 remain below thehead 109, along with their weight. - The
motors servo 111 allows themotors - In a specialized embodiment, the vehicle can carry an unmanned air vehicle (UAV) or an unmanned ground vehicle (UGV). Int is embodiment, the vehicle can fly and drive, and also deliver an additional UAV or UGV to a location by air, land, water, or any combination thereof. The vehicle of the present invention can be built to have the same functionality in various degrees of durability by altering the materials and size and strength of its component parts. This means the vehicle can range in size/weight from 120 to 5 pounds, but retain the same functionality and various payload capacities ranging from delivering batteries to containers.
- The combined UAV and UGV functionality also allows the vehicle to operate as a multi-vehicle system, where the vehicle can travel and land, then allow the UAV or UGV to carry out its function, which could be anything from delivering a secondary payload by air or ground to a secondary location. For example, a pizza or package delivery could be completed where the vehicle flies to a street or intersection, and then the UAV or UGV delivers the package to a specific location at that street or intersection, in a multi-step, multi-vehicle situation.
- In an autonomous embodiment, the vehicle of the present invention is comprised of a plurality of sensors including LADAR in both single line and
multiple line embodiments 112. The vehicle can use theLADAR 112 to provide mapping and obstacle detection. In this embodiment, the vehicle would be in fly mode using a single line LADAR to provide obstacle detection and two-dimensional mapping. A front facing LADAR provides horizontal line information while a rear sensor provides vertical line information. - One issue facing vehicle control and mapping is sensor “wobble”, which occurs during normal flight or ground exercises. When the sensors wobble accuracy is diminished and mapping can become blurred. To solve this issue, in a ground mode, during autonomous operation, the vehicle uses its sensors to provide mapping in the direction it is moving or to its front, while using Ladar to detect the ground so that a correction can be made as the vehicle is in motion.
- In another embodiment, the present invention can be equipped with ranging radios. Ranging radios can be used to measure the distance between the vehicle and other objects in its environment. In some situations, this can be used to monitor and maintain a specific distance between the vehicle and a walker/pedestrian or another vehicle.
- In one specific embodiment of the present invention, a plurality of ranging radios can be placed on each of the four corners of another vehicle, which could be stationary or in motion itself. The four ranging radios then provide corner information to the vehicle so that the vehicle can land on it.
- Currently, many UAVs will follow each other in a platooning type situation and merely execute a program to maintain direction and proximity, or they may even rely on GPS information to maintain and adjust their movement, but this does not work in a GPS-denied embodiment, and does not provide overcome many of the current shortcomings.
- For example, it is currently very difficult to correctly find and control a vehicle and have it follow another vehicle if they are out of sight of the operator. The present invention, using ranging radios, can place the vehicle not just in the area of another vehicle, person, or combination thereof, but it can follow that target based on the information provided to it by the ranging radios. Additionally, multiple vehicles, each equipped with their own ranging radio can find each other using the ranging radios and then communicate with each other.
- In the ranging radio embodiment, the one or more vehicles can maintain complete functionality using only the sensors it is carrying and any additional information received from ranging radios detectable to it. In this embodiment, the need for a GPS signal or any GPS information is removed and the vehicles will still be able to determine and know their location(s). Additionally, a software method has been developed to control and use the information in the proper manner.
- In another embodiment, the vehicle of the present invention can be used to gather visual information in a live stream format to be combined with model data for viewing by an operator or other interested parties at one or more remote locations from the vehicle. In this embodiment, the vehicle is equipped with a single line sensor for mapping and the vehicle is rotated around the environment for continuous, real-time mapping. This data and information would be very difficult for an operator or other interested party to view. For the operator, the information would make orientation of the vehicle and subsequent control and maneuverability very difficult as location and orientation based on a such information would be difficult to remember and control of direction and location quickly lost or confused by the operator. Equally, any third party viewer would have the same orientation issues with respect to the information.
- In an effort to make the information collected by the vehicle more valuable and user friendly, the vehicles continues visual data is combined with a 3D model of the location and the real time data is projected onto the 3D model like a table cloth covering a table. This projection of real time visual data onto the model makes many things possible. Now the operator and any third party viewer are not looking at two-dimensional graphical information, but three-dimensional information. This allows the operator to better control the vehicle and to avoid obstacles and identify and find better travel or following paths around the environment.
- Additionally, the information can be used to provide the automatic tracking of people and objects. In this application of the information, the movement of people and objects can be combined or added to the visual representation being show so that the visualizations is not a composite of live information and past or historical information on the movement of people or objects. This can be beneficial in many setting, one being military applications for tracking people and objects or identifying new or re-placed objects in a setting that could represent hidden bombs, mines, or other explosives.
- In yet another embodiment the vehicle can be equipped with LADAR or acoustical detectors.
- Now, focusing on the blades used by the vehicle of the present invention, the blades are used in fly mode, but could also be used in a drive mode if the vehicle where on ice, water, or in another situation where additional ground propulsive force or propulsive ground force, not coming from the tracks or in combination with the tracks is desired.
