CN108860603A - A kind of single hovering flight pedal - Google Patents
A kind of single hovering flight pedal Download PDFInfo
- Publication number
- CN108860603A CN108860603A CN201810638309.1A CN201810638309A CN108860603A CN 108860603 A CN108860603 A CN 108860603A CN 201810638309 A CN201810638309 A CN 201810638309A CN 108860603 A CN108860603 A CN 108860603A
- Authority
- CN
- China
- Prior art keywords
- fixedly connected
- wall
- hovering flight
- block
- panel
- 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.)
- Withdrawn
Links
- 238000003466 welding Methods 0.000 claims description 7
- ZZUFCTLCJUWOSV-UHFFFAOYSA-N furosemide Chemical group C1=C(Cl)C(S(=O)(=O)N)=CC(C(O)=O)=C1NCC1=CC=CO1 ZZUFCTLCJUWOSV-UHFFFAOYSA-N 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 2
- 230000005611 electricity Effects 0.000 abstract description 16
- 230000000694 effects Effects 0.000 abstract description 11
- 238000012360 testing method Methods 0.000 abstract description 7
- 238000005516 engineering process Methods 0.000 abstract description 3
- 239000000725 suspension Substances 0.000 abstract description 2
- 238000000034 method Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000034994 death Effects 0.000 description 1
- 231100000517 death Toxicity 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 210000000232 gallbladder Anatomy 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
-
- 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
- B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The present invention relates to single suspension technology fields, and disclose a kind of single hovering flight pedal, including hovering flight device.The present invention solves single hovering flight device when in use, need the rate regulation to individual lift device, such as when test man's landing, only to the control of revolving speed, it can just guarantee that test man steadily lands, not so the problem of necessarily causing casualties is landed suddenly, this programme passes through the rotational speed regulation panel that connects on the front of wind speed round control panel, wherein the effect of rotational speed regulation panel is to control electricity size, when electricity is small, motor suffered by rotation control motor is affected, revolving speed is with becoming smaller, when otherwise electricity is big, revolving speed becomes larger, wherein rotational speed regulation panel is divided into three gears, propeller blade is driven to be rotated positioned at rotation column itself rotation that the top of rotation control motor is connected.
Description
Technical field
The present invention relates to single suspension technology field, specially a kind of single hovering flight pedal.
Background technique
With the invention and extensive use of internal combustion engine, aerial flight is increasingly becoming possibility.1903, the U.S.
Lai Te brother takes the lead in producing the aircraft that can be flown in american system, and realizes the dream of flight.Then, aircraft and its correlation
Science and Technology, developed rapidly, but in really a remote dream of China, as the step of era development also has one
A little National People's Congress's gallbladders propose some methods, but we do not see that U.S.'s Martin Corporation with regard to pushing away to a high-profile as substantive progress
It is a out to be suitble to manned single aerodynamic vehicle.
When in use for single hovering flight device, the rate regulation to individual lift device is needed, such as is being tested
When member's landing, only to the control of revolving speed, it can just guarantee that test man steadily lands, and not so lands suddenly and necessarily causes people
Member's injures and deaths.
Summary of the invention
（One）The technical issues of solution
In view of the deficiencies of the prior art, the present invention provides a kind of single hovering flight pedal, single hovering flight device is solved
When in use, the rate regulation to individual lift device is needed, not so lands the problem of necessarily causing casualties suddenly, this
Outside, using the cooperation of shoulder belt placer and shoulder belt ontology, reach the fixation to people's shoulder, be equivalent to the effect of safety belt, greatly
The safety of aircraft is improved greatly.
（Two）Technical solution
To achieve the above object, the present invention provides the following technical solutions：A kind of single hovering flight pedal, including hovering flight
Device, the left and right sides is fixedly connected to shoulder belt placer, the front of the shoulder belt placer on the front of the hovering flight device
On be fixedly connected with shoulder belt ontology, the bottom of the shoulder belt placer is fixedly connected with fixed link, under the outer wall of the fixed link
Side is connected with sleeve, and screw thread hand handle, the left and right sides of the hovering flight device are fixedly connected on the outer wall of the sleeve
It is fixedly connected to wind speed round control panel, is fixedly connected with rotational speed regulation face on the front of the wind speed round control panel
Plate is fixedly connected with conducting wire on the outer wall of the wind speed round control panel, wind wheel ontology, institute is provided at the top of the conducting wire
It states and is fixedly connected with closing disk in the bottom interior wall of wind wheel ontology, position is fixedly connected among the top face of the wind wheel ontology
There is large-scale silk nut living, is fixedly connected with connection component, the top of the connection component in the top exterior walls of the wind wheel ontology
Left side is fixedly connected with bolt, and the top left side of connection component, and the top left with wind wheel ontology are run through in the bottom of the bolt
Side is fixedly connected, and the front upside of the hovering flight device is fixedly connected with air bag placer.
It is fixedly connected to long geosynclinal block on the left and right sides inner wall of the large-scale silk bolt living, is lived in the slot of the long geosynclinal block
It is dynamic to be connected with block, rotation column is fixedly connected between two blocks, the bottom of the rotation column is fixedly connected with rotation
Control motor, be fixedly connected with propeller blade on the outer wall of the rotation column, the bottom of the rotation control motor with lead
It is fixedly connected at the top of line, the propeller blade is four groups and cooperates.
Preferably, support cylinder is fixedly connected in the bottom interior wall of the shoulder belt placer, the shoulder belt placer
It is groove-like on top and bottom inner wall, the top and bottom of the support cylinder is respectively positioned in groove, the support cylinder
Outer wall on be socketed with rotating cylinder, belt is fixedly connected on the outer wall of the rotating cylinder, the bottom of the belt is fixed with stationary plane
Plate, the bottom of the fixed panel are fixedly connected with spring, and the spring and fixed panel are respectively positioned in holder, the spring
Bottom be it is planar, the right side inner wall of the bottom of the spring and holder welds.
Preferably, wide head grafting is fixedly connected on the outside of the left and right sides outer wall of the hovering flight device and wind wheel ontology
Block, the top of the width head grafting block is wide head, and the bottom of wide head grafting block is the right side inner wall for being welded on wind wheel ontology
On.
Preferably, the intermediate position of the fixed panel is circular hole, and the block is adapted with elongated slot block size, described
Block is discoid with long geosynclinal block.
Preferably, the bottom of the screw thread hand handle is through the outer wall front of sleeve, and activity is extruded in the outer wall of fixed link
On, the bottom of the sleeve is fixedly connected with fixed block, and welding block, the welding are fixedly connected on the front of the fixed block
Ball slot is offered on the front of block, and ball slot is long mode hemisphere channel-shaped, is fixedly connected on the outer wall of the ball slot
Grip, the bottom of the fixed block are fixedly connected with sole, and object is fixedly connected on the right side of the sole and places soft band.
Working principle：This programme by the rotational speed regulation panel that is connected on the front of wind speed round control panel, wherein
The effect of rotational speed regulation panel be to electricity size control, when electricity is small, rotation control motor suffered by motor by
To influence, revolving speed is with becoming smaller, otherwise electricity is big, revolving speed becomes larger, and wherein rotational speed regulation panel is divided into three gears,
Propeller blade is driven to be rotated positioned at rotation column itself rotation that the top of rotation control motor is connected.
（Three）Beneficial effect
The present invention provides a kind of single hovering flight pedals.Has following beneficial effect：
（1）This programme controls the cooperation of motor using wind speed round control panel and wind wheel ontology and rotation, and this programme passes through
The rotational speed regulation panel connected on the front of wind speed round control panel, wherein the effect of rotational speed regulation panel is to electricity
Size control, when electricity is small, motor suffered by rotation control motor is affected, and revolving speed is with becoming smaller, otherwise electricity
When big, revolving speed becomes larger, and wherein rotational speed regulation panel is divided into three gears, and the top positioned at rotation control motor is connected
Rotation column itself rotation and drive propeller blade to be rotated, connected at left and right sides of the top of rotation column
Block is inserted into the inner cavity of large-scale silk nut living, and the length by being connected on the left and right sides inner wall of large-scale silk nut living
Geosynclinal block carries out carrying out block placement fixation, and is fixed by closing disk to the support of large-scale silk nut living, solves sole flight
Device when in use, needs the rate regulation to individual lift device, such as when test man's landing, only to revolving speed
Control, can just guarantee that test man steadily lands, and not so lands suddenly and necessarily causes casualties.
