CN205010496U - Unmanned aerial vehicle umbrella cabin spiral -lock is put - Google Patents
Unmanned aerial vehicle umbrella cabin spiral -lock is put Download PDFInfo
- Publication number
- CN205010496U CN205010496U CN201520651687.5U CN201520651687U CN205010496U CN 205010496 U CN205010496 U CN 205010496U CN 201520651687 U CN201520651687 U CN 201520651687U CN 205010496 U CN205010496 U CN 205010496U
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- CN
- China
- Prior art keywords
- bracing frame
- parachute
- control module
- attaching parts
- stay bearing
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- Expired - Fee Related
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Abstract
The utility model aims at providing an unmanned aerial vehicle umbrella cabin spiral -lock is put, including backup pad, parachute -opening control module, first support frame, coil, transmission, safe round pin, second support frame, connecting piece, third support frame, safe pinhole, spring, limiting plate, round hole, parachute -opening control module accessible looper drive transmission, transmission then drive the safe clockwise motion of selling, and safe round pin is extracted in safe pinhole, and the limiting plate then upwards pops out under the effect of both ends spring, and umbrella cabin spiral -lock is put promptly for opening, the beneficial effect of the utility model: adopt the drive of parachute -opening control module through coil transmission, that has realized that umbrella cabin spiral -lock puts opens fast, provides the sound assurance for unmanned aerial vehicle's harmless parachuting.
Description
Technical field
The utility model relates to unmanned aircraft parachute descent and reclaims field, particularly relates to a kind of unmanned plane umbrella cabin buckle device.
Background technology
Unmanned plane is driverless operation on a kind of machine, by radio telecommand or automatic program control flight, and reusable aerocraft.Unmanned plane range of use is very wide, has widened military, the civilian and large field of scientific research three.Because demand constantly expands, the requirement reducing unmanned plane cost improves constantly, can be safe and reliable harmless recovery is carried out to unmanned plane, realize unmanned plane and repeatedly use, also become the important indicator evaluating unmanned plane performance.Parachuting is reclaimed, and as one of common unmanned plane way of recycling, is control to open the parachute carried above unmanned plane during flying to recovery area to slow down, and drops to the way of recycling in the region of specifying.This way of recycling safety simple to operate, is mainly used in reclaiming middle-size and small-size unmanned plane.
The utility model provides a kind of unmanned plane umbrella cabin buckle device, adopts parachute-opening control module to be driven through coil driving device, achieves the quick unlatching of umbrella cabin buckle device, for the harmless parachuting of unmanned plane provides sound assurance.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane umbrella cabin buckle structure that can open fast.
The technical solution of the utility model is: a kind of unmanned plane umbrella cabin buckle device, it is characterized in that: comprise stay bearing plate, parachute-opening control module, first bracing frame, coil, driving device, safety pin, second bracing frame, attaching parts, 3rd bracing frame, safe pin-and-hole, spring, positioning plate, described parachute-opening control module is positioned at stay bearing plate side, described parachute-opening control module is fixedly linked by the first bracing frame and stay bearing plate, described driving device is positioned at the top of described parachute-opening control module, described parachute-opening control module can drive transmission by coil, described driving device is connected with safety pin, described driving device can drive safety pin clockwise movement, described second bracing frame is positioned at the upside of the first bracing frame, described second bracing frame and stay bearing plate are fixedly linked, described safety pin passes across the second bracing frame and is connected with attaching parts with stay bearing plate, described attaching parts is positioned at the opposite side of stay bearing plate, safe pin-and-hole is provided with below described attaching parts, described safety pin and safe pin-and-hole fasten, described positioning plate is positioned at the top of attaching parts, described positioning plate and attaching parts are fixedly linked, described 3rd bracing frame is positioned at the below of attaching parts, described 3rd bracing frame and stay bearing plate are fixedly linked, described 3rd bracing frame two ends are provided with spring, described spring is connected with positioning plate by attaching parts.
Further, described driving device comprises hinge axis, drive link, rocking arm, and described drive link is connected with brace table by hinge axis, and described rocking arm is connected with drive link by set pin.
Further, on described stay bearing plate and the second bracing frame, correspondence position offers a circular hole.
Further, described safety pin is inserted in safe pin-and-hole by circular hole.
Further, described number of springs is two.
The beneficial effects of the utility model are: adopt technique scheme, and parachute-opening control module, by coil drive driving device, can realize the quick unlatching of umbrella cabin buckle device, provide sound assurance for unmanned plane can't harm parachuting.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is lateral plan of the present utility model;
Fig. 3 is the front view of attaching parts of the present utility model.
Wherein:
1, stay bearing plate 2, parachute-opening control module 3, first bracing frame 4, coil
5, driving device 6, hinge axis 7, drive link 8, rocking arm
9, safety pin 10, second bracing frame 11, attaching parts 12, safe pin-and-hole
13, positioning plate 14, the 3rd bracing frame 15, spring 16, circular hole
Detailed description of the invention
Below in conjunction with accompanying drawing, brief description is made to detailed description of the invention of the present utility model.
As shown in Figure 1, a kind of unmanned plane parachute cabin buckle structure, it is characterized in that: comprise stay bearing plate 1, parachute-opening control module 2, first bracing frame 3, coil 4, driving device 5, hinge axis 6, drive link 7, rocking arm 8, safety pin 9, second bracing frame 10, attaching parts 11, safe pin-and-hole 12, positioning plate 13, 3rd bracing frame 14, spring 15, circular hole 16, described parachute-opening control module 2 is positioned at stay bearing plate 1 side, described parachute-opening control module 2 is fixedly linked with stay bearing plate 1 by the first bracing frame 3, described driving device 5 is positioned at the top of described parachute-opening control module 2, described parachute-opening control module 2 is by coil 4 drive transmission 5, described driving device 5 is connected with safety pin 9, described driving device 5 can drive safety pin 9 clockwise movement, described second bracing frame 10 is positioned at the upside of the first bracing frame 3, described second bracing frame 10 is fixedly linked with stay bearing plate 1, described safety pin 9 passes across the second bracing frame 10 and is connected with attaching parts 11 with stay bearing plate 1, described attaching parts 11 is positioned at the opposite side of stay bearing plate 1, described attaching parts 11 is provided with safe pin-and-hole 12, described safety pin 9 fastens with safe pin-and-hole 12, described positioning plate 13 is positioned at the top of attaching parts 11, described positioning plate 13 is fixedly linked with attaching parts 11, described 3rd bracing frame 14 is positioned at the below of attaching parts 11, described 3rd bracing frame 14 is fixedly linked with stay bearing plate 1, described 3rd bracing frame 14 two ends are provided with spring 15, described spring 15 is connected with positioning plate 13 by attaching parts 11, described driving device 5 comprises hinge axis 6, drive link 7, rocking arm 8, described drive link 7 is connected with brace table by hinge axis 6, described rocking arm 8 is fixedly linked with drive link 7, on described stay bearing plate 1 and the second bracing frame 10, correspondence position all offers a circular hole 16, described safety pin 9 to be inserted in safe pin-and-hole 12 by circular hole 16, the quantity of described spring 15 is two.
Mode of operation: when unmanned plane needs parachuting, operating personal utilizes long-range control setup to send wireless control signal, after parachute-opening control module receives wireless control signal, parachute-opening control module 2 is by coil 4 drive transmission 5, driving device 5 can drive safety pin 9 to do clockwise movement, and safety pin 9 12 to be extracted in safe pin-and-hole, and positioning plate 13 pops up under the effect of two ends spring 15, now umbrella cabin buckle device is opened, and can release a parachute and land.
Above an embodiment of the present utility model has been described in detail, but described content being only preferred embodiment of the present utility model, can not being considered to for limiting practical range of the present utility model.All equalizations done according to the utility model application range change and improve, and all should still belong within patent covering scope of the present utility model.
Claims (5)
1. a unmanned plane umbrella cabin buckle device, it is characterized in that: comprise stay bearing plate, parachute-opening control module, first bracing frame, coil, driving device, safety pin, second bracing frame, attaching parts, 3rd bracing frame, safe pin-and-hole, spring, positioning plate, described parachute-opening control module is positioned at stay bearing plate side, described parachute-opening control module is fixedly linked by the first bracing frame and stay bearing plate, described driving device is positioned at the top of described parachute-opening control module, described parachute-opening control module can drive transmission by coil, described driving device is connected with safety pin, described driving device can drive safety pin clockwise movement, described second bracing frame is positioned at the upside of the first bracing frame, described second bracing frame and stay bearing plate are fixedly linked, described safety pin passes across the second bracing frame and is connected with attaching parts with stay bearing plate, described attaching parts is positioned at the opposite side of stay bearing plate, safe pin-and-hole is provided with below described attaching parts, described safety pin and safe pin-and-hole fasten, described positioning plate is positioned at the top of attaching parts, described positioning plate and attaching parts are fixedly linked, described 3rd bracing frame is positioned at the below of attaching parts, described 3rd bracing frame and stay bearing plate are fixedly linked, described 3rd bracing frame two ends are provided with spring, described spring is connected with positioning plate by attaching parts.
2. a kind of unmanned plane umbrella cabin buckle device according to claim 1, it is characterized in that: described driving device comprises hinge axis, drive link, rocking arm, described drive link is connected with brace table by hinge axis, and described rocking arm and drive link are fixedly linked.
3. a kind of unmanned plane umbrella cabin buckle device according to claim 1, is characterized in that: on described stay bearing plate and the second bracing frame, correspondence position all offers a circular hole.
4. a kind of unmanned plane umbrella cabin buckle device according to claim 1 or claim 3, is characterized in that: described safety pin is inserted in safe pin-and-hole by circular hole.
5. a kind of unmanned plane umbrella cabin buckle device according to claim 1, is characterized in that: described number of springs is two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520651687.5U CN205010496U (en) | 2015-08-26 | 2015-08-26 | Unmanned aerial vehicle umbrella cabin spiral -lock is put |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520651687.5U CN205010496U (en) | 2015-08-26 | 2015-08-26 | Unmanned aerial vehicle umbrella cabin spiral -lock is put |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205010496U true CN205010496U (en) | 2016-02-03 |
Family
ID=55209110
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520651687.5U Expired - Fee Related CN205010496U (en) | 2015-08-26 | 2015-08-26 | Unmanned aerial vehicle umbrella cabin spiral -lock is put |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205010496U (en) |
-
2015
- 2015-08-26 CN CN201520651687.5U patent/CN205010496U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160203 Termination date: 20210826 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |