CN208828125U - Firing device of low-recoil mounting platform of small unmanned aerial vehicle - Google Patents
Firing device of low-recoil mounting platform of small unmanned aerial vehicle Download PDFInfo
- Publication number
- CN208828125U CN208828125U CN201821605324.8U CN201821605324U CN208828125U CN 208828125 U CN208828125 U CN 208828125U CN 201821605324 U CN201821605324 U CN 201821605324U CN 208828125 U CN208828125 U CN 208828125U
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- CN
- China
- Prior art keywords
- percussion
- trigger
- pull rod
- mounting plate
- rifle
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000010304 firing Methods 0.000 title abstract description 4
- 238000009527 percussion Methods 0.000 claims abstract description 69
- 238000000034 method Methods 0.000 abstract description 5
- 238000009434 installation Methods 0.000 abstract description 2
- 238000000926 separation method Methods 0.000 abstract 2
- 230000001960 triggered effect Effects 0.000 abstract 1
- 230000009471 action Effects 0.000 description 5
- 238000005516 engineering process Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 230000008859 change Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007667 floating Methods 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
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Abstract
The utility model discloses a percussion device of a small unmanned aerial vehicle low-recoil hanging platform, which comprises a percussion machine mounting plate fixedly mounted with a rifle connecting frame through screws, a trigger pull rod guide plate connected with the percussion machine mounting plate through screws, a percussion steering engine fixedly connected with the percussion machine mounting plate through bolts, a trigger toggle wheel connected with a rotating disc of the percussion steering engine, a percussion pull rod separation blade movably connected with the trigger toggle wheel, a trigger pull rod riveted with the other end of the percussion pull rod separation blade through a stud, and a percussion rod in threaded connection with the trigger pull rod; the trigger mounting plate is arranged on the upper part; a sliding groove is formed in one side, away from the percussion cabin machine, of the trigger poking wheel; the utility model discloses a low recoil carry platform's of unmanned aerial vehicle percussion device, it is firm with the installation of rifle link, its trigger of rifle can be triggered well to the firing bar, and the percussion in-process is more stable.
Description
Technical field
The utility model relates to a kind of percussion locks of the low recoil carry platform of small drone, belong to military equipment technology
Field.
Background technique
Fighting efficiency and application prospect after small drone carry small arms are all ideal, but small arms
The recoil generated when shooting is the key problem for influencing small arms in conjunction with small drone；Small drone is flown in the sky
When balance is kept by air force, firearm recoil is to unmanned plane during flying stability and shooting essence under this state
The influence of degree will be amplified, and especially automatic weapon (rifle, machine gun etc.) influence of recoil in continuous fire is to continue
, this will cause very big influence to the flight stability performance of small drone, or even will cause overturning and the pendant of unmanned plane
It falls；Solution to this problem can have following several: (1) the dedicated small arms of carry, and dedicated small arms are i.e. exclusively for small-sized
The small arms of unmanned aerial vehicle design can be reduced gently by modes such as optimization self structure, reduction bullet powder charge, installation muzzle brakes
Influence of the weapon recoil to small drone；Design specialized small arms mean to reduce the general degree of weapon, Er Qiehuo
Power fragment action is also affected；(2) enhance the anti-interference ability of small drone, the stability of small drone and anti-interference
Ability and the design feature of its own, power mode and material composition etc. are because being known as much relations；By optimizing small drone
Its stability and anti-interference ability are improved, this requirement to small drone the relevant technologies is very high；Currently, small drone is also
It is unable to reach the requirement of direct carry small arms, and the raising of its relevant technologies is had got long long way to go；(3) it designs low
Recoil carry platform is designed a kind of low recoil carry platform suitable for small drone, is reduced even using carry platform
Influence of the firearm recoil to unmanned plane during flying stability is eliminated, the requirement to small drone performance is reduced, guarantees simultaneously
The versatility of carry weapon, undoubtedly one very in conjunction with small drone for solving the problems, such as small arms for this mode
Good selection.
With the continuous development of war form, unmanned platform is widely applied, on unmanned platform carry weapon at
For an important development direction；Basic weaponry of the firearms as army, small in size because its structure is simple, firepower duration
The features such as strong, is more suitable for and miniature self-service platform carry；However, the recoil generated when riflery will make optimal in structure
At very big influence；Recoil when especially air fighting platform carries riflery directly affects weapon-shooting precision and takes
The flight stability of carrying platform.Automatic weapon is known as preshoot percussion principle into the principle fired in the process multiple；Using preceding impact
When sending out the weapon-shooting of principle, the energy of the preshoot energy meeting partial offset powder gas of preshoot body backward, to reduce shooting
When recoil；There are blowback, semi-free rifle bolt, gun barrel floating type using the automatic weapon of preshoot percussion principle at present
Deng；In order to cooperate the low recoil carry platform of small drone its shooting percussion, need individually develop can on forward rushing mechanism
The percussion lock that rifle connection frame is fixedly mounted.
Utility model content
In order to solve the above problems, the utility model proposes, and a kind of small drone based on whole rifle preshoot percussion principle is low
The percussion lock of recoil carry platform, can be stably mounted on the rifle connection frame of forward rushing mechanism, and can be well matched with
Auxiliary percussion.
The percussion lock of the low recoil carry platform of the small drone of the utility model, including be fixedly installed in by screw
Percussion lock mounting plate on rifle connection frame, and the trigger pull rod guide plate being connected by screw to percussion lock mounting plate, and with
The percussion steering engine that percussion lock mounting plate is bolted to connection, and the trigger turning wheel being connect with percussion its rotating disc of steering engine,
And the percussion pull rod baffle being flexibly connected with trigger turning wheel, and pulled with percussion its other end of pull rod baffle by what stud riveted
Machine pull rod, and the trigger shaft being connect with trigger pull rod screw；The trigger turning wheel its away from percussion cabin machine side be provided with cunning
Slot；It is movably installed in its sliding slot of trigger turning wheel away from trigger pull rod one end the percussion pull rod baffle, when work, percussion
Steering engine band trigger action turning wheel rotates, and percussion pull rod baffle moves in trigger turning wheel sliding slot, thus with trigger action pull rod and
Trigger shaft is moved along trigger pull rod guide plate, and trigger shaft cocking in motion process, rifle is opened fire, and is fired steering engine later and is driven
Percussion lock resets.
Further, the trigger pull rod one end and percussion pull rod baffle riveting, the other end pass through trigger pull rod and lead
It is threadedly coupled to plate and with trigger shaft.
Still further, the trigger shaft is connect with its trigger of rifle.
Compared with prior art, the percussion of the low recoil carry platform of the small drone of the utility model
Device is firmly installed with rifle connection frame, and trigger shaft can trigger its trigger of rifle well, more stable during percussion.
Detailed description of the invention
Fig. 1 is the firing lock structural schematic diagram of the utility model.
Each component mark in attached drawing are as follows: 21- trigger shaft, 22- trigger pull rod, 23- trigger pull rod guide plate, 24- fire rudder
Machine, 25- trigger turning wheel, 26- fire pull rod baffle, 27- percussion lock mounting plate, the sliding slot of 28- trigger turning wheel.
Specific embodiment
The percussion lock of the low recoil carry platform of small drone as shown in Figure 1, including percussion lock mounting plate 27, and with
The trigger pull rod guide plate 23 that percussion lock mounting plate 27 is connected by screw to, and with 27 company of being bolted of percussion lock mounting plate
The percussion steering engine 24 connect, and the trigger turning wheel 25 being connect with percussion its rotating disc of steering engine 24, and it is movable with trigger turning wheel 25
The percussion pull rod baffle 26 of connection, and the trigger pull rod 22 riveted with percussion its other end of pull rod baffle 26 by stud, and with
The trigger shaft 21 that trigger pull rod 22 is threadedly coupled；The percussion lock mounting plate 27 is fixedly installed in rifle connection frame 6 by screw
On；The trigger turning wheel 25 its away from percussion 24 side of cabin machine be provided with sliding slot 28；The percussion pull rod baffle 26 its deviate from
22 one end of trigger pull rod is movably installed in its sliding slot 28 of trigger turning wheel 25；22 one end of trigger pull rod and percussion pull rod
Baffle 26 rivets, and the other end passes through trigger pull rod guide plate 23 and is threadedly coupled with trigger shaft 21；The trigger shaft 21 and step
The connection of its trigger of rifle.
The percussion lock of the low recoil carry platform of the small drone of the utility model, the course of work are as follows: percussion lock
When structure works, percussion steering engine band trigger action turning wheel is rotated, and percussion pull rod baffle moves in trigger turning wheel sliding slot, thus band
Trigger action pull rod and trigger shaft are moved along trigger pull rod guide plate, and trigger shaft cocking in motion process, rifle is opened fire, later
Firing steering engine drives percussion lock to reset；
Above-described embodiment is only the better embodiment of the utility model, therefore all according to the utility model patent application range
The equivalent change or modification that the structure, feature and principle is done, is included in the scope of the utility model patent application.
Claims (3)
1. a kind of percussion lock of the low recoil carry platform of small drone, it is characterised in that: including passing through with rifle connection frame
The percussion lock mounting plate that screw is fixedly mounted, and the trigger pull rod guide plate being connected by screw to percussion lock mounting plate, and with
The percussion steering engine that percussion lock mounting plate is bolted to connection, and the trigger turning wheel being connect with percussion its rotating disc of steering engine,
And the percussion pull rod baffle being flexibly connected with trigger turning wheel, and pulled with percussion its other end of pull rod baffle by what stud riveted
Machine pull rod, and the trigger shaft being connect with trigger pull rod screw；The percussion lock mounting plate is in upper；The trigger turning wheel its deviate from
Percussion cabin machine side is provided with sliding slot；The percussion pull rod baffle its be movably installed in trigger turning wheel away from trigger pull rod one end
In its sliding slot.
2. the percussion lock of the low recoil carry platform of small drone according to claim 1, it is characterised in that: described to pull
Machine pull rod one end and percussion pull rod baffle riveting, the other end pass through trigger pull rod guide plate and are threadedly coupled with trigger shaft.
3. the percussion lock of the low recoil carry platform of small drone according to claim 1 or 2, it is characterised in that: institute
Stating trigger shaft, its trigger is connect with rifle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821605324.8U CN208828125U (en) | 2018-09-29 | 2018-09-29 | Firing device of low-recoil mounting platform of small unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821605324.8U CN208828125U (en) | 2018-09-29 | 2018-09-29 | Firing device of low-recoil mounting platform of small unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208828125U true CN208828125U (en) | 2019-05-07 |
Family
ID=66317138
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821605324.8U Expired - Fee Related CN208828125U (en) | 2018-09-29 | 2018-09-29 | Firing device of low-recoil mounting platform of small unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208828125U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110530195A (en) * | 2019-09-11 | 2019-12-03 | 中航技进出口有限责任公司 | A kind of driving structure for unmanned plane carry machine gun |
| CN111114786A (en) * | 2020-01-14 | 2020-05-08 | 吉林省翼启飞科技有限公司 | Grenade and grenade throwing device |
-
2018
- 2018-09-29 CN CN201821605324.8U patent/CN208828125U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110530195A (en) * | 2019-09-11 | 2019-12-03 | 中航技进出口有限责任公司 | A kind of driving structure for unmanned plane carry machine gun |
| CN111114786A (en) * | 2020-01-14 | 2020-05-08 | 吉林省翼启飞科技有限公司 | Grenade and grenade throwing device |
| CN111114786B (en) * | 2020-01-14 | 2021-08-31 | 吉林省翼启飞科技有限公司 | Grenade and grenade throwing device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190507 Termination date: 20200929 |