（2）This programme uses the cooperation of shoulder belt placer and shoulder belt ontology, and this programme passes through in the bottom of shoulder belt placer
The support cylinder connected on inner wall, by covering the rotating cylinder of elder sister on the outer wall of support cylinder, and shoulder belt ontology is to be wrapped in turn
On the outer wall of cylinder, secondly supports on the upside of the outer wall of cylinder and be fixedly connected with belt, through rotating cylinder under the pulling of shoulder belt ontology, i.e.,
It can be rotated with support cylinder is closed, and be connected to the belt on the upside of support cylindrical outer wall this moment and be supported turning for cylinder
Dynamic, also will appear must will appear elastic force wherein the spring for being connected to belt bottom is being pulled to the winding of support cylinder
Recoil, the length that can be pulled out to shoulder belt ontology is shunk, and has reached the fixation to people's shoulder, is equivalent to the effect of safety belt
Fruit.
Detailed description of the invention
Fig. 1 is hovering flight device structural schematic diagram of the present invention；
Fig. 2 is hovering flight device front view of the present invention；
Fig. 3 is wind wheel ontology of the present invention and component structure diagram；
Fig. 4 is shoulder belt placer structural schematic diagram of the present invention.
In figure：1 hovering flight device, 2 shoulder belt placers, 3 wind speed round control panels, 4 rotational speed regulation panels, 5 conducting wires, 6
Wide head grafting block, 7 large-scale living silk nuts, 8 wind wheel ontologies, 9 bolts, 10 connection components, 11 air bag placers, 12 shoulder belt ontologies,
13 fixed links, 14 screw thread hand handles, 15 fixed blocks, 16 welding blocks, 17 sleeves, 18 ball slots, 19 grips, 20 objects are placed soft
Band, 21 soles, 22 closing disks, 23 propeller blades, 24 blocks, 25 long geosynclinal blocks, 26 rotation columns, 27 rotation control motors, 28
Support cylinder, 29 rotating cylinders, 30 belts, 31 holders, 32 fixed panels, 33 springs.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
As shown in Figs 1-4, the present invention provides a kind of technical solution：A kind of single hovering flight pedal, including hovering flight
Device 1, the left and right sides is fixedly connected to shoulder belt placer 2 on the front of hovering flight device 1, solid on the front of shoulder belt placer 2
Surely it is connected with shoulder belt ontology 12, the bottom of shoulder belt placer 2 is fixedly connected with fixed link 13, activity on the downside of the outer wall of fixed link 13
It is connected with sleeve 17, screw thread hand handle 14 is fixedly connected on the outer wall of sleeve 17, the left and right sides of hovering flight device 1 is fixed to be connected
It is connected to wind speed round control panel 3, rotational speed regulation panel 4 is fixedly connected on the front of wind speed round control panel 3, wind wheel turns
Conducting wire 5 is fixedly connected on the outer wall of fast control panel 3, the top of conducting wire 5 is provided with wind wheel ontology 8, the bottom of wind wheel ontology 8
Closing disk 22 is fixedly connected on inner wall, position is fixedly connected with large-scale silk nut 7 living among the top face of wind wheel ontology 8,
Connection component 10 is fixedly connected in the top exterior walls of wind wheel ontology 8, the top left side of connection component 10 is fixedly connected with bolt
9, the top left side of connection component 10 is run through in the bottom of bolt 9, and is fixedly connected with the top left side of wind wheel ontology 8, suspends and flies
The front upside of row device 1 is fixedly connected with air bag placer 11, and the bottom of screw thread hand handle 14 is positive through the outer wall of sleeve 17, and
Activity is extruded on the outer wall of fixed link 13, and the bottom of sleeve 17 is fixedly connected with fixed block 15, is consolidated on the front of fixed block 15
Surely it is connected with welding block 16, ball slot 18 is offered on the front of welding block 16, and ball slot 18 is long mode hemisphere channel-shaped, circle
Grip 19 is fixedly connected on the outer wall of ball groove 18, the bottom of fixed block 15 is fixedly connected with sole 21, the right side of sole 21
It is fixedly connected with object and places soft band 20, be fixedly connected to long geosynclinal block 25 on the left and right sides inner wall of large size silk bolt 7 living, it is long
It is connected with block 24 in the slot of geosynclinal block 25, rotation column 26 is fixedly connected between two blocks 24, rotation column 26
Bottom is fixedly connected with rotation control motor 27, rotates and is fixedly connected with propeller blade 23 on the outer wall of column 26, rotation control
The bottom of motor 27 processed is fixedly connected with the top of conducting wire 5, and propeller blade 23 is four groups and cooperates, shoulder belt placer
It is fixedly connected with support cylinder 28 in 2 bottom interior wall, is groove-like on the top and bottom inner wall of shoulder belt placer 2, branch
The top and bottom for holding round column 28 is respectively positioned in groove, is supported and is socketed with rotating cylinder 29, the outer wall of rotating cylinder 29 on the outer wall of cylinder 28
On be fixedly connected with belt 30, the bottom of belt 30 is fixed with fixed panel 32, and the bottom of fixed panel 32 is fixedly connected with bullet
Spring 33, spring 33 and fixed panel 32 are respectively positioned in holder 31, the bottom of spring 33 be it is planar, the bottom of spring 33 with put
The right side inner wall welding of box 31 is set, the left and right sides outer wall of hovering flight device 1 and the outside of wind wheel ontology 8 are fixedly connected with wide head
Grafting block 6, the top of wide head grafting block 6 is wide head, and the bottom of wide head grafting block 6 is the right side for being welded on wind wheel ontology 8
On inner wall, the intermediate position of fixed panel 32 is circular hole, and block 24 is adapted with long 25 size of geosynclinal block, block 24 and long geosynclinal block
25 be discoid.
Working principle：This programme by the rotational speed regulation panel 4 that is connected on the front of wind speed round control panel 3,
The effect of transfer speed adjusting panel 4 is to control electricity size, when electricity is small, electricity suffered by rotation control motor 27
Machine is affected, revolving speed is with becoming smaller, otherwise electricity is big, revolving speed becomes larger, and wherein rotational speed regulation panel 4 is divided into three
Gear drives propeller blade to be revolved positioned at rotation column 26 itself rotation that the top of rotation control motor 27 is connected
Turn.
It can to sum up obtain, this programme controls matching for motor 27 using wind speed round control panel 3 and wind wheel ontology 8 and rotation
It closes, this programme is by the rotational speed regulation panel 4 connected on the front of wind speed round control panel 3, wherein rotational speed regulation panel 4
Effect be to electricity size control, when electricity is small, rotation control motor 27 suffered by motor be affected, revolving speed
With becoming smaller, otherwise electricity is big, revolving speed becomes larger, and wherein rotational speed regulation panel 4 is divided into three gears, is located at rotation control
The rotation column 26 that the top of motor 27 processed is connected itself rotates and propeller blade is driven to be rotated, and is located at rotation column
The block 24 connected at left and right sides of 26 top is inserted into the inner cavity of large-scale silk nut 7 living, and by large size silk spiral shell living
The long geosynclinal block 25 connected on the left and right sides inner wall of cap 7 carries out carrying out block 24 placement fixation, and by closing disk 22 to big
The support of type silk nut 7 living is fixed, and is solved individual lift device when in use, is needed the rate tune to individual lift device
Control, such as when test man's landing, only to the control of revolving speed, can just guarantee that test man steadily lands, not so suddenly
Landing necessarily causes casualties, and this programme uses the cooperation of shoulder belt placer 2 and shoulder belt ontology 12, and this programme passes through in shoulder belt
The support cylinder 28 connected in the bottom interior wall of placer 2, by covering the rotating cylinder 29 of elder sister on the outer wall of support cylinder 28, and
Shoulder belt ontology 12 is to be wrapped on the outer wall of rotating cylinder 29, secondly supports on the upside of the outer wall of cylinder 28 and is fixedly connected with belt 30, leads to
Rotating cylinder 29 is crossed under the pulling of shoulder belt ontology 12, can be rotated with support cylinder 28 is closed, and is connected to branch this moment and holds round
Belt 30 on the upside of 28 outer wall of column also will appear the winding to support cylinder 28, wherein connecting in the rotation for being supported cylinder 28
It connects the spring 33 in 30 bottom of belt pulled, elastic force recoil must be will appear, the length that shoulder belt ontology 12 can be pulled out
Degree is shunk, and has reached the fixation to people's shoulder, is equivalent to the effect of safety belt.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.In the absence of more restrictions, the element limited by sentence " including a reference structure ", is not arranged
Except there is also other identical elements in the process, method, article or apparatus that includes the element.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
A variety of variations, modification, replacement can be carried out to these embodiments without departing from the principles and spirit of the present invention by understanding
And modification, the scope of the present invention is defined by the appended.
Claims (4)
1. a kind of single hovering flight pedal, including hovering flight device（1）, it is characterised in that：The hovering flight device（1）Just
The left and right sides is fixedly connected to shoulder belt placer on face（2）, the shoulder belt placer（2）Front on be fixedly connected with shoulder belt
Ontology（12）, the shoulder belt placer（2）Bottom be fixedly connected with fixed link（13）, the fixed link（13）Outer wall on the downside of
It is connected with sleeve（17）, the sleeve（17）Outer wall on be fixedly connected with screw thread hand handle（14）, the hovering flight device
（1）The left and right sides be fixedly connected to wind speed round control panel（3）, the wind speed round control panel（3）Front on
It is fixedly connected with rotational speed regulation panel（4）, the wind speed round control panel（3）Outer wall on be fixedly connected with conducting wire（5）, institute
State conducting wire（5）Top be provided with wind wheel ontology（8）, the wind wheel ontology（8）Bottom interior wall on be fixedly connected with closing disk
（22）, the wind wheel ontology（8）Top face among position be fixedly connected with large-scale living silk nut（7）, the wind wheel ontology
（8）Top exterior walls on be fixedly connected with connection component（10）, the connection component（10）Top left side be fixedly connected with spiral shell
Bolt（9）, the bolt（9）Bottom run through connection component（10）Top left side, and with wind wheel ontology（8）Top left side it is solid
Fixed connection, the hovering flight device（1）Front upside be fixedly connected with air bag placer（11）；
The large-scale silk bolt living（7）Left and right sides inner wall on be fixedly connected to long geosynclinal block（25）, the long geosynclinal block（25）
Slot in be connected with block（24）, two blocks（24）Between be fixedly connected with rotation column（26）, the rotation column
（26）Bottom be fixedly connected with rotation control motor（27）, the rotation column（26）Outer wall on be fixedly connected with propeller
Blade（23）, the rotation control motor（27）Bottom and conducting wire（5）Top be fixedly connected, the propeller blade（23）
It cooperates for four groups.
2. a kind of single hovering flight pedal according to claim 1, it is characterised in that：The shoulder belt placer（2）'s
Support cylinder is fixedly connected in bottom interior wall（28）, the shoulder belt placer（2）Top and bottom inner wall on be groove
Shape, the support cylinder（28）Top and bottom be respectively positioned in groove, the support cylinder（28）Outer wall on be socketed with turn
Cylinder（29）, the rotating cylinder（29）Outer wall on be fixedly connected with belt（30）, the belt（30）Bottom be fixed with stationary plane
Plate（32）, the fixed panel（32）Bottom be fixedly connected with spring（33）, the spring（33）With fixed panel（32）?
Positioned at holder（31）It is interior, the spring（33）Bottom be planar, the spring（33）Bottom and holder（31）'s
The welding of right side inner wall.
3. a kind of single hovering flight pedal according to claim 1, it is characterised in that：The hovering flight device（1）'s
Left and right sides outer wall and wind wheel ontology（8）Outside be fixedly connected with wide head grafting block（6）, the width head grafting block（6）Top
Portion is wide head, and wide head grafting block（6）Bottom be welded on wind wheel ontology（8）Right side inner wall on.
4. a kind of single hovering flight pedal according to claim 4, it is characterised in that：The fixed panel（32）In
Between position be circular hole, the block（24）With long geosynclinal block（25）Size is adapted, the block（24）With long geosynclinal block（25）?
It is discoid.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810638309.1A CN108860603A (en) | 2018-06-20 | 2018-06-20 | A kind of single hovering flight pedal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810638309.1A CN108860603A (en) | 2018-06-20 | 2018-06-20 | A kind of single hovering flight pedal |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108860603A true CN108860603A (en) | 2018-11-23 |
Family
ID=64339997
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810638309.1A Withdrawn CN108860603A (en) | 2018-06-20 | 2018-06-20 | A kind of single hovering flight pedal |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108860603A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4302791A1 (en) * | 1993-02-02 | 1994-08-04 | Juergen Schuster | Portable helicopter attachment for lifting single person |
| GB2419122A (en) * | 2004-10-05 | 2006-04-19 | Alexander Stuart Hardy | Vertical take-off and landing aircraft |
| CN101108654A (en) * | 2007-06-27 | 2008-01-23 | 东莞市龙行航空科技有限公司 | Double-duct single-person vertical take-off and landing aircraft |
| CN101341050A (en) * | 2005-12-19 | 2009-01-07 | 奥托立夫开发公司 | Seat belt retractor with controlled belt extension force limiting |
| RU2401772C1 (en) * | 2009-08-31 | 2010-10-20 | Юлия Алексеевна Щепочкина | Flying belt |
| CN102501969A (en) * | 2011-12-13 | 2012-06-20 | 北京君研院科技有限公司 | One-man flight vehicle capable of jetting at points of rotor blades |
| DE102011082719A1 (en) * | 2011-09-14 | 2013-03-14 | Antun Sljivac | Ultralight helicopter i.e. one-man helicopter, for transporting persons from traffic jam caused by motor vehicles in heavy traffic, has control unit for controlling position of coaxial rotors and rotor blades and regulating engine power |
| CN206381621U (en) * | 2016-11-28 | 2017-08-08 | 广东美嘉欣创新科技股份有限公司 | A kind of propeller set of unmanned plane |
-
2018
- 2018-06-20 CN CN201810638309.1A patent/CN108860603A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4302791A1 (en) * | 1993-02-02 | 1994-08-04 | Juergen Schuster | Portable helicopter attachment for lifting single person |
| GB2419122A (en) * | 2004-10-05 | 2006-04-19 | Alexander Stuart Hardy | Vertical take-off and landing aircraft |
| CN101341050A (en) * | 2005-12-19 | 2009-01-07 | 奥托立夫开发公司 | Seat belt retractor with controlled belt extension force limiting |
| CN101108654A (en) * | 2007-06-27 | 2008-01-23 | 东莞市龙行航空科技有限公司 | Double-duct single-person vertical take-off and landing aircraft |
| RU2401772C1 (en) * | 2009-08-31 | 2010-10-20 | Юлия Алексеевна Щепочкина | Flying belt |
| DE102011082719A1 (en) * | 2011-09-14 | 2013-03-14 | Antun Sljivac | Ultralight helicopter i.e. one-man helicopter, for transporting persons from traffic jam caused by motor vehicles in heavy traffic, has control unit for controlling position of coaxial rotors and rotor blades and regulating engine power |
| CN102501969A (en) * | 2011-12-13 | 2012-06-20 | 北京君研院科技有限公司 | One-man flight vehicle capable of jetting at points of rotor blades |
| CN206381621U (en) * | 2016-11-28 | 2017-08-08 | 广东美嘉欣创新科技股份有限公司 | A kind of propeller set of unmanned plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN206546745U (en) | A kind of wire twisting equipment of cable | |
| CN206536499U (en) | A kind of robot is grabbed | |
| CN113086173B (en) | Multifunctional UAV Landing Gear and UAV | |
| CN113785692A (en) | A pineapple picker, picking method and picking robot integrating clipping and cutting | |
| CN108423153A (en) | Modularized micro unmanned plane | |
| CN208360500U (en) | A kind of hovering flight pedal | |
| CN107831044A (en) | A kind of high unmanned plane of security performance for water sampling | |
| CN102779438A (en) | Flight simulated mechanical execution system simulating full-motion of airplane | |
| CN108860603A (en) | A kind of single hovering flight pedal | |
| CN203094441U (en) | Improved four-rotor aircraft | |
| CN108583885A (en) | A kind of hovering flight pedal | |
| CN109436322B (en) | Small fruit picking unmanned aerial vehicle and working method thereof | |
| CN103803069A (en) | Bevel-gear-transmission four-rotor-wing aircraft | |
| CN208602703U (en) | A kind of geological disaster real time monitoring uses unmanned plane | |
| CN204433056U (en) | Buoyancy is auxiliary rises unmanned plane | |
| CN105852148A (en) | Quick chestnut sheller | |
| CN206674545U (en) | A kind of end effector mechanism of seed ball picking robot | |
| CN107516451A (en) | Fixed-wing UAV Intelligent flight training system | |
| CN112586191A (en) | Semi-automatic pine nut picking machine based on self-balancing vibration superposition excitation | |
| CN106904055A (en) | A kind of rotorcycle | |
| CN216970001U (en) | An extended-range composite fixed-wing unmanned aerial vehicle | |
| CN102673785A (en) | Flapping-wing aircraft | |
| CN206766345U (en) | A kind of four rotor wing unmanned aerial vehicles with crawl function | |
| CN209852590U (en) | A UAV flight grabbing system | |
| CN205076037U (en) | Multi -rotor -wing aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181123 |
|
| WW01 | Invention patent application withdrawn after publication |