CN209553513U - A kind of rotating electromagnet control unmanned plane weapon carrier - Google Patents
A kind of rotating electromagnet control unmanned plane weapon carrier Download PDFInfo
- Publication number
- CN209553513U CN209553513U CN201920116805.0U CN201920116805U CN209553513U CN 209553513 U CN209553513 U CN 209553513U CN 201920116805 U CN201920116805 U CN 201920116805U CN 209553513 U CN209553513 U CN 209553513U
- Authority
- CN
- China
- Prior art keywords
- hook
- rotating electromagnet
- rocker arm
- unmanned plane
- hanger
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
A kind of rotating electromagnet control unmanned plane 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 equipped 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.The utility model is easy to operate, carry body when it is fixed, can be combined, can be reused, compact-sized, high reliablity with airborne electronic equipment system using rotating electromagnet.
Description
Technical field
The utility model belongs to unmanned plane manufacturing field, and in particular to a kind of rotating electromagnet control unmanned plane weapon extension
Frame.
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.
Utility model content
The purpose of this utility model is that being directed to above-mentioned the problems of the prior art, a kind of rotating electromagnet control nothing is provided
Man-machine weapon carrier, by the lifting lug of hook connection guided missile, using rotating electromagnet control weapon release, reliable in action is used
It is convenient.
To achieve the goals above, the technical solution adopted in the utility model 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 utility model is with following the utility model has the advantages that passing through front support and tail-bracket for guided missile
Body hold out against, by the lifting lug of hook connection guided missile between front support and tail-bracket, scotch withstands rocker cam, makes to link up with
Position be kept fixed, guided missile can not loosen.When weapon is discharged, rotating electromagnet, which is powered, drives driver plate rotation, driver plate
Scotch rotation is driven by connecting rod, hook disengages guided missile lifting lug under the action of latch cam.The utility model is easy to operate,
It carries fixed when body, additionally it is possible to it is applied to that other unmanned plane weapons are installed, it can be with airborne electricity using rotating electromagnet
Subsystem combines, and solves the problems, such as the installation of small drone weapon, can reuse, compact-sized, high reliablity.
Further, the utility model scotch is mounted in braking roll, and stop torsional spring, rocker arm shaft are equipped in braking roll
On rocking arm torsional spring is installed, the middle part of hook is connect with tension spring, and limited block is mounted on the limit shaft of hanger enclosure interior, limit
Limit torsional spring is installed on axis, by reasonable combination torsional spring and the elastic force of tension spring, guarantees direction of rotation and the activity model of hook
It encloses.
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 the utility model assembled state；
Rearview under Fig. 4 the utility model assembled state；
The schematic perspective view of Fig. 5 the utility model Rocker arm section；
The schematic perspective view of Fig. 6 the utility model hook portion；
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
The following describes the utility model in further detail with reference to the accompanying drawings.
Referring to Fig. 1-2, the utility model unmanned plane weapon carrier 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 and action process of the utility model 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 above is only the preferred embodiment of the present invention, not to do in any form to the utility model
It limits, it will be apparent to a skilled person that this is practical new under conditions of not departing from the spirit of the present invention and principle
Type can also carry out several modifications or simple replacement, these modifications and replacement also each fall within the model delimited by submitted claim
Within enclosing.
Claims (8)
1. a kind of rotating electromagnet controls unmanned plane weapon carrier, it is characterised in that: including hanger shell, the bottom surface of hanger shell
Front support (21) and tail-bracket (20) are respectively set along the rear and front end of guided missile installation direction, front support (21) and tail-bracket (20)
Between be equipped with hook (13) for connecting guided missile lifting lug, the hook axis of hanger enclosure interior is mounted in the middle part of hook (13)
(16) on, hanger enclosure interior is provided with rotating electromagnet (3), and rotating electromagnet (3) is able to drive driver plate (4) and is rotated,
Driver plate (4) is connect by connecting rod (5) with the scotch (6) that can be pivoted；The tail portion for linking up with (13) is installed by latch cam
(15), latch cam (15) is matched with the rocker arm (10) that can be pivoted, one end connecting rocker arm axis (12) of rocker arm (10),
The other end installs rocker cam (9)；Scotch (6) is matched with rocker cam (9), and scotch (6) passes through rocker cam (9) band
Shake arm (10) rotation, rocker arm (10) drives hook (13) rotation by latch cam (15).
2. rotating electromagnet according to claim 1 controls unmanned plane weapon carrier, it is characterised in that: the scotch
(6) it is mounted in the braking roll (8) of hanger enclosure interior, stop torsional spring (7) is installed in braking roll (8).