- The
ground propulsion mechanism 115, as shown in the figures, provides a means of track type propulsion similar to that of a tank.Continuous track 103, also called tank tread or caterpillar track, is a system of vehicle propulsion in which a continuous band of treads or track plates is driven by two or more wheels. In the present invention, thetracks 103 are not merely wrapped aroundwheels 113, but they also include and require an additional component to retain thetrack 103 against thewheels 113 since, thetrack 103 is comprised of an angle under 90 degrees, which would cause thetrack 103 to pull away or separate from thewheel 113. - The
ground propulsion mechanism 115 of the vehicle of the present invention is also unique in that it rotates up to protect theblades 104 when not in use. This provides a means of protection for theblades 104 when in a flight mode. Additionally, the present invention uses aservo 111 system that allows theground propulsion mechanism 115 andtracks 103 to be raised or lowered to any angle, not just fixed positions. This provides a means for adjusting the center of gravity of the vehicle, which is very important as now the vehicle can be optimally adjusted for weight distribution for anypayload 102, sensor package, or operational environmental conditions. This ability to adjust the center of gravity and provide protective coverage to theblades 104 andelectric motors - In the prior art, flying vehicles or drones, have been equipped with moving parts to control and raise the blades and engines at a different angle. The present invention improves upon these prior art devices by using the servo which allows any angle of adjust compared to the prior art devices that used fixed positions of adjustment. Additionally, the present invention has a
second hinge 116 to control and raise the tracks of theground propulsion mechanism 115 to any desired angle. - In another embodiment of the present invention shown in
FIGS. 3 and 4 , the vehicle is equipped with a double bladed design where the more common,single blades 104 of a drone or similar vehicle are replaced/supplemented with adouble blade second blade electric motors second blades upper blade 104 is located on the top side. - In yet another embodiment, the
ground propulsion mechanism 115 of the present invention can be further comprised of asuspension system 119 made from a heavier resin material or carbon fiber to strengthen the vehicle. In this embodiment, thetracks 103 remain as shown in the figures, but thesolid legs 120 are replaced by a configuration providing asuspension system 119. The leg and track location, angle, and position can be adjusted to handle various landing platforms and be adjusted for various weight ranges of the vehicle with and without a payload. - Suspension solutions include a leaf spring design and a shock/damper design.
- In another embodiment, the vehicle of the present invention is used in combination with a cradle that provides a means of securing it to another vehicle or stationary position as well as providing charging capability. Landing a vehicle such as a drone or one with capable of a variety of locomotions can be very difficult. Landing a flying vehicle is very difficult and often results in hard landings, or imperfect landings that can damage the vehicle or landing platform.
- What is needed is a mechanical constraint with a large “sweet spot” or window for providing a successful landing. A landing platform designed in the shape of a triangle or pyramid in the three dimensional shape/sense providers a larger margin for landing error, resulting in a larger sweet spot for a successful landing. This is due to the mechanical nature of the shape, which when combine with the legs and tracks of the present invention results in a self-correcting mechanical advantage once contact is made.
- Upon contact between the tracks/legs portion of the vehicle and a pyramid shaped cradle or docking station, the legs, angled in an inverted triangle/pyramid shape engage the pyramid shape of the cradle and, following the laws of physics, will pull themselves into each other and settle into a position of having the lowest potential energy, which is that of an inverted triangle secured between the sides of two adjacent triangles, which is a particularly stable position. The angle of the legs/cradle is in a range of zero to 10 degree and optimally about 5 degrees.
- In practice, the legs are moved at an angle, to a mechanically more stable location then simply straight up and down and parallel to each other. Next, as the vehicle engages the vehicle, the cradle and legs make contact. Here, the rails of the cradle guide the tracks into a track slot. A charging mechanism then makes contact with a charging port on the vehicle. A closing pin can flip to lock and secure the tracks and/or legs into place against the cradle. When in the closing location, the closing pin can also be equipped with a charging connection. If an imperfect landing occurs, an operator an use the tracks to drive the vehicle forward or backward until the tracks fall into the track retaining slots.
- In a variable pitch embodiment, the vehicle is equipped with double blades as shown in
FIGS. 3 and 4 . In this embodiment, an operator or software running on the vehicle can select an optimal blade pitch for the operating conditions or activity. In this embodiment, each blade 121-124 is controlled by its own, independent motor 125-127. Theblades bottom motor top blades top motor - Another consideration of the multi-blade embodiment is noise. The noise characteristic of the vehicle can be drastically affected by the selection of blades based on their size, pitch, and other factors. Each motor gives off a wave, which is in the spectrum for being heard by the human ear. In order to avoid a vehicle that generates a standing wave, that can be continuously be heard, the motors must not run in sync or at the same RPM or at a multiple which can also create a standing or amplified wave. The motors need to be selected for RPM efficiency and arranged in a manner so that they are operated at their most efficient RPM, while not combining to create a standing wave.
- In this manner, the motors can be run at a very efficient rate, without having to all run at the same RPM or in a synchronized manner to have the same or an increased efficiency as those run in a more simple, synchronized manner. To accomplish this, the present invention uses a variety of ratios of gears to ensure rotor rotation is not in sync or running at any multiples. An algorithm is used to calculate and determine the best combination of blade size, pitch, and motor RPM for the entire vehicle as a unit.
- Blade angle of the vehicle of the present invention should not be horizontal as it provides for better control during landing. The present invention uses a
linkage 129 that, when in flight, puts theblades 104 and 121-124 in a flat position for increased efficiency and control during flight modality. During landing, thesame linkage 129 is used to place theblades 104 and 121-124 in a non-flat position, resulting in better control and handling characteristics. - Just like the wings of an most commercial airplanes are construction with a slight upward tilt to provide better control on landing, the angle of the blades on a drone or vehicle like that of the present invention are different for performance or landing. The present invention provides a means for the angel of the
blades 104 and 121-124 to be changes based on a plurality of modalities, two of them being landing and performance/efficiency. This angle changed is done by adjusting the length of thelinkage 129. - The
tracks 103 used by the present invention for ground propulsion have a uniqueconcave bend 130. This requires the use of atrack tensioner 114 to keep them retained against thetrack frame 131. Thetrack frame 131, when made from a closed cell material can also double as floats or platoons, enabling the present invention to float and move on water. - In another track embodiment, a
single track 103 is replaced by a two or threetrack 136 embodiment where each segment of thetrack frame 103 has its own associated and corresponding track. This would eliminate theconcave bend 130 in the single track embodiment. -
Tracks 103 can be made out of various materials and contain various tread designs and other features such as blades or paddles. - In another embodiment, the vehicle of the present invention can incorporate solar panels to charge onboard batteries 1006 or provide energy directly to the components.
- The present invention uses hot
swappable batteries 106. The inventors use their own propriety electronics and PCBs to enable this feature with the vehicle. - One main advantage of the present invention is that the
blades 104 and 121-124 are occluded by thetracks 103. Similar vehicles in the prior art provide for multiple locomotion, but their track or ground transportation mechanism occludes the blades hindering performance and efficiency. - In another embodiment, the linkage or
legs 120 of theground transportation mechanics 115 are not straight, but banana shaped to increase payload size. The fourbar linkage 132 used minimizes parts and enables various angles to be used rather than fixed angles. - In some embodiments, there is an excessive amount of play or looseness in the
linkage 132. The present invention useshard stops 133 to remove this play. At the end of the range of motion, thelinkage 132 pulls into ahard stop 133. In drive mode a bar is used as thehard stop 133 making the vehicle more rigid. Aloop 134 is used in fly mode to hard stop against thelinkage 132 tube's circumference. This set ofhard stops hard stops - In an operating mode, the vehicle can hold a position by using a camera as the payload looking down on an object or feature and holding a position with respect to the object or feature.
- In this operational embodiment, a light can also be provided to light the object or feature in which the camera is fixed on and the vehicle is holding its position on. An alternative is to use infrared (IR) illumination to located, look down on, and hold position.
- In another embodiment, auto takeoff and landing controls the movement of the legs/arms of the ground propulsion mechanism based on an acoustic sensor, single line LADAR, or an inertial measurement unit (IMU).
- A single remote is used to control the vehicle in both ground and fly modes. A ranging radio in the controller allows the vehicle to follow the operator, any other object with a ranging radio, or return home in a non-GPS environment.
- In another embodiment using variable pitch blades, the
blades 104 and 121-124 may be controlled manually by a control mechanism to adjust the pitch for noise multipliers. Although this adjustment may not be efficient, the operator could prefer to have a quieter operating vehicle, even if that means the motors are working in an opposing direction to run quieter or cancel out any sound waves. - By using
variable pitch blades 104 and 121-124, the motors can be run at the correct RPM for their efficiency or operating range by changing pitch for performance or hovering to optimize energy consumption for performance, hovering, or in response to operating conditions. This can be done in configurations with one motor or two motors, but not with four motors. - In another embodiment, the present invention can twist blades base on velocity. Larger blades are more efficient as length is directly proportional to efficiency.
- In another embodiment, crisscross blades are linked which allows for larger blades before they collide. This is not possible on multi-rotor designs. With respect to current blade sizes, this embodiment, using the mechanical connection, allows massive blade sizes to be used.
- Noise cancellation is hard with multiple speeds. Active noise cancellation is easier with one motor at a steady speed compared to other embodiments described herein.
- In a double blade embodiment using crisscross blades, a twist in the track/rubber band track provides counter rotation. This enables the vehicle to fly upside down easily if the operator desires such functionality. Additionally, this embodiment could “stick” to a wall or provide extra traction using the blades when in drive mode is the surface has a low coefficient of friction.
- Track motors have decoders to provide wheel geometry.
- In future embodiments, the vehicle of the present invention will operate in both drive and fly modes autonomously.
- Thus, it is appreciated that the optimum dimensional relationships for the parts of the invention, to include variation in size, materials, shape, form, function, and manner of operation, assembly and use, are deemed readily apparent and obvious to one of ordinary skill in the art, and all equivalent relationships to those illustrated in the drawings and described in the above description are intended to be encompassed by the present invention.
- Furthermore, other areas of art may benefit from this method and adjustments to the design are anticipated. Thus, the scope of the invention should be determined by the appended claims and their legal equivalents, rather than by the examples given.
Claims (28)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US15/794,931 US20180117981A1 (en) | 2016-10-27 | 2017-10-26 | Vehicle Capable of Multiple Varieties of Locomotion |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201662413474P | 2016-10-27 | 2016-10-27 | |
US15/794,931 US20180117981A1 (en) | 2016-10-27 | 2017-10-26 | Vehicle Capable of Multiple Varieties of Locomotion |
Publications (1)
Publication Number | Publication Date |
---|---|
US20180117981A1 true US20180117981A1 (en) | 2018-05-03 |
Family
ID=62020191
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US15/794,931 Abandoned US20180117981A1 (en) | 2016-10-27 | 2017-10-26 | Vehicle Capable of Multiple Varieties of Locomotion |
US15/794,944 Active 2038-01-17 US11247522B2 (en) | 2016-10-27 | 2017-10-26 | Vehicle capable of multiple varieties of locomotion |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US15/794,944 Active 2038-01-17 US11247522B2 (en) | 2016-10-27 | 2017-10-26 | Vehicle capable of multiple varieties of locomotion |
Country Status (1)
Country | Link |
---|---|
US (2) | US20180117981A1 (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10207805B2 (en) * | 2017-01-06 | 2019-02-19 | Michael Steward Evans | Drone transport system |
CN109866936A (en) * | 2019-03-14 | 2019-06-11 | 燕山大学 | UAV Landing based on six degree of freedom hybrid mechanism recycles integrated mobile platform |
CN111469617A (en) * | 2020-03-23 | 2020-07-31 | 中国人民解放军军事科学院国防科技创新研究院 | Unmanned plane |
US20200354084A1 (en) * | 2016-06-10 | 2020-11-12 | ETAK Systems, LLC | Drone Package Loading Based on Package Characterization |
US20210009260A1 (en) * | 2019-07-11 | 2021-01-14 | The Boeing Company | Tuned mass damper for aircraft |
US20210094687A1 (en) * | 2019-09-30 | 2021-04-01 | Ford Global Technologies, Llc | Landing apparatuses for unmanned aerial vehicles |
CN114347736A (en) * | 2022-01-07 | 2022-04-15 | 中国人民解放军陆军装甲兵学院 | A Multi-Domain Target Indication Platform |
US12327852B2 (en) * | 2021-09-22 | 2025-06-10 | Volvo Truck Corporation | Cooling system for a vehicle |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9944386B1 (en) * | 2017-07-13 | 2018-04-17 | Kitty Hawk Corporation | Multicopter with wide span rotor configuration and protective fuselage |
US10086931B2 (en) | 2016-08-26 | 2018-10-02 | Kitty Hawk Corporation | Multicopter with wide span rotor configuration |
US10675990B2 (en) * | 2017-04-11 | 2020-06-09 | Anuj Sharma | Drone docking system |
US10526079B1 (en) | 2017-07-13 | 2020-01-07 | Kitty Hawk Corporation | Multicopter with wide span rotor configuration and protective fuselage |
US10059436B1 (en) | 2017-07-13 | 2018-08-28 | Kitty Hawk Corporation | Sealed float with batteries |
CN108873013B (en) * | 2018-06-27 | 2022-07-22 | 江苏大学 | Method for acquiring passable road area by adopting multi-line laser radar |
KR102083132B1 (en) * | 2019-12-12 | 2020-02-28 | 우현선박기술 주식회사 | Drone system for inspecting and measuring ships with ultrasonic wave thickness measurement technology and sending capabilities |
CN112093060B (en) * | 2020-10-10 | 2021-07-20 | 南京棠邑科创服务有限公司 | Device capable of increasing load capacity by utilizing multiple unmanned aerial vehicles |
CN112758342B (en) * | 2020-12-30 | 2022-06-07 | 山东省科学院海洋仪器仪表研究所 | Automatic recovery, release and charging device and method for multi-rotor unmanned aerial vehicle |
CN112895825B (en) * | 2021-03-17 | 2022-04-08 | 哈尔滨工程大学 | A variable-configuration multimodal amphibious joint |
CN117246283B (en) * | 2023-09-25 | 2024-05-17 | 北京朗信智能科技有限公司 | Chassis mechanism of multifunctional robot |
CN120117199B (en) * | 2025-05-15 | 2025-08-01 | 飞客工场科技(北京)有限公司 | Unmanned aerial vehicle truss storehouse and unmanned aerial vehicle that has it |
Citations (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3053480A (en) * | 1959-10-06 | 1962-09-11 | Piasecki Aircraft Corp | Omni-directional, vertical-lift, helicopter drone |
US3306250A (en) * | 1965-10-13 | 1967-02-28 | Arthur H Pitchford | Amphibious vehicle |
US20050003715A1 (en) * | 2003-06-18 | 2005-01-06 | Hewitt Stanley C. | Amphibious vehicle |
US20070228214A1 (en) * | 2005-09-26 | 2007-10-04 | Honeywell International Inc. | Autonomous launch pad for micro air vehicles |
US8639400B1 (en) * | 2012-09-26 | 2014-01-28 | Silverlit Limited | Altitude control of an indoor flying toy |
