CN107543449A - A kind of rotor armed drones for carrying automatic grenade launcher - Google Patents
A kind of rotor armed drones for carrying automatic grenade launcher Download PDFInfo
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- CN107543449A CN107543449A CN201710829473.6A CN201710829473A CN107543449A CN 107543449 A CN107543449 A CN 107543449A CN 201710829473 A CN201710829473 A CN 201710829473A CN 107543449 A CN107543449 A CN 107543449A
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- grenade launcher
- automatic grenade
- rotor
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- aerial vehicle
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Abstract
The invention discloses a kind of rotor armed drones for carrying automatic grenade launcher, belong to rotor wing unmanned aerial vehicle and automatic grenade launcher application field.The rotor armed drones of automatic grenade launcher are carried, including close coupled type oil electric mixed dynamic unmanned plane, sight take aim at system, fire control module, automatic grenade launcher, remote trigger device.Using rotary engine and the unmanned aerial vehicle platform of the double main rotors of close coupled type, noise is small, compact-sized, hovering performance is good, continuation of the journey and lifting capacity are stronger.The grenade launcher recoil of carrying is small, by guide rod spring damping, further reduces the impact to unmanned aerial vehicle platform.System is taken aim in sight and fire control module preferably meets aimed fire demand of the grenade launcher in unmanned aerial vehicle platform.
Description
Technical field
The present invention relates to rotor wing unmanned aerial vehicle and automatic grenade launcher application field, and in particular to rotor wing unmanned aerial vehicle is as flat
Platform carries automatic grenade launcher.
Background technology
Rotor wing unmanned aerial vehicle have the characteristics that landing convenience, maneuverability, can hovering, apply to military equipment field will
With stronger penetration ability.But current electronic rotor wing unmanned aerial vehicle is constrained by battery, and endurance is short, voyage is limited, lifting capacity has
Limit；Fuel power rotor wing unmanned aerial vehicle, overcomes that electronic rotor wing unmanned aerial vehicle endurance is short, voyage is limited, load-carrying energy to a certain extent
The weakness of power, but the shortcomings of volume is big, noise is big be present, disguise is reduced, it is still inadequate as weapon carrying platform.Rotor
The development of armed drones, unmanned plane is on the one hand limited by, is on the other hand subject to armament systems.Carried Weapon Combat prestige
Power is too small, and the meaning of carrying is with regard to little；The weapon power carried is big, also big to the shock loading of unmanned aerial vehicle platform, it is desirable to
It is higher.For this reason, it may be necessary to can be within tolerance range in rotor wing unmanned aerial vehicle, considering Operational Effectiveness of Weapon Equipment and actual fight needs
Ask to determine the weaponry of rotor wing unmanned aerial vehicle carrying.By Comprehensive Comparison small arms equipment power, effective range and
The indexs such as setback-impact load, find automatic grenade launcher than the conveniently weapon as rotor wing unmanned aerial vehicle carrying.But rotor
Unmanned aerial vehicle platform carries automatic grenade launcher, also in the presence of some technical bottlenecks, is shot in particular for solving grenade launcher
When to unmanned plane impact it is larger, aimed fire is more difficult the problem of.Rotor wing unmanned aerial vehicle is in order to more preferably meet to carry grenade launcher
Demand, it is necessary to the advantages of comprehensive electronic and fuel power rotor wing unmanned aerial vehicle, develop new long endurance, load-carrying is big, noise is small,
The good rotor wing unmanned aerial vehicle of hoverning stability.Both above-mentioned science are integrated into a kind of rotor for carrying automatic grenade launcher to equip with arms
Unmanned plane, there is highly important value and significance.
The content of the invention
Invention disclosed herein is intended to build a kind of rotor armed drones for carrying automatic grenade launcher, mainly solves
Carry capability problemses and the automatic grenade launcher for improving rotor wing unmanned aerial vehicle manipulate problem in the weapon of unmanned aerial vehicle platform.One kind is taken
The rotor armed drones of automatic grenade launcher are carried, including close coupled type oil electric mixed dynamic unmanned plane, sight take aim at system, fire control mould
Block, automatic grenade launcher, remote trigger device.
The close coupled type oil electric mixed dynamic unmanned plane, preferably fuel oil rotary engine.
System is taken aim in the sight includes electric platform, camera, rangefinder, navigation position instrument.Camera and rangefinder installation
On electric platform, preferable camera has white light, infrared function simultaneously；Preferable rangefinder, which has, surveys relative distance, phase
To the function of difference in height, navigation position instrument monitors unmanned plane parameter in real time.
The fire control module includes processor, sighting angle control device.Processor and rangefinder, navigation position instrument, take aim at
Quasi- angle controller is connected.The sighting angle control device includes motor, curved surface turbine, enveloping worm, guide rod and fixation
Seat.
The guide rod phase that the automatic grenade launcher passes through connection component and the sighting angle control device of unmanned aerial vehicle platform
Even, and shock-absorbing spring is added at guide rod both ends.
Preferably, automatic grenade launcher is mounted with efficient muzzle brake, employs the buffering method of body of a gun short recoil, recoil
Impact relatively small.
Preferably, remote trigger device uses coilgun.
Compared with prior art, the present invention has the advantage that is with beneficial effect：The present invention has created a kind of carry automatically
The rotor armed drones of grenade launcher.Using the unmanned aerial vehicle platform of the double main rotors of rotary engine and close coupled type, noise is small,
It is compact-sized, hovering performance it is good, continuation of the journey and lifting capacity it is stronger.The grenade launcher recoil of carrying is small, is subtracted by guide rod spring
Shake, further reduce the impact to unmanned aerial vehicle platform.System is taken aim in sight and fire control module preferably meets grenade launcher in nothing
The aimed fire demand of people's machine platform.
Brief description of the drawings
A kind of rotor armed drones' general illustrations for carrying automatic grenade launcher of Fig. 1；
A kind of rotor armed drones' bottom schematic views for carrying automatic grenade launcher of Fig. 2.
Embodiment
To describe the technology contents of the present invention, construction feature, the objects and the effects in detail, below in conjunction with embodiment
And accompanying drawing is coordinated to be explained in detail.
As shown in Figure 1 and Figure 2, a kind of rotor armed drones for carrying automatic grenade launcher, including close coupled type oil electricity are mixed
Power unmanned plane is closed, sees and takes aim at system, fire control module, automatic grenade launcher.
The close coupled type oil electric mixed dynamic unmanned plane, preferably fuel oil rotary engine 4.The power of rotary engine 4 is steady,
With small vibration, coaxial rotor hoverning stability is good.
System is taken aim in the sight includes electric platform 11, camera 13, rangefinder 12, navigation position instrument 5, camera 13 and survey
Distance meter 12 is arranged on electric platform, and preferable camera 13 has white light, infrared function simultaneously；Preferable rangefinder 12 has
Relative distance, the function of relative height differential are surveyed, navigation position instrument 5 monitors unmanned plane parameter in real time.
The fire control module includes processor 6, sighting angle control device.Processor 6 and rangefinder 12, navigation position instrument
5th, sighting angle control device is connected.Processor 6 receives the distance, difference in height, motion that rangefinder 12 and navigation position instrument 5 transmit
The parameters such as speed calculate angle of emergence parameter, and will instruct the motor 1 for passing to sighting angle control device.
The sighting angle control device includes motor 1, curved surface turbine 2, enveloping worm 3, guide rod 7 and fixed seat 8.Guide rod
7 one end hinges are connected with fixed seat 8, and the other end is connected with curved surface turbine 2, and enveloping worm 3 matches with curved surface turbine 2.When
When firing angle instruction is passed to motor 1 by processor 6, motor 1 drives enveloping worm 3, and enveloping worm 3 drives curved surface turbine 2 to move,
Corresponding adjustment occurs for the angle of guide rod 7, so as to control the shooting angle of weapon.
The automatic grenade launcher 14 passes through connection component and the guide rod 7 of the sighting angle control device of unmanned aerial vehicle platform
It is connected, and shock-absorbing spring 9 is added at the both ends of guide rod 7, setback-impact is further reduced while firing angle is adjusted.
The remote trigger device uses coilgun 10.Coilgun 10 is arranged on immediately ahead of trigger, and percussion thimble afterbody is put
In coilgun center, head alignment trigger center, head is curved to prevent from slipping on trigger, and return spring is placed on percussion top
In the middle part of pin, make percussion thimble being capable of Rapid reset after launching.
This rotor armed drones possess compact-sized, total arrangement is reasonable, platform stabilization is good, run-home is quick etc.
Advantage.
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 (8)
1. a kind of rotor armed drones for carrying automatic grenade launcher, it is characterised in that including close coupled type oil electric mixed dynamic
System, fire control module, automatic grenade launcher, remote trigger device are taken aim in unmanned plane, sight.
A kind of 2. rotor armed drones for carrying automatic grenade launcher according to claim 1, it is characterised in that institute
State close coupled type oil electric mixed dynamic unmanned plane, preferably fuel oil rotary engine.
A kind of 3. rotor armed drones for carrying automatic grenade launcher according to claim 2, it is characterised in that institute
State sight take aim at system include electric platform, camera, rangefinder, navigation position instrument, camera and rangefinder are arranged on electric platform
On.
A kind of 4. rotor armed drones for carrying automatic grenade launcher according to claim 3, it is characterised in that institute
Stating fire control module includes processor, sighting angle control device, and processor controls with rangefinder, navigation position instrument, sighting angle
Device is connected.
A kind of 5. rotor armed drones for carrying automatic grenade launcher according to claim 4, it is characterised in that institute
Stating sighting angle control device includes motor, curved surface turbine, enveloping worm, guide rod and fixed seat.