3. rotating electromagnet according to claim 1 controls unmanned plane weapon carrier, it is characterised in that: the rocker arm shaft
(12) it is mounted on the inside of hanger shell, rocking arm torsional spring (11) are installed on rocker arm shaft (12).
4. rotating electromagnet according to claim 1 controls unmanned plane weapon carrier, it is characterised in that: the hook (13)
Middle part be connected with the tension spring (14) in the portion that is immobilized in the shell, hook (13) will overcome the pulling force of tension spring (14) when opening.
5. rotating electromagnet according to claim 1 controls unmanned plane weapon carrier, it is characterised in that: the hanger shell
Body is internally provided with limited block (17), and the baffle matched with the gib head of hook (13) is provided on limited block (17).
6. rotating electromagnet according to claim 5 controls unmanned plane weapon carrier, it is characterised in that: the limited block
(17) it is mounted on the limit shaft (19) of hanger enclosure interior, limit torsional spring (18) is installed on limit shaft (19).
7. rotating electromagnet according to claim 1 controls unmanned plane weapon carrier, it is characterised in that: the hanger shell
Body is internally provided with electromagnet stent (2), and rotating electromagnet (3) is mounted on electromagnet stent (2).
8. rotating electromagnet according to claim 1 controls unmanned plane weapon carrier, it is characterised in that: the front support
(21) it is equipped on 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 |
|---|---|---|---|
| CN201920116805.0U CN209553513U (en) | 2019-01-23 | 2019-01-23 | A kind of rotating electromagnet control unmanned plane weapon carrier |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920116805.0U CN209553513U (en) | 2019-01-23 | 2019-01-23 | A kind of rotating electromagnet control unmanned plane weapon carrier |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209553513U true CN209553513U (en) | 2019-10-29 |
Family
ID=68307238
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920116805.0U Active CN209553513U (en) | 2019-01-23 | 2019-01-23 | A kind of rotating electromagnet control unmanned plane weapon carrier |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209553513U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109760841A (en) * | 2019-01-23 | 2019-05-17 | 西安深瞳智控技术有限公司 | A kind of small drone weapon carrier |
| CN112407287A (en) * | 2021-01-25 | 2021-02-26 | 西安富沃德光电科技有限公司 | Missile hanging rack and using method thereof |
-
2019
- 2019-01-23 CN CN201920116805.0U patent/CN209553513U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109760841A (en) * | 2019-01-23 | 2019-05-17 | 西安深瞳智控技术有限公司 | A kind of small drone weapon carrier |
| CN109760841B (en) * | 2019-01-23 | 2024-01-26 | 西安深瞳智控技术有限公司 | Small unmanned aerial vehicle weapon stores pylon |
| CN112407287A (en) * | 2021-01-25 | 2021-02-26 | 西安富沃德光电科技有限公司 | Missile hanging rack and using method thereof |
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 | |
| CN110271669B (en) | Fire control disaster relief unmanned aerial vehicle | |
| CN217198654U (en) | Unmanned aerial vehicle machine carries system of throwing | |
| CN210310886U (en) | Unmanned aerial vehicle for fire control and disaster relief | |
| CN208216982U (en) | Equip with arms unmanned helicopter | |
| CN217836033U (en) | Fire extinguishing bomb launcher based on unmanned aerial vehicle | |
| CN209479991U (en) | The cold hairdo multitube bomb rack control of unmanned plane | |
| CN217032188U (en) | Small-size hand-held type pneumatic fire extinguishing bomb jettison device | |
| CN209230422U (en) | It increases rain artificially hail-suppression rocket bullet storage and conveying box | |
| CN111141173B (en) | Unmanned aerial vehicle carries rifle | |
| CN113428365B (en) | Unmanned aerial vehicle firearms carry structure | |
| CN109927916A (en) | A kind of military aircraft composite material radome fairing | |
| CN108327897A (en) | Equip with arms unmanned helicopter | |
| CN114537669A (en) | Unmanned aerial vehicle machine carries system of throwing | |
| RU2703695C1 (en) | Armored facility armored compartment | |
| CN113959256B (en) | Protective missile launching box and remote control weapon station | |
| CN207631498U (en) | A kind of unmanned plane bomb droping gear | |
| CN219277812U (en) | Can section of thick bamboo shoot horizontal folding unmanned aerial vehicle | |
| CN214267981U (en) | Automatic expansion device based on unmanned aerial vehicle parachute | |
| CN113120251B (en) | Air-jet unmanned aerial vehicle launching tube | |
| CN219927968U (en) | Built-in weapon stores pylon system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |