US20020092949A1 - Anti-submarine warfare uav and method of use thereof - Google Patents
Anti-submarine warfare uav and method of use thereof Download PDFInfo
- Publication number
- US20020092949A1 US20020092949A1 US09/761,076 US76107601A US2002092949A1 US 20020092949 A1 US20020092949 A1 US 20020092949A1 US 76107601 A US76107601 A US 76107601A US 2002092949 A1 US2002092949 A1 US 2002092949A1
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- aircraft
- fuselage
- submarine
- detecting equipment
- body portion
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/005—Flying-boats; Seaplanes with propellers, rudders or brakes acting in the water
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/08—Air-cushion wherein the cushion is created during forward movement of the vehicle by ram effect
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/20—Vertical take-off and landing [VTOL] aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
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- 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
- B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
- B64U30/296—Rotors with variable spatial positions relative to the UAV body
- B64U30/297—Tilting rotors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/12—Propulsion using turbine engines, e.g. turbojets or turbofans
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/13—Propulsion using external fans or propellers
- B64U50/14—Propulsion using external fans or propellers ducted or shrouded
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/15—Propulsion using combustion exhausts other than turbojets or turbofans, e.g. using rockets, ramjets, scramjets or pulse-reactors
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U60/00—Undercarriages
- B64U60/10—Undercarriages specially adapted for use on water
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
- B64U70/60—Take-off or landing of UAVs from a runway using their own power
-
- 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
-
- 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
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
- B64U2101/18—UAVs specially adapted for particular uses or applications for conventional or electronic warfare for dropping bombs; for firing ammunition
-
- 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]
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- 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
Definitions
- Amphibious aircraft both manned and unmanned have been well known in the prior art.
- Such aircraft have sponson structure allowing the craft to take off and land in water, as well as engine apparatus carried on the wing at a position substantially above the surface of the water so that neither the water or the spray interferes with the generation of propulsion by the engine apparatus.
- Another object of the present invention is to provide a novel ASW apparatus including a mobile craft capable of flight and an enemy locating and identifying capability deployable at predetermined positions so that naval battle groups can be protected.
- FIG. 1 the sole figure in the drawings, depicts the ASW unmanned airborne vehicle of the present invention.
- the UA V 100 is shown to feature a widely spaced catamaran configuration designed for stability in rough seas.
- the UAV as shown includes a fuselage 20 having a nose portion 30 , a tail portion 40 , lateral platforms 52 , 54 and sponsons 62 , 64 disposed outwardly of the lateral platforms and connected to the fuselage 20 by the lateral platforms 52 , 54 , respectively.
- the wing ailerons 43 and body flaps 41 would be fully deployed downward and, along with the sponsons, the design would provide a closed cell beneath the wing.
- the tail portion 40 includes a rear deck 42 extending rearwardly of the body portion 20 and a rear stabilizer 44 supported atop and connecting parallel, spaced apart, rudder structures 46 , 48 .
- the lateral platforms 52 , 54 are substantially horizontally disposed.
- Torpedo bays 66 , 68 are housed inside the sponsons and are arranged substantially in alignment with the longitudinal axis of the fuselage and are deployable upon detection of hostile or enemy submarines, related craft and/or objects.
- the fuselage houses propulsion means, preferably dual turbo fan engines 22 , 24 and includes intake inlets arranged forwardly of the propulsion means.
- the intake inlets are provided with covers (not shown) that close the inlets to keep water out of the engines when the craft is sitting in the water.
- the fuselage is also designed to house such ASW equipment as one or more dipping sonar devices, an IR sensor, a low light level television, multi-mode radar, a towed magnetic anomaly detector 71 , and sonobuoys 72 .
- the aircraft 100 would then take off and move ahead another 100 nm or to some other predetermined site or location, deploy a second set of sonobuoys, land in the water and repeat the monitoring for another 4 hours.