A kind of 6. rotor armed drones for carrying automatic grenade launcher according to claim 5, it is characterised in that institute
Automatic grenade launcher is stated by connection component with the guide rod of the sighting angle control device of unmanned aerial vehicle platform to be connected, and in guide rod
Both ends add shock-absorbing spring.
7. a kind of rotor armed drones for carrying automatic grenade launcher according to claim 6, it is characterised in that excellent
The automatic grenade launcher of choosing is mounted with efficient muzzle brake, employs the buffering method of the short back seat of the body of a gun, and setback-impact is relatively small.
8. a kind of rotor armed drones for carrying automatic grenade launcher according to claim 7, it is characterised in that excellent
The remote trigger device of choosing uses coilgun.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710829473.6A CN107543449A (en) | 2017-09-14 | 2017-09-14 | A kind of rotor armed drones for carrying automatic grenade launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710829473.6A CN107543449A (en) | 2017-09-14 | 2017-09-14 | A kind of rotor armed drones for carrying automatic grenade launcher |
Publications (1)
| Publication Number | Publication Date |
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| CN107543449A true CN107543449A (en) | 2018-01-05 |
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| CN201710829473.6A Pending CN107543449A (en) | 2017-09-14 | 2017-09-14 | A kind of rotor armed drones for carrying automatic grenade launcher |
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Cited By (6)
| 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 |
| CN108945493A (en) * | 2018-09-29 | 2018-12-07 | 中国人民解放军陆军工程大学 | Low-backseat mounting platform of small unmanned aerial vehicle |
| CN109464766A (en) * | 2018-09-14 | 2019-03-15 | 广州市华科尔科技股份有限公司 | A kind of fire-fighting method of fire-fighting 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 |
| CN110382993A (en) * | 2018-04-28 | 2019-10-25 | 深圳市大疆创新科技有限公司 | Ammunition booster structure, gun post and the unmanned plane of gun post |
| CN111928733A (en) * | 2020-07-24 | 2020-11-13 | 北斗安泽防务科技有限公司 | Horizontally shooting type grenade launcher |
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| CN203558208U (en) * | 2013-05-10 | 2014-04-23 | 刘鹏 | Rotor craft capable of carrying weapon delivery mechanism |
| CN204473131U (en) * | 2014-12-22 | 2015-07-15 | 吉林威和航空科技有限公司 | The many rotor wing unmanned aerial vehicles of a kind of oil electric mixed dynamic |
| CN105539828A (en) * | 2015-12-08 | 2016-05-04 | 陈蜀乔 | Petrol-electric hybrid multi-rotor aerial vehicle capable of self electricity generation |
| CN205345332U (en) * | 2016-01-22 | 2016-06-29 | 江苏数字鹰科技发展有限公司 | Police uses multi -functional unmanned aerial vehicle |
| CN205499385U (en) * | 2016-02-14 | 2016-08-24 | 普宙飞行器科技（深圳）有限公司 | Oil -electricity hybrid vehicle unmanned aerial vehicle |
| 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 |
| CN107021224A (en) * | 2017-04-28 | 2017-08-08 | 深圳市轻准科技有限公司 | Hang down and throw howitzer unmanned plane |
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| CN203558208U (en) * | 2013-05-10 | 2014-04-23 | 刘鹏 | Rotor craft capable of carrying weapon delivery mechanism |
| CN204473131U (en) * | 2014-12-22 | 2015-07-15 | 吉林威和航空科技有限公司 | The many rotor wing unmanned aerial vehicles of a kind of oil electric mixed dynamic |
| CN105539828A (en) * | 2015-12-08 | 2016-05-04 | 陈蜀乔 | Petrol-electric hybrid multi-rotor aerial vehicle capable of self electricity generation |
| CN205345332U (en) * | 2016-01-22 | 2016-06-29 | 江苏数字鹰科技发展有限公司 | Police uses multi -functional unmanned aerial vehicle |
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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 |
| CN107021224A (en) * | 2017-04-28 | 2017-08-08 | 深圳市轻准科技有限公司 | Hang down and throw howitzer unmanned plane |
Cited By (7)
| 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 |
| CN110382993A (en) * | 2018-04-28 | 2019-10-25 | 深圳市大疆创新科技有限公司 | Ammunition booster structure, gun post and the unmanned plane of gun post |
| CN109464766A (en) * | 2018-09-14 | 2019-03-15 | 广州市华科尔科技股份有限公司 | A kind of fire-fighting method of fire-fighting unmanned plane |
| CN108945493A (en) * | 2018-09-29 | 2018-12-07 | 中国人民解放军陆军工程大学 | Low-backseat mounting platform of small unmanned aerial vehicle |
| CN108945493B (en) * | 2018-09-29 | 2023-10-20 | 中国人民解放军陆军工程大学 | Low squatting and mounting platform of small 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 |
| CN111928733A (en) * | 2020-07-24 | 2020-11-13 | 北斗安泽防务科技有限公司 | Horizontally shooting type grenade launcher |
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Application publication date: 20180105 |
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