CN109760841A - A kind of small drone weapon carrier - Google Patents
A kind of small drone weapon carrier Download PDFInfo
- Publication number
- CN109760841A CN109760841A CN201910064341.8A CN201910064341A CN109760841A CN 109760841 A CN109760841 A CN 109760841A CN 201910064341 A CN201910064341 A CN 201910064341A CN 109760841 A CN109760841 A CN 109760841A
- Authority
- CN
- China
- Prior art keywords
- hook
- rocker arm
- hanger
- cam
- scotch
- 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.)
- Granted
Links
- 238000009434 installation Methods 0.000 claims abstract description 5
- 239000007787 solid Substances 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
A kind of small drone weapon carrier, including hanger shell, front support and tail-bracket is respectively set along the rear and front end of guided missile installation direction in the bottom surface of hanger shell, the hook for connecting guided missile lifting lug is equipped between front support and tail-bracket, it is mounted in the middle part of hook on the hook axis of hanger enclosure interior, hanger enclosure interior is provided with rotating electromagnet, and rotating electromagnet is able to drive driver plate and is rotated, and driver plate is connect by connecting rod with the scotch that can be pivoted；Latch cam is installed in the tail portion of hook, and latch cam is matched with the rocker arm that can be pivoted, one end connecting rocker arm axis of rocker arm, and the other end installs rocker cam；Scotch is matched with rocker cam, and scotch drives rocker arm to rotate by rocker cam, and rocker arm drives hook rotation by latch cam.Operation of the present invention is convenient, carries fixed when body, can be combined, can be reused, compact-sized, high reliablity with airborne electronic equipment system using rotating electromagnet.
Description
Technical field
The invention belongs to unmanned plane manufacturing fields, and in particular to a kind of small drone weapon carrier.
Background technique
The task scope of modern military unmanned plane is observed and is injured assessment etc. via traditional aerial reconnaissance, battlefield and expands
Inhibit to battlefield, air-to-ground attack, intercept the fields such as cruise missile or even dog fight.Unmanned plane not only to someone's fighter plane into
Row is supported, and plays a part of substituting manned aircraft in many cases.It is small in the developing direction of the following unmanned plane
Type attack unmanned plane will occupy the effect that do not replace, and unmanned plane carries guided bomb or guided missile, and enemy is found during investigation
The important goal that side temporarily occurs can be attacked in real time, realized " examining knotting to close ", given full play to the fighting efficiency of weaponry,
Reduce because call for fire support be delayed opportunity of combat a possibility that, unmanned plane make a return voyage after again carry weapon continue to use.
Summary of the invention
It is an object of the invention to be directed to above-mentioned the problems of the prior art, a kind of small drone weapon carrier is provided,
By the lifting lug of hook connection guided missile, using rotating electromagnet control weapon release, reliable in action is easy to use.
To achieve the goals above, the technical solution adopted by the present invention are as follows:
Including hanger shell, front support is respectively set with after along the rear and front end of guided missile installation direction in the bottom surface of hanger shell
Bracket is equipped with the hook for connecting guided missile lifting lug, is mounted in hanger shell in the middle part of hook between front support and tail-bracket
On the hook axis in portion, hanger enclosure interior is provided with rotating electromagnet, and rotating electromagnet is able to drive driver plate and is rotated, driver plate
It is connect by connecting rod with the scotch that can be pivoted；Latch cam is installed in the tail portion of hook, latch cam with can be around axis
The rocker arm of rotation matches, one end connecting rocker arm axis of rocker arm, and the other end installs rocker cam；The scotch and rocker arm are convex
Wheel matches, and scotch drives rocker arm to rotate by rocker cam, and rocker arm drives hook rotation by latch cam.
The scotch is mounted in the braking roll of hanger enclosure interior, and stop torsional spring is equipped in braking roll.
The rocker arm shaft is mounted on the inside of hanger shell, is equipped with rocking arm torsional spring on rocker arm shaft.
The middle part of the hook is connected with the tension spring in the portion that is immobilized in the shell, and when opening of hook will overcome the drawing of tension spring
Power.
The hanger enclosure interior is provided with limited block, and the gear matched with the gib head of hook is provided on limited block
Plate.