- the on board batteries would be recharged during the flight, and during the day from solar panels (not shown) located on the upper surface of the aircraft body and horizontal tail.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
Abstract
An anti-submarine warfare system includes an unmanned “sea-sitting” aircraft housing submarine detecting equipment, the aircraft including a body portion having a catamaran configuration adapted for stably supporting the body portion when sitting in water, the body portion including a fuselage and laterally disposed sponsons connected to the fuselage via platforms, and submarine detecting equipment housed within the fuselage and adapted to be electronically linked to sonobuoys disposed in adjacent water locations.
Description
- 1. Field of the Invention
- The present invention relates to unmanned airborne vehicles (UAVs), and more particularly to unmanned airborne vehicles designed for use in calm and rough seas while conducting anti-submarine detection exercises.
- 2. Description of the Related Art
- Amphibious aircraft, both manned and unmanned, have been well known in the prior art. Typically, such aircraft have sponson structure allowing the craft to take off and land in water, as well as engine apparatus carried on the wing at a position substantially above the surface of the water so that neither the water or the spray interferes with the generation of propulsion by the engine apparatus.
- It is also well-known to use sonar devices for the purpose of locating and identifying structures beneath the surface of water, and especially for the purpose of locating and identifying enemy or even hidden underwater vehicles or objects.
- However, as yet, no one has combined the two concepts in a single, unmanned, propulsive device, such as an aircraft.
- Against this background of known technology, the applicants have developed a novel system including an unmanned amphibious craft housing propulsive engines and armament, and being designed for deploying a plurality of sonobuoys, thereby creating a detecting field. The craft then sits on the water to monitor the readings generated by the field of sonobuoys, and if an enemy craft is detected, the anti-submarine armament is released and directed toward the enemy craft.
- It is therfore a principal object of the present invention to provide a novel around-the-clock anti-submarine warfare (ASW) apparatus for providing coverage for a raval battle group using an unmanned airborne vehicle, while overcoming many of the disadvantages and drawbacks of similar submersible systems known in the art.
- Another object of the present invention is to provide a novel ASW apparatus including a mobile craft capable of flight and an enemy locating and identifying capability deployable at predetermined positions so that naval battle groups can be protected.
- Still another object of the invention is to provide an ASW system which includes an unmanned seaplane constituting a floating command station capable of deploying a network of submergible listening devices and then monitoring the network of listening devices in order to determine the possible presence of enemy craft, and in the event that such craft are detected, launching weapons capable of destroying such enemy craft.
- Other objects, advantages and features of the invention will become more apparent, as will equivalent structures which are intended to be covered herein, with the teaching of the principles of the invention in connection with the disclosure of the preferred embodiments thereof in the specification, claims and drawings in which:
- FIG. 1, the sole figure in the drawings, depicts the ASW unmanned airborne vehicle of the present invention.
- The following description is provided to enable any person skilled in the art to make and use the invention and sets forth the best modes contemplated by the inventor of carrying out his invention. Various modifications, however, will remain readily apparent to those skilled in the art, since the generic principles of the present invention have been defined herein specifically to provide an ASW unmanned airborne vehicle housing equipment adapted for detecting enemy craft and objects, while also carrying armament capable of destroying detected enemy craft and objects.
- Unlike prior known systems, which deploy sonobuoys and then monitor their signals from a manned ASW aircraft flying overhead, the system of the present invention monitors the sonobuoys from an unmanned platform sitting quietly on the surface of the water.
- Referring now to the sole Figure of the drawing, the UA V 100 is shown to feature a widely spaced catamaran configuration designed for stability in rough seas. The UAV as shown includes a
fuselage 20 having anose portion 30, atail portion 40, 52, 54 andlateral platforms 62, 64 disposed outwardly of the lateral platforms and connected to thesponsons fuselage 20 by the 52, 54, respectively. During takeoff of thelateral platforms craft 100, thewing ailerons 43 andbody flaps 41 would be fully deployed downward and, along with the sponsons, the design would provide a closed cell beneath the wing. Two propulsive devices located in thefuselage 20 would exhaust beneath the wing pressurizing the closed cell region to help lift the aircraft out of the water during take-off. This concept, called propulsion augmented ram (PAR), reduces the required thrust-to-weight for rough sea takeoff by a factor of 2.5, and helps balance the propulsion system for cruise operation. - The
tail portion 40 includes arear deck 42 extending rearwardly of thebody portion 20 and arear stabilizer 44 supported atop and connecting parallel, spaced apart, 46, 48. Therudder structures 52, 54 are substantially horizontally disposed.lateral platforms 66, 68 are housed inside the sponsons and are arranged substantially in alignment with the longitudinal axis of the fuselage and are deployable upon detection of hostile or enemy submarines, related craft and/or objects. The fuselage houses propulsion means, preferably dualTorpedo bays 22, 24 and includes intake inlets arranged forwardly of the propulsion means. The intake inlets are provided with covers (not shown) that close the inlets to keep water out of the engines when the craft is sitting in the water. It is contemplated that the engines would be shut down and the inlet covers closed prior to landing in the water. The fuselage is also designed to house such ASW equipment as one or more dipping sonar devices, an IR sensor, a low light level television, multi-mode radar, a towedturbo fan engines magnetic anomaly detector 71, andsonobuoys 72. - In operation, the
aircraft 100 would be assigned to and controlled from a host ship in a naval battle group. The aircraft would be deployed from the host ship, either by hoisting the aircraft onto the water or by a VTOL mechanism, such as tilt rotors. The aircraft would cruise out 100-300 nautical miles (nm) ahead of the battle group or to some predetermined site or location in accordance with a mission plan. When the aircraft reaches its target coordinates, it would deploy a sonobuoy pattern and then land in the water, whereupon it would lower its own hydrophone and water environment sensor, and raise an RF antenna via a balloon (for communicating with sonobuoys). After sensing the water environment (e.g., temperature profile, salinity, pressure, etc.), the aircraft would instruct the sonobuoys to lower their hydrophones to optimum depths. The aircraft world be able to move around quietly about the sonobuoy field on battery power at about 4 knots, sensing the water environment and providing sonobuoy field refinement. The aircraft is designed to move about at a higher speed using the onboard APU, but would generate noise that could be detected by submerged (perhaps enemy) submarines. - It is contemplated that the
aircraft 100 will sit and listen for about 4 hours (equivalent to conventional battery life of sonobuoys or longer as battery and/or energy cells or systems become more efficient) while the battle group moves ahead. Equipment in theaircraft 100 will provide a datalink connection with the host ship in the battle group via SATCOM. It is further contemplated that theaircraft 100 will be autonomous during its mission, all the while however, the remote control operator on board the host ship would be monitoring the course of events and have override command capabilities. - The
aircraft 100 would then take off and move ahead another 100 nm or to some other predetermined site or location, deploy a second set of sonobuoys, land in the water and repeat the monitoring for another 4 hours. The on board batteries would be recharged during the flight, and during the day from solar panels (not shown) located on the upper surface of the aircraft body and horizontal tail. - By employing the apparatus of the present invention, many advantages are realized over manned airborne ASW systems. First, fewer ASW platforms are required to provide around-the-clock ASW for the battle group (a “sea-sitting” UAV offers much longer time-on-station than a manned airborne ASW craft). Second, significantly less fuel, maintenance and manpower costs are required. Third, the unmanned ASW aircraft sitting quietly in the water while monitoring sonobuoys is not detectable by nearby submerged submarines (the manned aircraft flying overhead is detectable by submerged submarines). Fourth, A human crew is not at risk during the ASW operation. Fifth, a “sea-sitting” ASW aircraft can continually monitor the sea environment and instruct the sonobuoys to adjust their hydrophones for the optimum depth.
- Those skilled in the art will appreciate that various adoptions and modifications of the invention as described above can be configured without departing from the scope and spirit of the invention. Therefore, it is to be understood that, within the scope of the appended claims, the invention may be practiced other than as specifically described herein.
Claims (11)
1. An unmanned anti-submarine warfare aircraft, comprising:
a body portion having a catamaran configuration adapted for stably supporting said body portion when sitting in water, said body portion including a fuselage and laterally disposed sponsons connected to said fuselage via platforms and
submarine detecting equipment housed within said fuselage and adapted to be linked to sonobuoys disposed in adjacent water locations,
2. The aircraft of claim 1 , wherein said sonobuoys are deployed from said fuselage while said aircraft is airborne over a predetermined target location.
3. The aircraft of claim 2 wherein said sonobuoys are deployed from said fuselage while said aircraft is sitting in the water at a predetermined location.
4. The aircraft of claim 3 , wherein said fuselage further includes propulsion apparatus housed therein, and said sponsons each house torpedo tubes for launching torpedo armament when an enemy submarine or other object is detected.
5. The aircraft of claim 4 , wherein power for said detecting equipment is derived from solar collecting devices supported by said fuselage or said laterally extending platforms.
6. The aircraft of claim 5 , wherein power for said detecting equipment is derived from on board APU and batteries.
7. The aircraft of claim 4 wherein said armament may be deployed upon command from a host ship.
8. The aircraft of claim 4 wherein said detecting equipment may be deployed, activated or deactivated by command from a host ship.
9. The aircraft of claim 4 wherein said aircraft may autonomously activate and deactivate said armament and said detecting equipment
10. An anti-submarine warfare system, comprising:
host ship having a manned control center,
unmanned aircraft housing submarine detecting equipment, said aircraft capable of flying ahead of said host ship to a predetermined location where listening functions are to be performed by said aircraft, and
armament deployable from said unmanned aircraft upon detection of enemy submarines or enemy objects.
11. An anti-submarine warfare system, comprising:
an unmanned “sea-sitting aircraft housing submarine detecting equipment, said aircraft including a body portion having a catamaran configuration adapted for stably supporting said body portion when sitting in water, said body portion including a fuselage and laterally disposed sponsons connected to said fuselage via platforms, and
Submarine-detecting equipment housed within said fuselage and adapted to be electronically linked to sonobuoys disposed in adjacent water locations.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/761,076 US6409122B1 (en) | 2001-01-17 | 2001-01-17 | Anti-submarine warfare UAV and method of use thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/761,076 US6409122B1 (en) | 2001-01-17 | 2001-01-17 | Anti-submarine warfare UAV and method of use thereof |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| US6409122B1 US6409122B1 (en) | 2002-06-25 |
| US20020092949A1 true US20020092949A1 (en) | 2002-07-18 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US09/761,076 Expired - Fee Related US6409122B1 (en) | 2001-01-17 | 2001-01-17 | Anti-submarine warfare UAV and method of use thereof |
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| US20050188828A1 (en) * | 2000-11-30 | 2005-09-01 | Lockheed Martin Corporation | System and method for detecting objects and substances |
| US20060145000A1 (en) * | 2004-10-27 | 2006-07-06 | Robert Hensley | Multi-fuselage aircraft |
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| US20090121071A1 (en) * | 2007-11-12 | 2009-05-14 | Pik Wan Chan | Flying wing boat |
| WO2012039810A1 (en) * | 2010-06-29 | 2012-03-29 | Aerovironment, Inc. | Uav having hermetically sealed modularized compartments and fluid drain ports |
| CN109347597A (en) * | 2018-11-26 | 2019-02-15 | 赵炼 | A kind of underwater sonar inveigles interference unit and its control method |
| RU2743311C1 (en) * | 2020-09-15 | 2021-02-17 | Дмитрий Сергеевич Дуров | Modular x-wing aircraft for arctic rocket aviation complexes |
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| US20050188828A1 (en) * | 2000-11-30 | 2005-09-01 | Lockheed Martin Corporation | System and method for detecting objects and substances |
| US7637196B2 (en) * | 2000-11-30 | 2009-12-29 | Lockheed-Martin Corporation | System and method for detecting objects and substances |
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