CN107380451A - A kind of rotor armed drones - Google Patents
A kind of rotor armed drones Download PDFInfo
- Publication number
- CN107380451A CN107380451A CN201710781422.0A CN201710781422A CN107380451A CN 107380451 A CN107380451 A CN 107380451A CN 201710781422 A CN201710781422 A CN 201710781422A CN 107380451 A CN107380451 A CN 107380451A
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- China
- Prior art keywords
- rotor
- armed drones
- weapon
- rotor armed
- aerial vehicle
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- 238000010304 firing Methods 0.000 claims abstract description 44
- 230000007246 mechanism Effects 0.000 claims abstract description 17
- 230000003019 stabilising effect Effects 0.000 claims abstract description 16
- 238000009527 percussion Methods 0.000 claims description 27
- 230000003139 buffering effect Effects 0.000 claims description 14
- 210000000038 chest Anatomy 0.000 claims description 3
- 238000009434 installation Methods 0.000 claims description 2
- 230000035939 shock Effects 0.000 abstract description 4
- 230000005540 biological transmission Effects 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 4
- 239000000872 buffer Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 230000001360 synchronised effect Effects 0.000 description 3
- 238000011161 development Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/02—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
- H04N23/54—Mounting of pick-up tubes, electronic image sensors, deviation or focusing coils
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a kind of rotor armed drones, the rotor armed drones, including rotor wing unmanned aerial vehicle, sight take aim at system, fire control system, armament systems, ground control station.The rotor wing unmanned aerial vehicle is maneuverability, handling good as weapon platform.It is described sight take aim at system can observe round the clock, accurate ranging, remote data transmission.The fire control system resolves trajectory, commands firing angle adjustment mechanism, manipulates weapon aiming.The armament systems include grenade launcher；Stabilising arrangement is buffered, effectively reduces shock loading；Remote trigger device, it is simple and reliable.The ground control station remotely monitor and manipulation unmanned plane, robot weapon are hit target, effectively protect our shooter's safety.The rotor armed drones of the present invention solve rotor wing unmanned aerial vehicle and carry weapon and manipulate the problem of weapon, have breakthrough meaning.
Description
Technical field
The present invention relates to rotor wing unmanned aerial vehicle field, and in particular to a kind of rotor wing unmanned aerial vehicle for carrying weapon, often carries howitzer
The small arms such as transmitter, rifle.
Background technology
Rotor wing unmanned aerial vehicle possesses landing convenience, maneuverability, is easy to the advantages such as hidden, relative inexpensiveness, melts in the army and the people
Under the national strategy promotion for closing depth development, it is incorporated into and applies to military equipment field and be well worth doing, complies with very much current
With future is unmanned, miniaturization, modularization, fly up the Development of Military Equipment demand come.
With the lifting of rotor wing unmanned aerial vehicle technical merit, rotor wing unmanned aerial vehicle is increasingly capable of acting as weapon platform and carries force
Device, if carrying weapon on rotor wing unmanned aerial vehicle platform, extreme low-altitude Strike blank will be filled up.But due to rotor wing unmanned aerial vehicle task
Small, the lasting endurance of load is weak, resistance to shock loads is poor, and there is presently no the rotor armed drones in real actual combat meaning.
According to rotor wing unmanned aerial vehicle feature, it is adapted to carry small arms, and with reference to Operational Effectiveness of Weapon Equipment and actual demand, preferably howitzer is sent out
Emitter carries weapon as optimal.But rotor wing unmanned aerial vehicle platform carries weapon, also in the presence of some technical bottlenecks, in particular for solution
The certainly problem of impact big, long-range aimed fire of the weapon-shooting to platform.
The content of the invention
It is an object of the invention to provide it is a kind of it is reasonable in design, manipulation is simple, stability is good, reliability is high, firepower is powerful,
Powerful rotor armed drones.
Invention disclosed herein aims to solve the problem that the problem of rotor wing unmanned aerial vehicle carries weapon and manipulation weapon.In embodiment,
Rotor armed drones, including rotor wing unmanned aerial vehicle, sight take aim at the five big main body such as system, fire control system, armament systems, ground control station
Part.
The rotor wing unmanned aerial vehicle includes power supply, flies control module, platform, and power supply and winged control module are arranged on above platform, are put down
Platform upper and lower surface is provided with interface, and platform upper interface is used to install fire control system（The push rod of firing angle adjustment mechanism is through flat
Platform）, platform lower installation sight take aim at system and have interface be used for connect firing angle adjustment mechanism.
System is taken aim in the sight includes white light/infrared camera, laser range finder, image transmitter, white light/infrared camera
Couple with image transmitter.
Preferably, laser range finder, which has, surveys relative distance, the function of relative height differential.
The fire control system includes arming signal receiver, processor, firing angle controller, firing controller, firing angle adjustment
Mechanism, processor and firing angle controller, arming signal receiver, firing controller, firing angle adjustment mechanism angular transducer and
The laser range finder connection for system of taking aim at is seen, firing angle controller is connected with the motor of firing angle adjustment mechanism.
Preferably, the firing angle adjustment mechanism includes motor, worm gear, worm screw, rocking bar, push rod, angular transducer.Penetrate
The motor and Worm and worm-wheel gearing of angle adjusting mechanism are fixed on platform, and motor provides input power to worm screw,
Worm screw promotes worm gear wheel, and a notch is opened in worm gear side, and rocking bar is placed in notch, and rocking bar one end is coaxially fixed with worm gear, rocking bar
The other end is connected by hinge with push rod one end, and push rod other end hinge is connected with buffering top guide bar one end of stabilising arrangement.
The top guide bar other end is connected by hinge with platform, and angular transducer is at this hinge.
Preferably, the information and instruction that the processor reception processing laser range finder, arming signal receiver transmit, under
Firing angle controller and firing controller are arrived up to instruction.
The armament systems include grenade launcher, buffering stabilising arrangement, percussion lock, buffering stabilising arrangement top guide bar one
End is connected to below platform, the push rod of buffering stabilising arrangement top guide bar other end connection firing angle adjustment mechanism, buffers stabilising arrangement
Lower guide rod both ends are connected with the connecting seat on grenade launcher, and top guide bar and lower guide rod are each passed through the guide hole in contiguous block, hit
Transmitting apparatus is arranged in front of grenade launcher trigger, and percussion lock is connected with firing controller.
Preferably, the grenade launcher is equipped with efficient thorax mouth muzzle brake, reduces impulsive force, and ejection direction is right side side,
Unmanned plane during flying safety is not influenceed；Transmitter can be used alone when the grenade launcher does not reside at unmanned aerial vehicle platform；It is described
Two fixed connecting seats are arranged at grenade launcher top, buffer stabilising arrangement for connecting, the grenade launcher trigger is anterior
Percussion lock is installed.
Preferably, the buffering stabilising arrangement includes contiguous block, spring, top guide bar, lower guide rod, and top guide bar adjusts with firing angle
Mechanism connects with platform, and lower guide rod is connected with the connecting seat on grenade launcher, has two pairs of parallel guide holes in contiguous block, above leads
Bar and lower guide rod are each passed through two guide holes in contiguous block, and the size of guide rod and contiguous block guide hole matches, and contiguous block is being led
Freely slidable on bar, the sectional area of guide rod and guide hole is rectangle, is advantageous to limitation grenade launcher and swings, spring housing
In top guide bar and lower guide rod both ends.
Preferably, the percussion lock includes coilgun, percussion thimble, return spring, and coilgun is arranged on immediately ahead of trigger,
Percussion thimble afterbody is placed in coilgun center, and head alignment trigger center, head is curved to prevent from slipping on trigger, multiple
Position spring is placed in the middle part of percussion thimble, percussion thimble is resetted after launching.
The ground control station includes information transceiving device, display, flies control operation device, arming signal transmitter.
Compared with prior art, the present invention has the advantage that is with beneficial effect：The present invention has created a brand-new rotation
Wing armed drones.By installing thorax mouth muzzle brake and buffering stabilising arrangement additional, to flying platform during significantly reducing weapon-shooting
Shock loading；Equipped with white light/infrared function camera, possesses round-the-clock fight capability；Equipped with laser range finder, fire control system
System, can be to target precision strike；, can remotely monitor and manipulation shooting, effectively protection equipped with image transmitter, remote trigger device
Our shooter is safe；There is the grenade launcher of dress face to kill ability, and firepower is powerful, and it is empty to fill up extreme low-altitude Strike technology
In vain.The rotor armed drones of the present invention, topology layout is compact, maneuverability is high, strong applicability, will be on solid assault, mountain
Ground operation, border prevention and control, pull out and a little take by force in battlefield surroundings to be waited using there is breakthrough meaning.
Brief description of the drawings
In order that present disclosure is more likely to be clearly understood, specific embodiment and combination below according to the present invention
Accompanying drawing, the present invention is further illustrated, wherein：
Fig. 1 is schematic diagram above the rotor armed drones general structure of the present invention；
Fig. 2 is schematic diagram below the rotor armed drones general structure of the present invention；
Fig. 3 is the fire control system workflow schematic diagram of the present invention；
Fig. 4 is the firing angle adjustment mechanism and buffering stabilising arrangement structural representation of the present invention；
Fig. 5 is the percussion lock structural representation of the present invention；
Fig. 6 is the ground control station structural representation of the present invention；
Fig. 7 is rotor armed drones' workflow schematic diagram of the present invention.
1- grenade launchers；2- processors；3- power supplys；4- motors；5- flies control module；6- image transmitters；7- platforms；8-
Arming signal receiver；9- firing angle controllers；10- firing controllers；11- white lights/infrared camera；12- laser range finders；
13- worm screws；14- worm gears；15- rocking bars；16- push rods；17- contiguous blocks；18- springs；19- top guide bars；20- lower guide rods；21- angles
Sensor；22- triggers；23- trigger frames；24- fires thimble；25- return springs；26- coilguns；27- displays；28- percussion letters
Number transmitter；29- flies control operation device；30- information transceiving devices.
Embodiment
In order that the purpose, technical scheme and advantage of the embodiment of the present invention are more clearly understood, with reference to attached
The invention will be further described with embodiment for figure.Here, the present invention illustrative examples and illustrate be used for explain this hair
It is bright but not as a limitation of the invention.
As shown in Figure 1 and Figure 2, a kind of rotor armed drones of the present embodiment, it includes rotor wing unmanned aerial vehicle, system is taken aim in sight,
The five big main part such as fire control system, armament systems, ground control station.Platform 7 is the fuselage of unmanned plane, and power supply 3 is whole system
System provides power, flies control module 5 and controls flight path and posture；See take aim at system white light/infrared camera 11 collect target and
Unmanned plane surrounding enviroment feature, and ground control station will send information to by image transmitter 6, laser range finder 12 measures nobody
The distance and difference in height of machine and target, and transfer data to the processor 2 of fire control system；The arming signal of fire control system receives
When device 8 receives ground control station instruction, processor 2 quickly carries out ballistic solution, according to calculation result under firing angle controller 9
Up to instruction, motor 4 is completed firing angle according to the instruction of firing angle controller 9 and adjusted, and after being adjusted in place, processor 2 is controlled to shooting
Device 10 processed assigns shooting instruction；Percussion lock driving grenade launcher 1 fires.
As shown in figure 3, the fire control system workflow of the present embodiment, the arming signal receiver 8 of fire control system receives
During the instruction that ground control station strikes target, the data that processor 2 transmits according to laser range finder 12 quickly carry out ballistic solution,
Instruction is assigned to firing angle controller 9 according to calculation result, motor 4 is according to the instruction of firing angle controller 9, driving firing angle adjustment
Mechanism carries out firing angle adjustment, is adjusted in place rear angular transducer and is reported to processor 2, and simultaneous processor 2 is to firing controller 10
Assign shooting instruction, percussion lock driving grenade launcher percussion.
As shown in figure 4, the firing angle adjustment mechanism of the present embodiment and buffering stabilising arrangement, Liang Ge mechanisms are closely coupled, firing angle
Adjustment mechanism buffers the angle of stabilising arrangement by adjusting, and reaches purpose of the adjustment weapon firing angle so as to run-home.Driving electricity
Machine 4 is received after firing angle controller 9 instructs and started working, and driving worm screw 13 rotates, and worm screw 13 promotes worm gear 14 to rotate, rocking bar 15
With the synchronous rotary of worm gear 14, rocking bar 15 drives push rod 16 to move up and down to adjust the angle of buffering stabilising arrangement, angular transducer
21 are arranged on the junction of platform 7 and top guide bar 19, and the relative angle of guide rod 19 and platform 7 is measured；The stable dress of buffering
Contiguous block 17 in putting connects 20,4 springs 20 of parallel top guide bar 19 and lower guide rod and is attached separately to top guide bar 19 and lower guide rod
20 both ends, the sectional area of top guide bar 19, lower guide rod 20 and the guide hole of contiguous block 17 is rectangle, can thus limit howitzer transmitting
Device 1 swings, when grenade launcher is shot, under recoil effect, and top guide bar 19 and the relative parallel movement of lower guide rod 20, and
Compression spring 18, reduces the shock loading to platform, and back seat recovers stable after in place under the effect of spring 18.
