CN107588679A - A kind of land and air double-used automatic grenade launcher - Google Patents
A kind of land and air double-used automatic grenade launcher Download PDFInfo
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- CN107588679A CN107588679A CN201711026042.2A CN201711026042A CN107588679A CN 107588679 A CN107588679 A CN 107588679A CN 201711026042 A CN201711026042 A CN 201711026042A CN 107588679 A CN107588679 A CN 107588679A
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- grenade launcher
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Abstract
The invention discloses a kind of land and air double-used automatic grenade launcher, belong to grenade launcher field, and in particular to a kind of be both conveniently carried on unmanned plane uses, and also allows for the automatic grenade launcher used on ground.Land and air double-used automatic grenade launcher, including the body of a gun, muzzle brake, casing, buffer gear, elastic buffering pad, pick up spit of fland Buddhist nun's guide rail, foot stool.Setback-impact during using the measure in efficient muzzle brake, the body of a gun recoil in casing to slow down weapon-shooting；The design of pick up spit of fland Buddhist nun's guide rail facilitates weapon to carry additionally functional part and UAV flight；The connection of foot stool and casing uses slot mechanism, solid and reliable, easy to loading and unloading, and foot stool is dismantled in UAV flight, is advantageous to lift unmanned plane payload weight.
Description
Technical field
The present invention relates to grenade launcher field, and in particular to a kind of be both conveniently carried on unmanned plane uses, and also allows for
The automatic grenade launcher used on ground.
Background technology
Automatic grenade launcher includes full-automatic grenade launcher and semi-automatic grenade launcher, is a kind of small-sized pomegranate of transmitting
The small arms of bullet, its small volume, firepower are violent, have stronger face lethal power and certain broken first ability, are mainly used in injuring out
Living aim and light armoring target in wealthy area and covered works, and provide fire support for infantry.
Unmanned plane includes fixed-wing unmanned plane, depopulated helicopter and multi-rotor unmanned aerial vehicle.It is more next with the species of unmanned plane
Abundanter, technology is increasingly advanced, and function is stronger and stronger, and application field is more and more wider, and UAV flight's weapon is into battlefield
A kind of trend will be turned into by playing a role.
Using unmanned plane as weapon platform, automatic grenade launcher is because volume weight is small, range power is greatly with congenital excellent
Gesture.Current automatic grenade launcher both domestic and external, the starting point and foothold that they are designed all are that ground uses weapon, are not considered
It is carried to the interface and particular/special requirement of weapon on unmanned plane.It is therefore desirable to according to automatic grenade launcher in unmanned plane and on ground
The different demands that face uses, use can both be carried on unmanned plane by developing, the land and air double-used automatic pomegranate that can be also used on ground
Ball emitter, to fill up technological gap.Impact capacity is limited when by unmanned plane load-carrying ability and bearing weapon-shooting, land sky two
Should be smaller than the transmitter only used on ground with automatic grenade launcher recoil, weight is also lighter, and needs
It is easy to the Interface design of handling..
The content of the invention
It may do a little simplified or omit in this part and the description of the present application summary and denomination of invention, and it is this
Simplify or omit and cannot be used for limiting the scope of the present invention.
In view of existing armed drones' fire control system has above mentioned problem, both conveniently taken it is an object of the invention to provide a kind of
It is downloaded on unmanned plane and uses, also allows for the automatic grenade launcher used on ground.
In order to solve the above-mentioned technical problem, the technical solution adopted by the present invention is：A kind of land and air double-used automatic howitzer transmitting
Device, including the body of a gun, muzzle brake, casing, buffer gear, elastic buffering pad, pick up spit of fland Buddhist nun's guide rail, foot stool.
The body of a gun includes gun barrel, automatic machine, and gun barrel tail end has the equally distributed journal stirrup of two or more, and gun barrel passes through journal stirrup
It is connected with buffer gear and constrains in gun barrel in casing.
The muzzle brake is arranged on gun barrel front end, and muzzle brake center is projectile flight passage, projectile flight passage both sides pair
Claim the powder gases passage for setting some spouts towards side rear.
The installation body of a gun among the casing, support and the constraint body of a gun.
The buffer gear includes guide rod, spring, and guide rod both ends are fixed on casing front portion, and guide rod passes through gun barrel journal stirrup, bullet
Spring is placed on guide rod.Preferably, spring is placed on gun barrel journal stirrup both sides on guide rod.
The elastic buffering pad is arranged between automatic drive end unit and casing.
Pick up spit of fland Buddhist nun's guide rail is arranged on above casing or side.
The foot stool is arranged on casing bottom, is connected for notch.
The present invention also proposes a kind of unmanned plane, and UAV flight grenade launcher described above, unmanned plane includes carry
Part.
The beneficial effects of the present invention are：The present invention has created a kind of land and air double-used automatic grenade launcher, using efficient
The setback-impact when measure in muzzle brake, the body of a gun recoil in casing is to slow down weapon-shooting；The design side of pick up spit of fland Buddhist nun's guide rail
Just weapon carrys additionally functional part and UAV flight；The connection of foot stool and casing uses slot mechanism, solid and reliable, handling side
Just, foot stool is dismantled in UAV flight, is advantageous to lift unmanned plane payload weight.
Brief description of the drawings
The land and air double-used automatic grenade launcher general structure schematic diagrams of Fig. 1；
Fig. 2 gun barrel journal stirrup schematic diagrames；
Fig. 3 buffer gears and elastic buffering pad partial sectional view；
Fig. 4 muzzle brake schematic diagrames；
Fig. 5 necks and foot stool partial schematic diagram；
Fig. 6 is mounted to unmanned plane use state diagram.
Embodiment
Many details are elaborated in the following description to facilitate a thorough understanding of the present invention, still the present invention can be with
It is different from other manner described here using other to implement, it is clear that described embodiment is only one of the present invention
Divide embodiment, rather than whole embodiments, therefore the present invention is not limited by following public specific embodiment.Based on this hair
Bright embodiment, those skilled in the art obtain all other embodiment in the case of creative work is not made, belonged to
In the scope of protection of the invention.The embodiment of the present invention is described in detail with reference to Figure of description.
As shown in figure 1, land and air double-used automatic grenade launcher general structure, including the body of a gun 2, muzzle brake 1, casing 4, buffering
Mechanism 5 (dashed box), elastic buffering pad 6 (dashed box), pick up spit of fland Buddhist nun's guide rail 3, foot stool 7.Muzzle brake 1 is arranged on gun barrel front end, is one
Body；The installation body of a gun among casing 2, support and constraint body of a gun motion；Buffer gear 5 connects the body of a gun and casing；Elastic buffer
Pad 6 is arranged between automatic drive end unit and casing, further reduces impact of the body of a gun motion to casing and shooter or platform；Pick up
Spit of fland Buddhist nun's guide rail 3 is arranged on above casing, can carry additionally the functional parts such as gun sight, and the handling of unmanned plane carry are also very convenient；Foot stool 7
Below casing, connected for notch, handling are convenient.
As shown in Fig. 2, gun barrel journal stirrup 22 is located at gun barrel tail end, has two or more to be uniformly distributed, and gun barrel 21 passes through journal stirrup 22
It is connected with buffer gear 6, and gun barrel 21 is constrained in casing 4.
As shown in figure 3, buffer gear includes guide rod 51, spring 52, guide rod 51 is consistent with the quantity of gun barrel journal stirrup 22 and uniform
Distribution, the both ends of guide rod 51 are fixed on casing 4, and guide rod 51 passes through gun barrel journal stirrup 22, and spring 52 is placed on gun barrel journal stirrup on guide rod 51
22 both sides.Elastic buffering pad 6 is arranged between the afterbody of automatic machine 23 and casing 4, reduces body of a gun motion to casing and shooter or flat
The impact of platform.
As shown in figure 4, muzzle brake is a body efficient muzzle brake, body center is projectile flight passage 11, bullet
The both sides of flight corridor 11 are symmetrical arranged some spouts towards the powder gases passage 12 at side rear.Gas passage is by powder gases to side
Rear exports, to offset recoil when shooting.
As shown in figure 5, an inserted sheet is arranged at foot stool top, respectively there is an elastic bayonet lock 71 inserted sheet middle part both sides.Neck 72
Positioned at the lower section of casing 4, in three face semi-surrounding structures, respectively there is a bayonet lock matched with elastic bayonet lock 71 neck both sides middle part
Hole 73, the direction of neck 72 are vertical with the direction of the body of a gun 2.Foot stool may be inserted into neck when compressing elastic bayonet lock, and elastic bayonet lock is from card
Foot stool is locked during the pin hole ejection of groove.
The present invention also proposes a kind of unmanned plane, and UAV flight grenade launcher described above, unmanned plane 8 includes carry
Part.As shown in fig. 6, pick up spit of fland Buddhist nun's guide rail of the carry part 9 of unmanned plane 8 locking transmitter, that is, complete carry.
Above in association with schematic diagram to the present invention have been described in detail, when the embodiment of the present invention is described in detail, for purposes of illustration only,
Schematic diagram can disobey general proportion and make partial enlargement, and the explanation of embodiment illustrated above is only intended to help and understands the present invention
Principle and method and it is unrestricted；Meanwhile for those skilled in the art, according to the thought of the present invention, in specific embodiment party
There will be changes in formula and application.In summary, this specification content should not be construed as limiting the invention, and appoint
What those familiar with the art the invention discloses technical scope in, change or replacement can be readily occurred in, all should
Cover within scope of the presently claimed invention.
Claims (9)
1. the empty general automatic grenade launcher in a kind of land, it is characterised in that including the body of a gun, muzzle brake, casing, buffer gear, elasticity
Cushion pad, pick up spit of fland Buddhist nun's guide rail, foot stool.
2. the body of a gun according to claim 1, it is characterised in that including gun barrel, automatic machine, gun barrel tail end has two or more uniform
The journal stirrup of distribution, gun barrel are connected with buffer gear by journal stirrup and constrain in gun barrel in casing.
3. muzzle brake according to claim 1, it is characterised in that center is projectile flight passage, projectile flight passage both sides pair
Claim the powder gases passage for setting some spouts towards side rear.
4. buffer gear according to claim 1, it is characterised in that including guide rod, spring, before guide rod both ends are fixed on casing
Portion, guide rod pass through gun barrel journal stirrup, and spring is placed on guide rod.
5. elastic buffering pad according to claim 1, it is characterised in that between automatic drive end unit and casing.
6. the empty general automatic grenade launcher in a kind of land according to claim 1, it is characterised in that pick up spit of fland Buddhist nun's guide rail is installed
Above casing or side.
7. foot stool according to claim 1, it is characterised in that installed in casing bottom, connected for notch.
8. neck according to claim 7, it is characterised in that below casing, in three face semi-surrounding structures, neck both sides
Respectively there is a pin hole middle part, and the direction of neck is vertical with gun barrel direction.
9. a kind of unmanned plane, it is characterised in that including the automatic grenade launcher described in claim any one of 1-8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711026042.2A CN107588679A (en) | 2017-10-27 | 2017-10-27 | A kind of land and air double-used automatic grenade launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711026042.2A CN107588679A (en) | 2017-10-27 | 2017-10-27 | A kind of land and air double-used automatic grenade launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107588679A true CN107588679A (en) | 2018-01-16 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711026042.2A Pending CN107588679A (en) | 2017-10-27 | 2017-10-27 | A kind of land and air double-used automatic grenade launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107588679A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109186327A (en) * | 2018-09-21 | 2019-01-11 | 浙江海洋大学 | A kind of practice rifle for shooting sports |
| CN109649652A (en) * | 2018-11-01 | 2019-04-19 | 广西康纳环保有限公司 | A kind of unmanned plane and fire-extinguishing |
| RU221643U1 (en) * | 2023-06-09 | 2023-11-15 | Карауланов Антон Александрович | Small unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202141378U (en) * | 2010-12-27 | 2012-02-08 | 中国北方工业公司 | General structure of automatic grenade launcher |
| US20130056586A1 (en) * | 2011-09-02 | 2013-03-07 | Sikorsky Aircraft Corporation | Automatic jettison system for a rotorcraft |
| CN205332921U (en) * | 2015-12-21 | 2016-06-22 | 四川华庆机械有限责任公司 | Shrapnel launcher is hung to pick up type rifle |
| CN105730698A (en) * | 2016-04-28 | 2016-07-06 | 山西阿瑞斯自动化科技有限公司 | Small fire extinguishing unmanned helicopter |
| 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 |
| CN206235240U (en) * | 2016-11-23 | 2017-06-09 | 深圳市轻准科技有限公司 | A kind of grenade launcher |
-
2017
- 2017-10-27 CN CN201711026042.2A patent/CN107588679A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202141378U (en) * | 2010-12-27 | 2012-02-08 | 中国北方工业公司 | General structure of automatic grenade launcher |
| US20130056586A1 (en) * | 2011-09-02 | 2013-03-07 | Sikorsky Aircraft Corporation | Automatic jettison system for a rotorcraft |
| CN205332921U (en) * | 2015-12-21 | 2016-06-22 | 四川华庆机械有限责任公司 | Shrapnel launcher is hung to pick up type rifle |
| CN105730698A (en) * | 2016-04-28 | 2016-07-06 | 山西阿瑞斯自动化科技有限公司 | Small fire extinguishing unmanned helicopter |
| 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 |
| CN206235240U (en) * | 2016-11-23 | 2017-06-09 | 深圳市轻准科技有限公司 | A kind of grenade launcher |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109186327A (en) * | 2018-09-21 | 2019-01-11 | 浙江海洋大学 | A kind of practice rifle for shooting sports |
| CN109649652A (en) * | 2018-11-01 | 2019-04-19 | 广西康纳环保有限公司 | A kind of unmanned plane and fire-extinguishing |
| RU221643U1 (en) * | 2023-06-09 | 2023-11-15 | Карауланов Антон Александрович | Small unmanned aerial vehicle |
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Application publication date: 20180116 |
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