CN208155144U - A kind of gun clamping device with spring bumper being assemblied in unmanned plane - Google Patents
A kind of gun clamping device with spring bumper being assemblied in unmanned plane Download PDFInfo
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- CN208155144U CN208155144U CN201820348375.0U CN201820348375U CN208155144U CN 208155144 U CN208155144 U CN 208155144U CN 201820348375 U CN201820348375 U CN 201820348375U CN 208155144 U CN208155144 U CN 208155144U
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- gun
- spring
- fixed
- cylinder boss
- steering engine
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Abstract
The utility model discloses a kind of gun clamping devices with spring bumper for being assemblied in unmanned plane, including gun clamping clamp mechanism, firing lock, the first cylinder boss, the second cylinder boss and Liang Zu spring buffer mechanism, Liang Zu spring buffer mechanism is symmetricly set on gun aid clamp mechanism two sides, firing lock is fixed on any one side bottom of gun aid clamp mechanism, first cylinder boss and the second cylinder boss are separately fixed at Liang Zu spring buffer mechanism lateral wall, the first cylinder boss and the second cylinder boss and cascade for holder.The utility model overall structure is concise, and quality is small;It is used in series using limit spring and buffer spring, so that firearms position when not firing is stablized, multiple also to be buffered into process while recoil process obtains buffering, the unnecessary impact vibration of reduction.
Description
Technical field
The utility model belongs to unmanned plane field, and in particular to a kind of rifle with spring bumper for being assemblied in unmanned plane
Branch clamping device.
Background technique
Unmanned plane is an important developing direction on Future Information battlefield, be with a wide range of applications with it is important
Application value in army, it has also become the hot subject that countries in the world are competitively studied.Although unmanned battle platform is as a kind of new general
The operational weapon of thought, but these unmanned battle platforms be mostly using ground unmanned vehicle or biggish fixed-wing unmanned plane as carrier,
Current small-sized rotor wing unmanned aerial vehicle is used to explore mostly, investigate, and there is no small-sized rotor wing unmanned aerial vehicle that can directly to enemy's attack.?
Fight against terrorism and violence field, research in this respect can provide air support firepower and reconnaissance capability well to the police.
Wu Jinji exists《Certain new special grasping system design studies》In propose a kind of clamping of new special automatic weapon
System realizes clamping by gun stock fixture and muzzle fixture, and utilizes pedestal and sliding rail, and be installed on the buffering of pedestal tail portion
Spring realizes that buffer function, main problem are that pedestal quality is excessive, and overall structure is huge, not enough simplify coordination, Wu Faan
Loaded on aerial platform, and firearms do not fire, in a free state, lack limiting device, and cannot be easily managed again into process.
Summary of the invention
The purpose of this utility model is to provide a kind of gun clamping machines with spring bumper for being assemblied in unmanned plane
What structure solves problem is solved the clamping percussion firearms on unmanned aerial vehicle platform, and provide the clamping machine of recoil pooling feature
The design of structure.
Realize the utility model aim technical solution be:It is a kind of be assemblied in unmanned plane with spring bumper
Gun clamping device, including gun clamping clamp mechanism, firing lock, the first cylinder boss, the second cylinder boss and two groups of springs
Buffer gear, Liang Zu spring buffer mechanism are symmetricly set on gun aid clamp mechanism two sides, and firing lock is fixed on gun aid
Any one side bottom of clamp mechanism, the first cylinder boss and the second cylinder boss are separately fixed on the outside of Liang Zu spring buffer mechanism
Wall, the first cylinder boss and the second cylinder boss are cascaded for holder.
Gun clamping clamp mechanism include baffle, handle rubber pad, the first gun connecting plate, the second gun connecting plate,
Two blocks of aluminium sheets, two the first rubber blocks, the second rubber block and a pair of of pipe clamp, the first gun connecting plate and the second gun connecting plate are flat
Row interval setting, its rear end are connected by baffle, and front inner wall is connected with a side wall of the first rubber block respectively, two blocks of aluminium sheets
It is separately fixed at another side wall of the first rubber block, is fixed with the second rubber block between two blocks of aluminium sheets;Handle rubber pad is fixed
On baffle, and between the first gun connecting plate and the second gun connecting plate, a pair of of pipe clamp is fixed on the top of aluminium sheet, rifle
Branch is fitted into gun aid clamp mechanism, and handle resists handle rubber pad, and gun barrel emission port stretches out pipe clamp, and pipe clamp clamps gun barrel
Position in conjunction with gun barrel, the first gun connecting plate bottom are equipped with protrusive board, and the protrusive board is located at firearm trigger position, for connecting
Firing lock, Liang Zu spring buffer mechanism are respectively symmetrically fixed on the outside of the first gun connecting plate and the second gun connecting plate
Wall.