As shown in figure 5, the percussion lock of the present embodiment, employs coilgun transmitting percussion thimble to realize trigger percussion
Scheme, coilgun 26 are fixed on the trigger frame 23 immediately ahead of trigger, and the percussion afterbody of thimble 24 is placed in the center of coilgun 26,
Head alignment trigger 22 center, in semi-surrounding shape, return spring 25 is placed on the percussion afterbody of thimble 24 and the head of coilgun 26
Between, after firing controller 8 is powered to coilgun 26, the transmitting percussion thimble 24 of coilgun 26, percussion thimble 24 promotes trigger 22
Percussion, while return spring 25 is compressed, after firing controller 8 powers off to coilgun 26, effect of the percussion thimble 24 in return spring 25
Under return in coilgun 26, preparation fire next time.
As shown in fig. 6, the ground control station of the present embodiment, fly control operation device 29 assign manipulation unmanned plane during flying track and
The instruction of posture；Information transceiving device 30 sends manipulation instruction to unmanned plane, receives the information that the transmission of graphics transport device comes；Display
Device 27 shows the information transmitted, real-time monitoring objective and unmanned plane surrounding enviroment；Arming signal transmitter 28 is under fire control system
Instructed up to aimed fire, Strike is carried out to target.
As shown in fig. 7, rotor armed drones' workflow of the present embodiment, system discovery target is taken aim in sight, and information is sent out
The information transceiving device 30 of ground control station is sent to, and is shown on display 27, flies control operation device 29 and is controlled to winged under module 5
Up to adjustment unmanned plane during flying posture instruction, when display show flight attitude be adjusted in place after, arming signal transmitter 28 to
Fire control system assigns aimed fire instruction, and the instruction of arming signal transmitter 28 is passed to processor 2 by arming signal receiver 8,
Measurement data is defeated by processor 2 by laser range finder 12 simultaneously, and processor 2 passes through ballistic solution, and finger is assigned to firing angle controller 9
Order, motor are started working after receiving the instruction of firing angle controller 9, and motor drives worm screw 13 to rotate, and worm screw 13 pushes away
Dynamic worm gear 14 rotates, rocking bar 15 and the synchronous rotary of worm gear 14, and rocking bar 15 drives push rod 16 to move up and down to adjust the stable dress of buffering
The angle put, weapon firing angle with buffering stabilising arrangement synchronous adjustment, angular transducer 21 to processor 2 report be adjusted in place after,
Processor 2 assigns jet instruction to firing controller 10, and after firing controller 10 is powered to coilgun 26, the transmitting of coilgun 26 is hit
Thimble 24 is sent out, percussion thimble 24 promotes trigger 22 to fire, while compresses return spring 25, and firing controller 10 powers off to coilgun 26
Afterwards, percussion thimble 24 is returned in the presence of return spring 25 in coilgun 26, is carried out percussion next time and is prepared.
Described above is only the preferred embodiment of the present invention, and protection scope of the present invention is not limited merely to above-mentioned implementation
Example, all technical schemes belonged under thinking of the present invention belong to protection scope of the present invention.It should be pointed out that the present invention is not being departed from
Some improvements and modifications under principle also should be regarded as within protection scope of the present invention.
Claims (9)
1. a kind of rotor armed drones, it is characterised in that the rotor armed drones include rotor wing unmanned aerial vehicle, sight is taken aim at and is
System, fire control system, armament systems, ground control station, the unmanned aerial vehicle platform upper and lower surface are provided with interface, are respectively used to installation fire
System, armament systems are taken aim in control system, sight.
2. a kind of rotor armed drones according to claim 1, it is characterised in that system is taken aim in the sight includes white light/red
Outer camera, laser range finder, image transmitter.
A kind of 3. rotor armed drones according to claim 2, it is characterised in that the fire control system include processor,
Firing angle controller, arming signal receiver, firing angle adjustment mechanism, firing controller.
4. a kind of rotor armed drones according to claim 3, it is characterised in that the firing angle adjustment mechanism includes driving
Dynamic motor, worm gear, worm screw, rocking bar, push rod, angular transducer.
5. a kind of rotor armed drones according to claim 4, it is characterised in that the armament systems are sent out including howitzer
Emitter, buffering stabilising arrangement, percussion lock.
6. a kind of rotor armed drones according to claim 5, it is characterised in that the grenade launcher installs thorax mouth
Muzzle brake.
7. a kind of rotor armed drones according to claim 6, it is characterised in that the buffering stabilising arrangement includes connecting
Connect block, spring, top guide bar, lower guide rod.
A kind of 8. rotor armed drones according to claim 7, it is characterised in that the percussion lock include coilgun,
Fire thimble, return spring.
9. a kind of rotor armed drones according to claim 8, it is characterised in that the ground control station includes information
R-T unit, display, fly control operation device, arming signal transmitter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710781422.0A CN107380451A (en) | 2017-09-01 | 2017-09-01 | A kind of rotor armed drones |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710781422.0A CN107380451A (en) | 2017-09-01 | 2017-09-01 | A kind of rotor armed drones |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107380451A true CN107380451A (en) | 2017-11-24 |
Family
ID=60347663
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710781422.0A Pending CN107380451A (en) | 2017-09-01 | 2017-09-01 | A kind of rotor armed drones |
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| Country | Link |
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| CN (1) | CN107380451A (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108327897A (en) * | 2018-03-09 | 2018-07-27 | 深圳市轻准科技有限公司 | Equip with arms unmanned helicopter |
| CN108341060A (en) * | 2018-04-17 | 2018-07-31 | 深圳市轻准科技有限公司 | Deflectable transmitting ammunition unmanned plane |
| CN108482680A (en) * | 2018-05-07 | 2018-09-04 | 辽宁力德航空科技有限公司 | Unmanned plane carry breaks first gun apparatus |
| CN108545205A (en) * | 2018-03-16 | 2018-09-18 | 清远市巨劲科技有限公司 | A kind of unmanned plane camera mounting support |
| CN108945462A (en) * | 2018-06-11 | 2018-12-07 | 易瓦特科技股份公司 | Power load-bearing emitter for unmanned plane |
| CN109665104A (en) * | 2018-12-18 | 2019-04-23 | 哈瓦国际航空技术（深圳）有限公司 | A kind of ejecting gun and unmanned plane |
| CN110525661A (en) * | 2019-09-11 | 2019-12-03 | 中航技进出口有限责任公司 | A kind of trigger driving and position-limit mechanism for unmanned plane carry machine gun |
| CN113428365A (en) * | 2021-07-22 | 2021-09-24 | 成都浩孚科技有限公司 | Unmanned aerial vehicle firearms carry structure |
| CN113716050A (en) * | 2021-09-26 | 2021-11-30 | 湖南数军物联网科技有限公司 | Automatic shooting unmanned aerial vehicle and unmanned on duty system |
| CN114910919A (en) * | 2022-04-20 | 2022-08-16 | 亿慧云智能科技（深圳）股份有限公司 | Use of low-light-level night vision device and target positioning method and device |
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| CN106477047A (en) * | 2016-11-23 | 2017-03-08 | 深圳市轻准科技有限公司 | A kind of aerial howitzer launch craft |
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| US2426744A (en) * | 1942-01-23 | 1947-09-02 | Bendix Aviat Corp | Automatic gun compensator |
| US20140150631A1 (en) * | 2008-11-12 | 2014-06-05 | Alliant Techsystems Inc. | Unmanned aerial vehicle weapon adapter |
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Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108327897A (en) * | 2018-03-09 | 2018-07-27 | 深圳市轻准科技有限公司 | Equip with arms unmanned helicopter |
| CN108545205A (en) * | 2018-03-16 | 2018-09-18 | 清远市巨劲科技有限公司 | A kind of unmanned plane camera mounting support |
| CN108341060A (en) * | 2018-04-17 | 2018-07-31 | 深圳市轻准科技有限公司 | Deflectable transmitting ammunition unmanned plane |
| CN108482680A (en) * | 2018-05-07 | 2018-09-04 | 辽宁力德航空科技有限公司 | Unmanned plane carry breaks first gun apparatus |
| CN108945462A (en) * | 2018-06-11 | 2018-12-07 | 易瓦特科技股份公司 | Power load-bearing emitter for unmanned plane |
| CN108945462B (en) * | 2018-06-11 | 2021-05-28 | 易瓦特科技股份公司 | A power bearing emitter for unmanned aerial vehicle |
| CN109665104A (en) * | 2018-12-18 | 2019-04-23 | 哈瓦国际航空技术（深圳）有限公司 | A kind of ejecting gun and unmanned plane |
| CN110525661A (en) * | 2019-09-11 | 2019-12-03 | 中航技进出口有限责任公司 | A kind of trigger driving and position-limit mechanism for unmanned plane carry machine gun |
| CN113428365A (en) * | 2021-07-22 | 2021-09-24 | 成都浩孚科技有限公司 | Unmanned aerial vehicle firearms carry structure |
| CN113716050A (en) * | 2021-09-26 | 2021-11-30 | 湖南数军物联网科技有限公司 | Automatic shooting unmanned aerial vehicle and unmanned on duty system |
| CN114910919A (en) * | 2022-04-20 | 2022-08-16 | 亿慧云智能科技（深圳）股份有限公司 | Use of low-light-level night vision device and target positioning method and device |
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Application publication date: 20171124 |