US20150014475A1 (en) * | 2013-05-03 | 2015-01-15 | Aerovironment, Inc. | Vertical Takeoff and Landing (VTOL) Air Vehicle |
US20150136902A1 (en) * | 2012-05-21 | 2015-05-21 | Messier-Dowty Limited | Aircraft brake assembly |
US9108479B1 (en) * | 2015-03-30 | 2015-08-18 | TTEH Associates, Trustee for Train track enabled helicopter CRT Trust | Train track enabled helicopter |
US20160023755A1 (en) * | 2014-05-05 | 2016-01-28 | King Fahd University Of Petroleum And Minerals | System and method for control of quadrotor air vehicles with tiltable rotors |
US20160130000A1 (en) * | 2014-11-11 | 2016-05-12 | Jon RIMANELLI | Unmanned air-ground vehicle |
US20160207637A1 (en) * | 2014-07-01 | 2016-07-21 | The Boeing Company | Mobile Unmanned Aerial Vehicle Infrastructure and Management System and Method |
FR3036379A1 (en) * | 2015-05-19 | 2016-11-25 | Florent Roque | DRONE WITH NOT VARIABLE ROTOR |
US20160368549A1 (en) * | 2015-06-19 | 2016-12-22 | Delve Equipment, LLC | Tracked vehicle suspension systems and methods |
US20170113797A1 (en) * | 2015-07-20 | 2017-04-27 | Allison Aviation Corp. | Convertible Aircraft |
US20170144771A1 (en) * | 2015-11-20 | 2017-05-25 | FlightWave Aerospace Systems | Gimbaled thruster configuration for use with unmanned aerial vehicle |
US20170225802A1 (en) * | 2014-10-13 | 2017-08-10 | Systems Engineering Associates Corporation | Systems and methods for deployment and operation of vertical take-off and landing (vtol) unmanned aerial vehicles |
US20180044000A1 (en) * | 2015-04-06 | 2018-02-15 | Davide VENTURELLI | Ground movement system plugin for vtol uavs |
US20180074488A1 (en) * | 2016-09-09 | 2018-03-15 | Wal-Mart Stores, Inc. | Geographic area monitoring systems and methods through interchanging tool systems between unmanned vehicles |
US20180079268A1 (en) * | 2015-03-19 | 2018-03-22 | Mitsubishi Heavy Industries, Ltd. | Amphibious vehicle |
US20180173245A1 (en) * | 2015-03-27 | 2018-06-21 | Planck Aerosystems Inc. | Unmanned aircraft navigation system and method |
US20190055018A1 (en) * | 2016-04-29 | 2019-02-21 | SZ DJI Technology Co., Ltd. | Systems and methods for uav transport and data acquisition |
Family Cites Families (52)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2702171A (en) | 1951-08-18 | 1955-02-15 | United Aircraft Corp | Flotation undercarriage for rotary wing aircraft |
US4682969A (en) | 1985-09-27 | 1987-07-28 | Mattel, Inc. | Reconfigurable vehicle-robot toy |
RU2166427C2 (en) | 1998-12-15 | 2001-05-10 | Кожевников Андрей Валерьевич | Versatile transformable modular robot |
IL138695A (en) | 2000-09-26 | 2004-08-31 | Rafael Armament Dev Authority | Unmanned mobile device |
US6930596B2 (en) | 2002-07-19 | 2005-08-16 | Ut-Battelle | System for detection of hazardous events |
US7834754B2 (en) | 2002-07-19 | 2010-11-16 | Ut-Battelle, Llc | Method and system for monitoring environmental conditions |
US7619739B1 (en) | 2002-08-29 | 2009-11-17 | Science Applications International Corporation | Detection and identification of biological agents using Bragg filters |
US9493235B2 (en) | 2002-10-01 | 2016-11-15 | Dylan T X Zhou | Amphibious vertical takeoff and landing unmanned device |
US7069124B1 (en) | 2002-10-28 | 2006-06-27 | Workhorse Technologies, Llc | Robotic modeling of voids |
US6974356B2 (en) | 2003-05-19 | 2005-12-13 | Nekton Research Llc | Amphibious robot devices and related methods |
US7343232B2 (en) | 2003-06-20 | 2008-03-11 | Geneva Aerospace | Vehicle control system including related methods and components |
US7398946B1 (en) | 2004-10-04 | 2008-07-15 | United States Of America As Represented By The Secretary Of The Air Force | Power line sentry charging |
DE102004063205B3 (en) | 2004-12-23 | 2006-05-04 | Julian Kuntz | Aircraft for transporting persons, has rotors/propellers with sheathings, which enable independent drive movement of aircraft on land according to function of wheel rims based on direct power transmission from aircraft to land |
US7389156B2 (en) | 2005-02-18 | 2008-06-17 | Irobot Corporation | Autonomous surface cleaning robot for wet and dry cleaning |
US8418957B2 (en) | 2005-11-09 | 2013-04-16 | Textron Innovations Inc. | Crash attenuation system for aircraft |
US8213977B2 (en) | 2007-06-15 | 2012-07-03 | Alcatel Lucent | Method and apparatus for presenting and controlling information for managing an event |
US8588852B2 (en) | 2007-09-28 | 2013-11-19 | Alcatel Lucent | Method and apparatus for controlling a phased deployment of a base station using an operational state of a vehicle |
US20090228355A1 (en) | 2008-03-07 | 2009-09-10 | Dawson Christopher J | Amelioration of unsolicited advertisements in a virtual universe through avatar transport offers |
US8464816B2 (en) | 2008-12-11 | 2013-06-18 | Carsaf, Llc | All-terrain hostile environment vehicle |
US8205820B2 (en) | 2009-02-03 | 2012-06-26 | Honeywell International Inc. | Transforming unmanned aerial-to-ground vehicle |
US20110061951A1 (en) | 2009-09-14 | 2011-03-17 | Ehud Gal | Transformable Robotic Platform and Methods for Overcoming Obstacles |
US8342440B2 (en) | 2009-12-10 | 2013-01-01 | Regents Of The University Of Minnesota | Miniature robotic vehicle with ground and flight capability |
US8167234B1 (en) | 2010-03-21 | 2012-05-01 | Michael Moore | Insect-like micro air vehicle having perching, energy scavenging, crawling, and offensive payload capabilities |
CN102050167B (en) | 2010-09-10 | 2012-05-16 | 北京航空航天大学 | Portable two-wheeled two-leg combined transformable robot |
FR2973335B1 (en) | 2011-03-29 | 2013-04-19 | Inst Superieur De L Aeronautique Et De L Espace | MICRO / NANO REMOTE CONTROL VEHICLE COMPRISING A SYSTEM FOR FLOOR, VERTICAL TAKEOFF AND LANDING |
US9004200B2 (en) | 2011-09-09 | 2015-04-14 | Pinhas Ben-Tzvi | Mobile robot with hybrid traction and mobility mechanism |
US8794564B2 (en) | 2012-08-02 | 2014-08-05 | Neurosciences Research Foundation, Inc. | Vehicle capable of in-air and on-ground mobility |
US8794566B2 (en) | 2012-08-02 | 2014-08-05 | Neurosciences Research Foundation, Inc. | Vehicle capable of stabilizing a payload when in motion |
US9061558B2 (en) | 2012-11-14 | 2015-06-23 | Illinois Institute Of Technology | Hybrid aerial and terrestrial vehicle |
US20140252166A1 (en) | 2013-03-06 | 2014-09-11 | Bell Helicopter Textron Inc. | Crash Load Attenuator for Water Ditching and Floatation |
EP2978665A4 (en) | 2013-03-24 | 2017-04-26 | Bee Robotics Corporation | Aerial farm robot system for crop dusting, planting, fertilizing and other field jobs |
US9216745B2 (en) | 2013-09-16 | 2015-12-22 | Disney Enterprises, Inc. | Shared control of semi-autonomous vehicles including collision avoidance in multi-agent scenarios |
US10399676B2 (en) | 2014-03-31 | 2019-09-03 | Working Drones, Inc. | Indoor and outdoor aerial vehicles for painting and related applications |
US9611038B2 (en) | 2014-06-03 | 2017-04-04 | Working Drones, Inc. | Mobile computing device-based guidance navigation and control for unmanned aerial vehicles and robotic systems |
US9550400B2 (en) | 2014-10-29 | 2017-01-24 | Qualcomm Incorporated | Unmanned aerial vehicle |
US9481460B1 (en) | 2015-04-15 | 2016-11-01 | International Business Machines Corporation | Drone-based microbial analysis system |
US9770703B1 (en) | 2015-06-12 | 2017-09-26 | The United States of America as reprensented by the Secretary of the Army | Magnetic materials for sensing and decontaminating toxic chemicals |
US10540901B2 (en) | 2015-11-23 | 2020-01-21 | Kespry Inc. | Autonomous mission action alteration |
AU2016359163A1 (en) | 2015-11-23 | 2018-07-05 | Kespry Inc. | Autonomous mission action alteration |
US9963230B2 (en) | 2016-01-11 | 2018-05-08 | The Procter & Gamble Company | Aerial drone cleaning device and method of cleaning a target surface therewith |
US20170199979A1 (en) | 2016-01-11 | 2017-07-13 | Bruce Reiner | Method and system of radiation profiling |
US20160144358A1 (en) | 2016-01-28 | 2016-05-26 | Nilesh Patel | Dynamic Lab on a Chip Based Point-Of-Care Device For Analysis of Pluripotent Stem Cells, Tumor Cells, Drug Metabolites, Immunological Response, Glucose Monitoring, Hospital Based Infectious Diseases, and Drone Delivery Point-of-Care Systems |
US20180180564A1 (en) | 2016-02-01 | 2018-06-28 | Nano Terra Inc. | Sensor device and methods |
US10175198B2 (en) | 2016-02-16 | 2019-01-08 | Inficon, Inc. | System and method for optimal chemical analysis |
CA3108226C (en) | 2016-04-29 | 2023-03-14 | United Parcel Service Of America, Inc. | Unmanned aerial vehicle pick-up and delivery systems |
US10730626B2 (en) | 2016-04-29 | 2020-08-04 | United Parcel Service Of America, Inc. | Methods of photo matching and photo confirmation for parcel pickup and delivery |
US10773177B2 (en) | 2016-05-19 | 2020-09-15 | Brave Robotics, Inc. | Transformable robot |
US10775792B2 (en) | 2017-06-13 | 2020-09-15 | United Parcel Service Of America, Inc. | Autonomously delivering items to corresponding delivery locations proximate a delivery route |
US20190009756A1 (en) | 2017-07-10 | 2019-01-10 | Qualcomm Incorporated | System and Method for Itinerant Power Source for Vehicles |
US10872534B2 (en) | 2017-11-01 | 2020-12-22 | Kespry, Inc. | Aerial vehicle inspection path planning |
US10834482B2 (en) | 2017-12-05 | 2020-11-10 | The Government of the United States of America, as represented by the Secretary of Homeland Security | Systems and methods for integrating first responder technologies |
US11884175B2 (en) | 2019-06-26 | 2024-01-30 | Robotic Research Opco, Llc | Self-powered drone tether |
-
2017
- 2017-10-26 US US15/794,931 patent/US20180117981A1/en not_active Abandoned
- 2017-10-26 US US15/794,944 patent/US11247522B2/en active Active
Patent Citations (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3053480A (en) * | 1959-10-06 | 1962-09-11 | Piasecki Aircraft Corp | Omni-directional, vertical-lift, helicopter drone |
US3306250A (en) * | 1965-10-13 | 1967-02-28 | Arthur H Pitchford | Amphibious vehicle |
US20050003715A1 (en) * | 2003-06-18 | 2005-01-06 | Hewitt Stanley C. | Amphibious vehicle |
US20070228214A1 (en) * | 2005-09-26 | 2007-10-04 | Honeywell International Inc. | Autonomous launch pad for micro air vehicles |
US20150136902A1 (en) * | 2012-05-21 | 2015-05-21 | Messier-Dowty Limited | Aircraft brake assembly |
US8639400B1 (en) * | 2012-09-26 | 2014-01-28 | Silverlit Limited | Altitude control of an indoor flying toy |
US20150014475A1 (en) * | 2013-05-03 | 2015-01-15 | Aerovironment, Inc. | Vertical Takeoff and Landing (VTOL) Air Vehicle |
US20160023755A1 (en) * | 2014-05-05 | 2016-01-28 | King Fahd University Of Petroleum And Minerals | System and method for control of quadrotor air vehicles with tiltable rotors |
US20160207637A1 (en) * | 2014-07-01 | 2016-07-21 | The Boeing Company | Mobile Unmanned Aerial Vehicle Infrastructure and Management System and Method |
US20170225802A1 (en) * | 2014-10-13 | 2017-08-10 | Systems Engineering Associates Corporation | Systems and methods for deployment and operation of vertical take-off and landing (vtol) unmanned aerial vehicles |
US20160130000A1 (en) * | 2014-11-11 | 2016-05-12 | Jon RIMANELLI | Unmanned air-ground vehicle |
US20180079268A1 (en) * | 2015-03-19 | 2018-03-22 | Mitsubishi Heavy Industries, Ltd. | Amphibious vehicle |
US20180173245A1 (en) * | 2015-03-27 | 2018-06-21 | Planck Aerosystems Inc. | Unmanned aircraft navigation system and method |
US9108479B1 (en) * | 2015-03-30 | 2015-08-18 | TTEH Associates, Trustee for Train track enabled helicopter CRT Trust | Train track enabled helicopter |
US20180044000A1 (en) * | 2015-04-06 | 2018-02-15 | Davide VENTURELLI | Ground movement system plugin for vtol uavs |
FR3036379A1 (en) * | 2015-05-19 | 2016-11-25 | Florent Roque | DRONE WITH NOT VARIABLE ROTOR |
US20160368549A1 (en) * | 2015-06-19 | 2016-12-22 | Delve Equipment, LLC | Tracked vehicle suspension systems and methods |
US20170113797A1 (en) * | 2015-07-20 | 2017-04-27 | Allison Aviation Corp. | Convertible Aircraft |
US20170144771A1 (en) * | 2015-11-20 | 2017-05-25 | FlightWave Aerospace Systems | Gimbaled thruster configuration for use with unmanned aerial vehicle |
US20190055018A1 (en) * | 2016-04-29 | 2019-02-21 | SZ DJI Technology Co., Ltd. | Systems and methods for uav transport and data acquisition |
US20180074488A1 (en) * | 2016-09-09 | 2018-03-15 | Wal-Mart Stores, Inc. | Geographic area monitoring systems and methods through interchanging tool systems between unmanned vehicles |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20200354084A1 (en) * | 2016-06-10 | 2020-11-12 | ETAK Systems, LLC | Drone Package Loading Based on Package Characterization |
US12358644B2 (en) * | 2016-06-10 | 2025-07-15 | Metal Raptor Inc. | Drone package loading based on package characterization |
US10207805B2 (en) * | 2017-01-06 | 2019-02-19 | Michael Steward Evans | Drone transport system |
CN109866936A (en) * | 2019-03-14 | 2019-06-11 | 燕山大学 | UAV Landing based on six degree of freedom hybrid mechanism recycles integrated mobile platform |
US20210009260A1 (en) * | 2019-07-11 | 2021-01-14 | The Boeing Company | Tuned mass damper for aircraft |
US11548626B2 (en) * | 2019-07-11 | 2023-01-10 | The Boeing Company | Tuned mass damper for aircraft |
US20210094687A1 (en) * | 2019-09-30 | 2021-04-01 | Ford Global Technologies, Llc | Landing apparatuses for unmanned aerial vehicles |
US11794894B2 (en) * | 2019-09-30 | 2023-10-24 | Ford Global Technologies, Llc | Landing apparatuses for unmanned aerial vehicles |
CN111469617A (en) * | 2020-03-23 | 2020-07-31 | 中国人民解放军军事科学院国防科技创新研究院 | Unmanned plane |
US12327852B2 (en) * | 2021-09-22 | 2025-06-10 | Volvo Truck Corporation | Cooling system for a vehicle |
CN114347736A (en) * | 2022-01-07 | 2022-04-15 | 中国人民解放军陆军装甲兵学院 | A Multi-Domain Target Indication Platform |
Also Published As
Publication number | Publication date |
---|---|
US20180117980A1 (en) | 2018-05-03 |
US11247522B2 (en) | 2022-02-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US11247522B2 (en) | Vehicle capable of multiple varieties of locomotion | |
US12351296B2 (en) | Adaptive thrust vector unmanned aerial vehicle | |
US20220357753A1 (en) | Drop-off location planning for delivery vehicle | |
AU2019216716B2 (en) | Trajectory planner for a vehicle | |
US8543265B2 (en) | Systems and methods for unmanned aerial vehicle navigation | |
US7818127B1 (en) | Collision avoidance for vehicle control systems | |
EP3428766B1 (en) | Multi-sensor environmental mapping | |
JP5688700B2 (en) | MOBILE BODY CONTROL DEVICE AND MOBILE BODY HAVING MOBILE BODY CONTROL DEVICE | |
US11307583B2 (en) | Drone with wide frontal field of view | |
US12110106B2 (en) | Aerial vehicle with differential control mechanisms | |
US9975624B1 (en) | Multicopter propeller guard system | |
RU2518440C2 (en) | Pilotless aircraft and aerial monitoring complex for it | |
US20200307783A1 (en) | Compact Transformable Robot | |
Danko et al. | Robotic rotorcraft and perch-and-stare: Sensing landing zones and handling obscurants | |
KR102861523B1 (en) | Trajectory planner for a vehicle | |
Ollero et al. | Aerial Robots | |
Panigrahi et al. | Design Principles of Autonomous Systems: UAV, UGV, and AUV | |
McLain et al. | Obstacle and Terrain Avoidance for Miniature Aerial Vehicles | |
MX2008006166A (en) | Control system for automatic circle flight |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STPP | Information on status: patent application and granting procedure in general |
Free format text: DOCKETED NEW CASE - READY FOR EXAMINATION |
|
AS | Assignment |
Owner name: ROBOTIC RESEARCH, LLC, MARYLAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:LACAZE, ALBERTO DANIEL, MR.;MURPHY, KARL NICHOLAS, MR.;SIGNING DATES FROM 20190508 TO 20190510;REEL/FRAME:049315/0392 Owner name: ROBOTIC RESEARCH, LLC, MARYLAND Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:LACAZE, ALBERTO DANIEL, MR.;MURPHY, KARL NICHOLAS, MR.;REEL/FRAME:049315/0195 Effective date: 20190529 |
|
AS | Assignment |
Owner name: ROBOTIC RESEARCH, LLC, MARYLAND Free format text: CORRECTIVE ASSIGNMENT TO CORRECT THE INCORRECT ASSIGNMENT 15/903,136 PREVIOUSLY RECORDED ON REEL 049315 FRAME 0195. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT;ASSIGNORS:LACAZE, ALBERTO DANIEL, MR.;MURPHY, KARL NICHOLAS, MR.;REEL/FRAME:049475/0907 Effective date: 20190529 Owner name: ROBOTIC RESEARCH, LLC, MARYLAND Free format text: CORRECTIVE ASSIGNMENT TO CORRECT THE INCORRECT APPLICATION NUMBER 15/903,136 PREVIOUSLY RECORDED ON REEL 049315 FRAME 0195. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT;ASSIGNORS:LACAZE, ALBERTO DANIEL, MR.;MURPHY, KARL NICHOLAS, MR.;REEL/FRAME:049562/0200 Effective date: 20190529 |
|
STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
STPP | Information on status: patent application and granting procedure in general |
Free format text: RESPONSE TO NON-FINAL OFFICE ACTION ENTERED AND FORWARDED TO EXAMINER |
|
STPP | Information on status: patent application and granting procedure in general |
Free format text: NON FINAL ACTION MAILED |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |
|
AS | Assignment |
Owner name: ROBOTIC RESEARCH OPCO, LLC, MARYLAND Free format text: MERGER;ASSIGNOR:ROBOTIC RESEARCH, LLC;REEL/FRAME:060877/0929 Effective date: 20211015 |