The spring buffer mechanism includes linear bearing, auxiliary stopper spring, buffer spring and two bearing blocks, linear axis
The bearing for including guide rod and being arranged on guide rod is contracted, the guide rod both ends of linear bearing are separately fixed on two bearing blocks, and two
Bearing block is fixed on the lateral wall of gun connecting plate, and guide rod is divided into two parts by bearing, covers on ipsilateral guide rod with baffle
There is auxiliary stopper spring, is cased with buffer spring on ipsilateral guide rod with pipe clamp;First cylinder boss and the second cylinder boss difference
It is fixed on the bearing of Liang Zu spring buffer mechanism.
The firing lock includes that steering engine, the matched connection frame of steering engine, rubber limited block, cylinder plectrum and steering engine are fixed
Block, steering engine are arranged on steering engine fixed block lateral wall, output shaft sequentially pass through after steering engine fixed block, rubber limited block with steering engine
Matched connection frame be connected, rubber limited block is located at the inner sidewall of steering engine fixed block, by bolt by steering engine, steering engine fixed block and
Rubber limited block is connected;Steering engine fixed block top and the first gun connecting plate bottom protrusive board are connected;Cylinder plectrum is fixed on connection
The inner wall end of frame.
The gun clamping device with spring bumper for being assemblied in unmanned plane further includes ring washer and tubular pad
Circle, air ring snare is in the second cylinder boss root, and for limiting to holder trunnion, tubular washer covers convex in the first cylinder
On platform, limited for the relative position to holder trunnion.
Compared with prior art, remarkable advantage is the utility model:(1)Overall structure is concise, and quality is small;(2)It adopts
It is used in series with limit spring and buffer spring, so that firearms position when not firing is stablized, recoil process is buffered same
When, multiple also to be buffered into process, the unnecessary impact vibration of reduction.
Detailed description of the invention
Fig. 1 is that the overall structure for the gun clamping device with spring bumper that the utility model is assemblied in unmanned plane is shown
It is intended to.
Fig. 2 is gun aid for the gun clamping device with spring bumper that the utility model is assemblied in unmanned plane
The structural schematic diagram of mechanism.
Fig. 3 is the spring buffer machine for the gun clamping device with spring bumper that the utility model is assemblied in unmanned plane
The structural schematic diagram of structure.
Fig. 4 is the firing lock for the gun clamping device with spring bumper that the utility model is assemblied in unmanned plane
Structural schematic diagram.
Fig. 5 is the linear bearing for the gun clamping device with spring bumper that the utility model is assemblied in unmanned plane
Structural schematic diagram.
Specific embodiment
The utility model is described in further detail with reference to the accompanying drawing.
In conjunction with Fig. 1 to Fig. 5, a kind of gun folder with spring bumper being assemblied in unmanned plane described in the utility model
Holding mechanism includes gun clamping clamp mechanism, firing lock, the first cylinder boss 6, the second cylinder boss 13 and two groups of spring buffers
Mechanism, Liang Zu spring buffer mechanism are symmetricly set on gun aid clamp mechanism two sides, and firing lock is fixed on gun aid handset
Any one side bottom of structure, the first cylinder boss 6 and the second cylinder boss 13 are separately fixed on the outside of Liang Zu spring buffer mechanism
Wall, the first cylinder boss 6 and the second cylinder boss 13 are cascaded for holder.
The gun clamping clamp mechanism includes baffle 1, handle rubber pad 2, the first gun connecting plate 3, the connection of the second gun
The first rubber block 8 of 11, two blocks of plate aluminium sheet 9, two, the second rubber block 10 and a pair of of pipe clamp 14, the first gun connecting plate 3 and second
The setting of 11 parallel interval of gun connecting plate, its rear end is connected by baffle 1, front inner wall one with the first rubber block 11 respectively
Side wall is connected, and two blocks of aluminium sheets 9 are separately fixed at another side wall of the first rubber block 11, are fixed with second between two blocks of aluminium sheets 9
Rubber block 10.Handle rubber pad 2 is fixed on baffle 1, and be located at the first gun connecting plate 3 and the second gun connecting plate 11 it
Between, a pair of of pipe clamp 14 is bolted on the top of aluminium sheet 9, and gun are fitted into gun aid clamp mechanism, and handle, which resists, to be held
Rubber pad 2, gun barrel emission port stretches out pipe clamp 14, and pipe clamp 14 clamps position of the gun barrel in conjunction with gun barrel, the connection of the first gun
3 bottom of plate is equipped with protrusive board, and the protrusive board is located at firearm trigger position.Above-mentioned attachment, which can be used, to be bolted.
The spring buffer mechanism includes linear bearing 15, auxiliary stopper spring 4, buffer spring 7 and two bearing block 15-
1, linear bearing 15 includes guide rod 15-2 and the bearing 15-3 being arranged on guide rod 15-2, the both ends guide rod 15-2 point of linear bearing
It is not fixed on two bearing block 15-1, two bearing block 15-1 are fixed on the lateral wall of gun connecting plate, and bearing 15-3 will be led
Bar 15-2 is divided into two parts, is cased with auxiliary stopper spring 4 on the guide rod 15-2 ipsilateral with baffle 1, ipsilateral with pipe clamp 14
Buffer spring 7 is cased on guide rod 15-2.
First cylinder boss 6 and the second cylinder boss 13 are bolted on the bearing of Liang Zu spring buffer mechanism respectively
On 15-3.The gun clamping device with spring bumper for being assemblied in unmanned plane further includes ring washer 12 and tubular pad
Circle 5,12 sets of ring washer in 13 root of the second cylinder boss, for limiting to holder trunnion, 5 sets of tubular washer first
On cylinder boss 6, limited for the relative position to holder trunnion.
The firing lock includes steering engine 19, the matched connection frame 17 of steering engine 19, rubber limited block 18,16 and of cylinder plectrum
Steering engine fixed block 20, steering engine 19 are arranged on 20 lateral wall of steering engine fixed block, and output shaft sequentially passes through steering engine fixed block 20, rubber
Connection frame 17 matched with steering engine 19 is connected after glue limited block 18, and rubber limited block 18 is located at the inner sidewall of steering engine fixed block 20,
Steering engine 19, steering engine fixed block 20 and rubber limited block 18 are connected by bolt.20 top of steering engine fixed block passes through bolt and the
One gun connecting plate, 3 bottom protrusive board is connected.Cylinder plectrum 16 is fixed on the inner wall end of connection frame 17, for stirring trigger.Rudder
Machine 19 is for being remotely controlled firing trigger.
The course of work:Screw is by 1 threaded hole of baffle, after resisting handle rubber pad 2 to clamp firearms, by long-range distant
Control, rotates the output shaft of steering engine 19, so that cylinder plectrum 16 is driven to move, firing trigger.Firearms and gun clamping at this time
Mechanism recoil together, moves backward relative to bearing 15-3, and bearing 15-3 is moved toward one another with bearing block 15-1, squeezes buffer spring
7, a part of recoil energy is stored in buffer spring, extends action time to reach, reduces suffered by unmanned machine head
The effect of impact force.
Claims (5)
1. a kind of gun clamping device with spring bumper for being assemblied in unmanned plane, it is characterised in that:It is clamped including gun
Clamp mechanism, firing lock, the first cylinder boss(6), the second cylinder boss(13)With Liang Zu spring buffer mechanism, two groups of springs delay
Punch mechanism is symmetricly set on gun aid clamp mechanism two sides, and firing lock is fixed on any side bottom of gun aid clamp mechanism
Portion, the first cylinder boss(6)With the second cylinder boss(13)It is separately fixed at Liang Zu spring buffer mechanism lateral wall, the first circle
Column boss(6)With the second cylinder boss(13)It is cascaded for holder.
2. the gun clamping device with spring bumper according to claim 1 for being assemblied in unmanned plane, feature exist
In:The gun clamping clamp mechanism includes baffle(1), handle rubber pad(2), the first gun connecting plate(3), the second gun connection
Plate(11), two blocks of aluminium sheets(9), two the first rubber blocks(8), the second rubber block(10)With a pair of of pipe clamp(14), the first gun company
Fishplate bar(3)With the second gun connecting plate(11)Parallel interval setting, its rear end passes through baffle(1)Be connected, front inner wall respectively with
First rubber block(8)A side wall be connected, two blocks of aluminium sheets(9)It is separately fixed at the first rubber block(8)Another side wall, two
Block aluminium sheet(9)Between be fixed with the second rubber block(10);Handle rubber pad(2)It is fixed on baffle(1)On, and it is located at the first gun
Connecting plate(3)With the second gun connecting plate(11)Between, a pair of of pipe clamp(14)It is fixed on aluminium sheet(9)Top, gun be packed into rifle
Branch accommodates in clamp mechanism, and handle resists handle rubber pad(2), gun barrel emission port stretching pipe clamp(14), pipe clamp(14)It clamps
Position of the gun barrel in conjunction with gun barrel, the first gun connecting plate(3)Bottom is equipped with protrusive board, and the protrusive board is located at firearm trigger position,
For connecting firing lock, Liang Zu spring buffer mechanism is respectively symmetrically fixed on the first gun connecting plate(3)Connect with the second gun
Fishplate bar(11)Lateral wall.
3. the gun clamping device with spring bumper according to claim 2 for being assemblied in unmanned plane, feature exist
In:The spring buffer mechanism includes linear bearing(15), auxiliary stopper spring(4), buffer spring(7)With two bearing blocks
(15-1), linear bearing(15)Including guide rod(15-2)With setting in guide rod(15-2)On bearing(15-3), linear bearing
Guide rod(15-2)Both ends are separately fixed at two bearing blocks(15-1)On, two bearing blocks(15-1)It is fixed on gun connecting plate
Lateral wall, bearing(15-3)By guide rod(15-2)Two parts are divided into, with baffle(1)Ipsilateral guide rod(15-2)On be cased with it is auxiliary
Help limit spring(4), with pipe clamp(14)Ipsilateral guide rod(15-2)On be cased with buffer spring(7);First cylinder boss(6)With
Two cylinder boss(13)It is separately fixed at the bearing of Liang Zu spring buffer mechanism(15-3)On.
4. the gun clamping device with spring bumper according to claim 2 for being assemblied in unmanned plane, feature exist
In:The firing lock includes steering engine(19), steering engine(19)Matched connection frame(17), rubber limited block(18), cylinder plectrum
(16)With steering engine fixed block(20), steering engine(19)It is arranged in steering engine fixed block(20)On lateral wall, output shaft sequentially passes through rudder
Machine fixed block(20), rubber limited block(18)Afterwards with steering engine(19)Matched connection frame(17)It is connected, rubber limited block(18)Position
In steering engine fixed block(20)Inner sidewall, by bolt by steering engine(19), steering engine fixed block(20)With rubber limited block(18)Gu
Even;Steering engine fixed block(20)Top and the first gun connecting plate(3)Bottom protrusive board is connected;Cylinder plectrum(16)It is fixed on connection frame
(17)Inner wall end.
5. the gun clamping device with spring bumper according to claim 1 for being assemblied in unmanned plane, feature exist
In:The gun clamping device with spring bumper for being assemblied in unmanned plane further includes ring washer(12)With tubular washer
(5), ring washer(12)It covers in the second cylinder boss(13)Root, for being limited to holder trunnion, tubular washer(5)Set
In the first cylinder boss(6)On, it is limited for the relative position to holder trunnion.
Priority Applications (1)
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CN201820348375.0U CN208155144U (en) | 2018-03-14 | 2018-03-14 | A kind of gun clamping device with spring bumper being assemblied in unmanned plane |
Applications Claiming Priority (1)
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CN201820348375.0U CN208155144U (en) | 2018-03-14 | 2018-03-14 | A kind of gun clamping device with spring bumper being assemblied in unmanned plane |
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CN208155144U true CN208155144U (en) | 2018-11-27 |
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CN201820348375.0U Withdrawn - After Issue CN208155144U (en) | 2018-03-14 | 2018-03-14 | A kind of gun clamping device with spring bumper being assemblied in unmanned plane |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108195227A (en) * | 2018-03-14 | 2018-06-22 | 南京理工大学 | A kind of gun clamping device with spring bumper for being assemblied in unmanned plane |
-
2018
- 2018-03-14 CN CN201820348375.0U patent/CN208155144U/en not_active Withdrawn - After Issue
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108195227A (en) * | 2018-03-14 | 2018-06-22 | 南京理工大学 | A kind of gun clamping device with spring bumper for being assemblied in unmanned plane |
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AV01 | Patent right actively abandoned |
Granted publication date: 20181127 Effective date of abandoning: 20230728 |
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AV01 | Patent right actively abandoned |
Granted publication date: 20181127 Effective date of abandoning: 20230728 |
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AV01 | Patent right actively abandoned | ||
AV01 | Patent right actively abandoned |