The limited block is mounted on the limit shaft of hanger enclosure interior, and limit torsional spring is equipped on limit shaft.
The hanger enclosure interior is provided with electromagnet stent, and rotating electromagnet is mounted on electromagnet stent.
Fixing screws are installed, the body of guided missile can be held out against by adjusting fixing screws pushing in the front support.
Compared with prior art, the present invention is with following the utility model has the advantages that passing through front support and tail-bracket for the bullet of guided missile
Body is held out against, and by the lifting lug of hook connection guided missile between front support and tail-bracket, scotch withstands rocker cam, makes the position of hook
It sets and is kept fixed, guided missile can not loosen.When weapon is discharged, rotating electromagnet, which is powered, drives driver plate rotation, and driver plate passes through
Connecting rod drives scotch rotation, and hook disengages guided missile lifting lug under the action of latch cam.Operation of the present invention is convenient, carries body
When it is fixed, additionally it is possible to be applied to install other unmanned plane weapons, can be with airborne electronic equipment system phase using rotating electromagnet
In conjunction with, solve the problems, such as small drone weapon installation, can reuse, compact-sized, high reliablity.
Further, scotch of the present invention is mounted in braking roll, and stop torsional spring is equipped in braking roll, is pacified on rocker arm shaft
Equipped with rocking arm torsional spring, the middle part of hook is connect with tension spring, and limited block is mounted on the limit shaft of hanger enclosure interior, on limit shaft
Limit torsional spring is installed, by reasonable combination torsional spring and the elastic force of tension spring, guarantees direction of rotation and the scope of activities of hook.
Detailed description of the invention
The structure sectional view of hanger under Fig. 1 opening of hook state；
Fig. 2 links up with the structure sectional view of hanger under closed state；
Main view under Fig. 3 assembled state of the present invention；
Rearview under Fig. 4 assembled state of the present invention；
The schematic perspective view of Fig. 5 Rocker arm section of the present invention；
The schematic perspective view of Fig. 6 invention hook part；
In attached drawing: 1- lower case；2- electromagnet stent；3- rotating electromagnet；4- driver plate；5- connecting rod；6- scotch；7- stops
Dynamic torsional spring；8- braking roll；9- rocker cam；10- rocker arm；11- rocking arm torsional spring；12- rocker arm shaft；13- hook；14- tension spring；15-
Latch cam；16- links up with axis；17- limited block；18- limits torsional spring；19- limit shaft；20- tail-bracket；21- front support；22- is solid
Determine screw；23- upper housing；24- weapon.
Specific embodiment
Present invention will be described in further detail below with reference to the accompanying drawings.
Referring to Fig. 1-2, small drone weapon carrier of the present invention includes the hanger shell being made of upper housing 23 and lower case 1
Front support 21 and tail-bracket 20, front support 21 is respectively set along the rear and front end of guided missile installation direction in the bottom surface of body, hanger shell
It is equipped with the hook 13 for connecting guided missile lifting lug between tail-bracket 20 and as shown in figures 3 and 4 fixed spiral shell is installed in front support 21
Nail 22, fixing screws 22 are arranged in the both ends of front support 21, and the body of guided missile can be held out against by adjusting the pushing of fixing screws 22.It hangs
The middle part of hook 13 is mounted on the hook axis 16 inside lower case 1, and rotating electromagnet 3, rotating electromagnet are equipped with inside lower case 1
3 are mounted on electromagnet stent 2.Rotating electromagnet 3 is able to drive driver plate 4 and is rotated, driver plate 4 by connecting rod 5 with can be around
The scotch 6 of axis rotation connects, and scotch 6 is mounted in the braking roll 8 inside lower case 1, and stop torsion is equipped in braking roll 8
Spring 7.Latch cam 15 is installed in the tail portion of hook 13, and latch cam 15 is matched with the rocker arm 10 that can be pivoted, rocker arm 10
One end connecting rocker arm axis 12, the other end installs rocker cam 9, and scotch 6 matches with rocker cam 9.Rocker arm shaft 12 is installed
In the inside of hanger shell, rocking arm torsional spring 11 is installed on rocker arm shaft 12.The middle part of hook 13 and the drawing for being immobilized in the shell portion
Spring 14 is connected.Limited block 17 is equipped with inside lower case 1, limited block 17 is mounted on limit shaft 19, installs on limit shaft 19 limited
Position torsional spring 18, the baffle matched with the gib head for linking up with 13 is provided on limited block 17.
