CN217673258U - Be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure - Google Patents
Be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure Download PDFInfo
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- CN217673258U CN217673258U CN202220871739.XU CN202220871739U CN217673258U CN 217673258 U CN217673258 U CN 217673258U CN 202220871739 U CN202220871739 U CN 202220871739U CN 217673258 U CN217673258 U CN 217673258U
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- Prior art keywords
- camera
- zoom
- aerial vehicle
- unmanned aerial
- connecting rod
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- 230000007246 mechanism Effects 0.000 claims abstract description 26
- 230000008878 coupling Effects 0.000 claims abstract description 19
- 238000010168 coupling process Methods 0.000 claims abstract description 19
- 238000005859 coupling reaction Methods 0.000 claims abstract description 19
- 125000003003 spiro group Chemical group 0.000 claims description 3
- 238000009434 installation Methods 0.000 abstract description 4
- 230000005693 optoelectronics Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
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Abstract
The utility model discloses a be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure in unmanned air vehicle technical field, including coupling mechanism, connecting rod, adjustment mechanism and camera, adjustment mechanism with the camera is connected to adjust the camera, connecting rod one end detachable connects in the coupling mechanism, the other end with adjustment mechanism connects. In this scheme, the cartridge through the connecting rod is inside the casing for load and unload between pothook and the fixture block, the installation is dismantled fast and conveniently, has improved the dismouting efficiency of aircraft bottom nacelle greatly. Simultaneously, slide in the sliding sleeve through the slide bar, can adjust the distance between camera and the aircraft.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is a be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure.
Background
The fuselage of aircraft is hung with photoelectric equipment such as visible light camera, infrared camera for work such as aerial photography, aim, monitoring or pursuit, according to the difference of work content, has to carry out debugging or change to the photoelectric equipment of fuselage mounting, that just means need repeatedly dismantle and assemble between fuselage and the photoelectric equipment. At present, the aircraft is mainly connected fuselage and optoelectronic device through a plurality of screws, need lock repeatedly or unscrew the screw, and the operation is inconvenient and the cost is long, and work efficiency is low.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure to solve the problem that the optoelectronic device cost time is long is connected to the aircraft that proposes in the above-mentioned background art.
In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides a be used for military police unmanned aerial vehicle zooming nacelle rapid disassembly structure, includes coupling mechanism, connecting rod, adjustment mechanism and camera, adjustment mechanism with the camera is connected to adjust the camera, connecting rod one end detachable connect in the coupling mechanism, the other end with adjustment mechanism connects.
Preferably, the connecting mechanism comprises a mounting plate, a casing, a spring, a push rod and a wedge-shaped clamping block, the push rod is slidably matched in the casing, the clamping block is fixedly connected to the push rod, one end of the connecting rod is fixedly connected with the wedge-shaped clamping hook, the clamping hook is matched with the clamping block, the spring is fixedly connected in the casing, and one end of the spring is fixedly connected to the clamping block.
Preferably, the adjusting mechanism comprises a sliding rod, a U-shaped mounting rack is fixedly connected to the sliding rod, a bolt is screwed to the mounting rack, a non-slip mat is fixedly connected to one end of the bolt, the camera is located inside the mounting rack, and the non-slip mat is abutted to the outer wall of the camera.
Preferably, the connecting rod is fixedly connected with a sliding sleeve, the sliding rod is slidably matched in the sliding sleeve, and the sliding sleeve is screwed with a screw.
Compared with the prior art, the beneficial effects of the utility model are that: in this scheme, adopt above-mentioned structural style, cartridge through the connecting rod is inside the casing for load and unload between pothook and the fixture block, the installation is dismantled fast and conveniently, has improved the dismouting efficiency of aircraft bottom nacelle greatly. Simultaneously, slide in the sliding sleeve through the slide bar, can adjust the distance between camera and the aircraft.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is the utility model discloses military police unmanned aerial vehicle zooms nacelle rapid disassembly structure's schematic diagram.
Fig. 2 is the utility model is used for military police unmanned aerial vehicle zooms nacelle rapid disassembly structure local structure sketch map.
Figure 3 is the utility model discloses a top view that is used for military police unmanned aerial vehicle zoom nacelle quick detach structure chart 2.
Fig. 4 isbase:Sub>A sectional view of the utility model used for military police unmanned aerial vehicle zoom nacelle quick detach structure 3 from thebase:Sub>A-base:Sub>A direction.
In the drawings, the reference numbers indicate the following list of parts:
1. mounting a plate; 2. a housing; 3. a connecting rod; 301. a hook; 4. a sliding sleeve; 5. a screw; 6. a clamping block; 7. a spring; 8. a push rod; 9. a slide bar; 10. a mounting frame; 11. a bolt; 12. a non-slip mat; 13. a camera is provided.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person skilled in the art without making creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-4, the present invention provides a technical solution: the utility model provides a be used for military affairs unmanned aerial vehicle to zoom nacelle rapid disassembly structure, includes coupling mechanism, connecting rod 3, adjustment mechanism and camera 13, and adjustment mechanism is connected with camera 13 to adjust camera 13, 3 one end detachable of connecting rod are connected in coupling mechanism, and the other end is connected with adjustment mechanism.
The connecting mechanism comprises an installation plate 1, a shell 2, a spring 7, a push rod 8 and a wedge-shaped fixture block 6, the push rod 8 is slidably matched in the shell 2, the fixture block 6 is fixedly connected on the push rod 8, one end of the connecting rod 3 is fixedly connected with a wedge-shaped fixture hook 301, the fixture hook 301 is matched with the fixture block 6, the spring 7 is fixedly connected in the shell 2, and one end of the spring 7 is fixedly connected on the fixture block 6.
The mounting plate 1 is provided with a mounting hole, so that the mounting plate can be connected to an aircraft, the shell 2 is connected with the mounting plate 1, the push rod 8 and the clamping block 6 can be mounted, the inclined plane of the clamping hook 301 is abutted to the inclined plane of the clamping block 6 during mounting, after force application, the clamping block 6 slides and compresses the spring 7, after the clamping block 6 is clamped in the clamping hook 301, the clamping block 6 is inserted into the clamping hook 301 under the elastic action of the spring 7, and the clamping hook 301 is limited to prevent the clamping hook 301 from falling off.
The rigid coupling has sliding sleeve 4 on connecting rod 3, the cooperation of slide bar 9 slidable is in sliding sleeve 4, the spiro union has screw 5 on sliding sleeve 4, adjustment mechanism includes slide bar 9, the rigid coupling has the mounting bracket 10 of U-shaped on slide bar 9, the spiro union has bolt 11 on the mounting bracket 10, bolt 11 serves the rigid coupling to have slipmat 12, camera 13 is located inside the mounting bracket 10, slipmat 12 supports and leans on camera 13 outer wall, connecting rod 3 and pothook 301 rigid coupling, in order to fix sliding sleeve 4, slide bar 9 can slide in the sliding sleeve, in order to adjust the height of the camera 13 of bottom, can lock the position of slide bar 9 through screw 5.
In this scheme, adopt above-mentioned structural style, the cartridge through connecting rod 3 is inside casing 2 for load and unload between pothook 301 and the fixture block 6, the installation is dismantled fast and conveniently, has improved the dismouting efficiency of aircraft bottom nacelle greatly. Meanwhile, the distance between the camera 13 and the aircraft can be adjusted by sliding the sliding rod 9 in the sliding sleeve 4.
In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, to thereby enable others skilled in the art to best understand the invention for and utilize the invention. The present invention is limited only by the claims and their full scope and equivalents.
Claims (4)
1. The utility model provides a be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure which characterized in that: including coupling mechanism, connecting rod (3), adjustment mechanism and camera (13), adjustment mechanism with camera (13) are connected to adjust camera (13), connecting rod (3) one end detachable connects in the coupling mechanism, the other end with adjustment mechanism connects.
2. The quick-release structure for the zoom pod of the military police unmanned aerial vehicle as claimed in claim 1, wherein: coupling mechanism includes mounting panel (1), casing (2), spring (7), push rod (8) and wedge-shaped fixture block (6), push rod (8) slidable cooperation is in casing (2), fixture block (6) rigid coupling is in on push rod (8), connecting rod (3) one end rigid coupling has wedge-shaped pothook (301), pothook (301) with fixture block (6) phase-match, spring (7) rigid coupling is in casing (2), the one end rigid coupling of spring (7) is in on fixture block (6).
3. The quick-release structure for the zoom pod of the military police unmanned aerial vehicle as claimed in claim 2, wherein: adjustment mechanism includes slide bar (9), the rigid coupling has mounting bracket (10) of U-shaped on slide bar (9), the spiro union has bolt (11) on mounting bracket (10), bolt (11) serve the rigid coupling have slipmat (12), camera (13) are located inside mounting bracket (10), slipmat (12) support and lean on camera (13) outer wall.
4. The quick-release structure for the zoom pod of the military police unmanned aerial vehicle as claimed in claim 3, wherein: the sliding rod (9) is slidably matched in the sliding sleeve (4), and a screw (5) is connected to the sliding sleeve (4) in a threaded manner.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220871739.XU CN217673258U (en) | 2022-04-15 | 2022-04-15 | Be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220871739.XU CN217673258U (en) | 2022-04-15 | 2022-04-15 | Be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217673258U true CN217673258U (en) | 2022-10-28 |
Family
ID=83733578
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220871739.XU Expired - Fee Related CN217673258U (en) | 2022-04-15 | 2022-04-15 | Be used for military police unmanned aerial vehicle to zoom nacelle rapid disassembly structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217673258U (en) |
-
2022
- 2022-04-15 CN CN202220871739.XU patent/CN217673258U/en not_active Expired - Fee Related
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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: 20221028 |