The working principle of the invention and action process are as follows:
When hanging weapon 24, the lifting lug on weapon 24 pushes up limited block 17 and hook 13, and hook 17 is with hook
Cam 15 is rotated clockwise around hook axis 16, so that tension spring 14 is in tension state, at this point, effect of the rocker arm 10 in rocking arm torsional spring 11
Under, it is rotated clockwise around rocker arm shaft 12, scotch 6 rotates clockwise under the action of stop torsional spring 7 around braking roll 8, and connecting rod 5 is drawn
Dynamic driver plate 4 makes rotating electromagnet 3 be in reset state, and tail-bracket 20 holds weapon 24, tighten fixing screws 22 by weapon 24 to
It pushes, keeps weapon 24 fixed, at this point, scotch 6 withstands rocker cam 9, so that rocker arm 10 is in horizontality, link up with 13 position
Fixed, weapon 24 can not loosen.When weapon 24 discharges, rotating electromagnet 3, which is powered, drives driver plate 4 to rotate, and driver plate 4 makes connecting rod 5
Scotch 6 is driven to rotate, at this point, rocker cam 9, without support, hook 13 revolves under the action of tension spring 14 around hook axis 16 counterclockwise
Turn, under the action of latch cam 15, rocker arm 10 around rocker arm shaft 12 counterclockwise rotate so that weapon 24 discharge, stop torsional spring 7 with
Rocking arm torsional spring 11 is in by the state of torsion.
The foregoing is merely presently preferred embodiments of the present invention, not to do restriction in any form to the present invention, this
Field technical staff is not it should be understood that under conditions of departing from spirit of that invention and principle, if the present invention can also carry out
Dry finishing changes or simple replacement, these modifications and replacement are also each fallen within the scope of being delimited by submitted claim.
Claims (8)
1. a kind of small drone weapon carrier, it is characterised in that: including hanger shell, the bottom surface of hanger shell is installed along guided missile
Front support (21) and tail-bracket (20) are respectively set in the rear and front end in direction, are equipped with and use between front support (21) and tail-bracket (20)
It is mounted on the hook axis (16) of hanger enclosure interior in the middle part of the hook (13) of connection guided missile lifting lug, hook (13), hanger
Enclosure interior is provided with rotating electromagnet (3), and rotating electromagnet (3) is able to drive driver plate (4) and is rotated, and driver plate (4) passes through
Connecting rod (5) is connect with the scotch (6) that can be pivoted；Latch cam (15) are installed in the tail portion for linking up with (13), latch cam
(15) it is matched with the rocker arm (10) that can be pivoted, one end connecting rocker arm axis (12) of rocker arm (10), other end installation is shaken
Arm cam (9)；The scotch (6) is matched with rocker cam (9), and scotch (6) drives rocker arm by rocker cam (9)
(10) it rotates, rocker arm (10) drives hook (13) rotation by latch cam (15).
2. small drone weapon carrier according to claim 1, it is characterised in that: the scotch (6) is mounted on
In the braking roll (8) of hanger enclosure interior, stop torsional spring (7) are installed in braking roll (8).
3. small drone weapon carrier according to claim 1, it is characterised in that: the rocker arm shaft (12) is mounted on
The inside of hanger shell is equipped with rocking arm torsional spring (11) on rocker arm shaft (12).
4. small drone weapon carrier according to claim 1, it is characterised in that: the middle part of the hook (13) and solid
The tension spring (14) for being scheduled on enclosure interior is connected, and hook (13) will overcome the pulling force of tension spring (14) when opening.
5. small drone weapon carrier according to claim 1, it is characterised in that: the hanger enclosure interior setting
Have limited block (17), the baffle matched with the gib head of hook (13) is provided on limited block (17).
6. small drone weapon carrier according to claim 5, it is characterised in that: the limited block (17) is mounted on
On the limit shaft (19) of hanger enclosure interior, limit torsional spring (18) is installed on limit shaft (19).
7. small drone weapon carrier according to claim 1, it is characterised in that: the hanger enclosure interior setting
Have electromagnet stent (2), rotating electromagnet (3) is mounted on electromagnet stent (2).
8. small drone weapon carrier according to claim 1, it is characterised in that: installed in the front support (21)
Have fixing screws (22), adjusts fixing screws (22) and push and the body of guided missile can be held out against.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910064341.8A CN109760841B (en) | 2019-01-23 | 2019-01-23 | Small unmanned aerial vehicle weapon stores pylon |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910064341.8A CN109760841B (en) | 2019-01-23 | 2019-01-23 | Small unmanned aerial vehicle weapon stores pylon |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109760841A true CN109760841A (en) | 2019-05-17 |
| CN109760841B CN109760841B (en) | 2024-01-26 |
Family
ID=66455227
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910064341.8A Active CN109760841B (en) | 2019-01-23 | 2019-01-23 | Small unmanned aerial vehicle weapon stores pylon |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109760841B (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110304253A (en) * | 2019-06-04 | 2019-10-08 | 成都飞机工业集团电子科技有限公司 | It is a kind of for the linkage of airborne external hanging device, limit, automatically controlled throwing mechanism |
| CN110654544A (en) * | 2019-11-15 | 2020-01-07 | 中国工程物理研究院总体工程研究所 | Position-adjustable airborne microminiature missile launching separation device for unmanned aerial vehicle |
| CN111942591A (en) * | 2020-08-20 | 2020-11-17 | 北京京东乾石科技有限公司 | Cargo throwing device and aircraft |
Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB543009A (en) * | 1940-10-25 | 1942-02-05 | Roe A V & Co Ltd | Improvements relating to bomb carriers for aircraft |
| US3898909A (en) * | 1973-03-05 | 1975-08-12 | Ml Aviation Co Ltd | Ejector release unit for use in aircraft |
| US4922799A (en) * | 1988-05-03 | 1990-05-08 | Messerschmitt-Boelkow-Blohm Gmbh | Apparatus for suspending, strapping, and launching a flying body from a carrier |
| EP2511178A1 (en) * | 2011-04-13 | 2012-10-17 | Dassault Aviation | Releasable locking device of a flying vehicle intended for being launched from a platform |
| US20160083089A1 (en) * | 2014-09-18 | 2016-03-24 | Raytheon Company | Aircraft store deployment system with improved safety of arming and releasing stores |
| CN106081112A (en) * | 2016-07-12 | 2016-11-09 | 于卫华 | Unmanned vehicle intelligence acceptance goods device and implementation |
| CN107406143A (en) * | 2014-12-01 | 2017-11-28 | Edo Mbm科技有限公司 | Small-sized storehouse suspension and releasing unit |
| KR101853264B1 (en) * | 2017-05-16 | 2018-04-30 | 아이원스 주식회사 | Bomb rack unit |
| CN207466973U (en) * | 2017-11-22 | 2018-06-08 | 河南三和航空工业有限公司 | A kind of airborne fire extinguisher bomb of combined guidance |
| CN108820214A (en) * | 2018-06-11 | 2018-11-16 | 天津航天中为数据系统科技有限公司 | A kind of aircraft, which is examined, beats control emission system |
| CN209553513U (en) * | 2019-01-23 | 2019-10-29 | 西安深瞳智控技术有限公司 | A kind of rotating electromagnet control unmanned plane weapon carrier |
-
2019
- 2019-01-23 CN CN201910064341.8A patent/CN109760841B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB543009A (en) * | 1940-10-25 | 1942-02-05 | Roe A V & Co Ltd | Improvements relating to bomb carriers for aircraft |
| US3898909A (en) * | 1973-03-05 | 1975-08-12 | Ml Aviation Co Ltd | Ejector release unit for use in aircraft |
| US4922799A (en) * | 1988-05-03 | 1990-05-08 | Messerschmitt-Boelkow-Blohm Gmbh | Apparatus for suspending, strapping, and launching a flying body from a carrier |
| EP2511178A1 (en) * | 2011-04-13 | 2012-10-17 | Dassault Aviation | Releasable locking device of a flying vehicle intended for being launched from a platform |
| US20160083089A1 (en) * | 2014-09-18 | 2016-03-24 | Raytheon Company | Aircraft store deployment system with improved safety of arming and releasing stores |
| CN107406143A (en) * | 2014-12-01 | 2017-11-28 | Edo Mbm科技有限公司 | Small-sized storehouse suspension and releasing unit |
| CN106081112A (en) * | 2016-07-12 | 2016-11-09 | 于卫华 | Unmanned vehicle intelligence acceptance goods device and implementation |
| KR101853264B1 (en) * | 2017-05-16 | 2018-04-30 | 아이원스 주식회사 | Bomb rack unit |
| CN207466973U (en) * | 2017-11-22 | 2018-06-08 | 河南三和航空工业有限公司 | A kind of airborne fire extinguisher bomb of combined guidance |
| CN108820214A (en) * | 2018-06-11 | 2018-11-16 | 天津航天中为数据系统科技有限公司 | A kind of aircraft, which is examined, beats control emission system |
| CN209553513U (en) * | 2019-01-23 | 2019-10-29 | 西安深瞳智控技术有限公司 | A kind of rotating electromagnet control unmanned plane weapon carrier |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110304253A (en) * | 2019-06-04 | 2019-10-08 | 成都飞机工业集团电子科技有限公司 | It is a kind of for the linkage of airborne external hanging device, limit, automatically controlled throwing mechanism |
| CN110654544A (en) * | 2019-11-15 | 2020-01-07 | 中国工程物理研究院总体工程研究所 | Position-adjustable airborne microminiature missile launching separation device for unmanned aerial vehicle |
| CN110654544B (en) * | 2019-11-15 | 2024-05-07 | 中国工程物理研究院总体工程研究所 | Unmanned aerial vehicle airborne micro missile throwing and separating device with adjustable position |
| CN111942591A (en) * | 2020-08-20 | 2020-11-17 | 北京京东乾石科技有限公司 | Cargo throwing device and aircraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109760841B (en) | 2024-01-26 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109760841A (en) | A kind of small drone weapon carrier | |
| CN209553513U (en) | A kind of rotating electromagnet control unmanned plane weapon carrier | |
| CN110937111B (en) | Small-size cluster unmanned aerial vehicle dispensing system of gliding style | |
| CN110271671B (en) | Bullet throwing device and fire-fighting unmanned aerial vehicle | |
| KR101947912B1 (en) | Rotating type apparatus for weapon release | |
| CN109387113A (en) | The transmission ammunition belt system of dozen aircraft is examined by a kind of omnidirectional | |
| CN111348194A (en) | Microminiature unmanned aerial vehicle guided missile mounting and releasing device integrated with fire control system | |
| US6060411A (en) | Low observable weapon kit | |
| CA3043563A1 (en) | Drone weapon system | |
| CN115465450A (en) | Gun-shot cluster type folding rotor micro unmanned aerial vehicle | |
| CN210310885U (en) | Bullet shooting device and fire control and disaster relief unmanned aerial vehicle | |
| RU2703695C1 (en) | Armored facility armored compartment | |
| CN209230422U (en) | It increases rain artificially hail-suppression rocket bullet storage and conveying box | |
| CN107588679A (en) | A kind of land and air double-used automatic grenade launcher | |
| CN114537669A (en) | Unmanned aerial vehicle machine carries system of throwing | |
| CN219277812U (en) | Can section of thick bamboo shoot horizontal folding unmanned aerial vehicle | |
| CN113959256B (en) | Protective missile launching box and remote control weapon station | |
| CN216186055U (en) | Bullet-throwing unmanned aerial vehicle | |
| CN211893655U (en) | Tear-gas shells emitter and unmanned aerial vehicle | |
| CN217969933U (en) | Omnidirectional bullet rack for scouting and beating airplane | |
| RU2601999C1 (en) | Helicopter pod-type machine-gun module | |
| RU2184333C2 (en) | Armored vehicle turret with weapons system | |
| RU2797525C1 (en) | Removable suspended aircraft weapons container | |
| CN211205049U (en) | Dual-purpose rope-catching and net-catching launching gun | |
| CN219948546U (en) | Machine carries marching type ammunition throwing device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |