CN205381412U - Unmanned aerial vehicle mission equipment quick assembly disassembly device - Google Patents
Unmanned aerial vehicle mission equipment quick assembly disassembly device Download PDFInfo
- Publication number
- CN205381412U CN205381412U CN201620113799.XU CN201620113799U CN205381412U CN 205381412 U CN205381412 U CN 205381412U CN 201620113799 U CN201620113799 U CN 201620113799U CN 205381412 U CN205381412 U CN 205381412U
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- secure component
- fixed
- unmanned plane
- fixing housing
- aerial vehicle
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- 238000009434 installation Methods 0.000 claims abstract description 10
- 210000000078 claw Anatomy 0.000 claims description 5
- 230000000694 effects Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005474 detonation Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle mission equipment quick assembly disassembly device, including fixed subassembly and activity subassembly, fixed subassembly passes through the screw connection to be fixed in unmanned aerial vehicle's bottom, and the cloud platform is fixed on the activity subassembly through the screw connection, fixed subassembly includes fixed casing, a clamping unit and presses the key cap, the set casing is internal to set up columniform installation cavity, and the lateral wall of fixed casing runs through and sets up a clamping unit mounting groove, the clamping unit mounting groove communicates with each other with the installation cavity, passes through screw fixed connection according to key cap and clamping unit, sets up a long circle groove on the top surface of fixed casing. The utility model discloses be used in on the unmanned aerial vehicle to realize the quick assembly disassembly between cloud platform and the unmanned aerial vehicle, on this cloud platform quick assembly disassembly device also can be used in other equipment certainly, for example car, security protection equipment etc, the utility model discloses can accurate arrival target location and can automatic fastening, dismantle convenience, easy operation, nimble practicality, good reliability.
Description
Technical field
This utility model relates to the fields such as unmanned plane, automobile, security protection, is specifically related to a kind of unmanned plane task device rapid dismounting apparatus.
Background technology
Increasingly mature along with unmanned air vehicle technique, the different field such as UAV flight's different task equipment extensive use mapping, security monitoring, fire-fighting, movies-making, power-line patrolling.UAV flight's each task equipment in such applications, performs different tasks.
Generally for convenient transportation, unmanned plane task device is all just be installed on unmanned plane before execution task, screw is mostly adopted to be locked between the two, existing assembling structure needs more time in installation process, dismantle trouble simultaneously, therefore it is unfavorable for that unmanned plane quickly performs task, and task switching etc..
Summary of the invention
Technical problem to be solved in the utility model is to provide and a kind of solves task device of the prior art assembling structure unmanned plane task device rapid dismounting apparatus of technical problem of complex operation, required time length when installation and removal.
This utility model is achieved through the following technical solutions: a kind of unmanned plane task device rapid dismounting apparatus, including fixation kit and moving component, described fixation kit is connected by screw the bottom being fixed on unmanned plane, and The Cloud Terrace is connected by screw and is fixed on moving component；
Described fixation kit includes a fixing housing, secure component and button cap, the installation cavity of one cylinder is set in described set casing body, the sidewall of fixing housing runs through and arranges a secure component mounting groove, described secure component mounting groove communicates with installing cavity, button cap is connected by screw is fixing with secure component, arranging an oval-shaped slot on the end face of fixing housing, the upper part of screw is embedded in the oval-shaped slot of fixing housing so that have an extreme position when secure component is moved to the left；
The sidewall of the right-hand end of secure component and fixing housing offsets so that have an extreme position when secure component moves right, and the end face lower surface of fixing housing is provided with two guide pin bushings；
Being provided with two springs in the open slot of fixing housing, one end of spring and open slot bottom surface offset, and the other end of spring and secure component offset；
Described moving component includes a movable housing, and the upper surface of described movable housing offers a circle rubber draw-in groove, installs a rubber ring in rubber draw-in groove.
As preferred technical scheme, two guide pin bushing positions of fixing housing are just correspondingly arranged on guide pillar by the upper surface of described movable housing, and guide pillar coordinates installation with guide pin bushing.
As preferred technical scheme, the upper surface of described movable housing is also equipped with two cantilevers, the claw that secure component upper end is just being arranged by cantilever.
As preferred technical scheme, described rubber ring is bonded in rubber draw-in groove by gum.
The beneficial effects of the utility model are: this utility model patent effectively solve in force existing unmanned plane moving component can not accurately install put in place, can not the problem of automatic fastening.This utility model patent can accurately arrive target location energy automatic fastening；When removing moving component, this utility model patent can realize the dismounting of moving component easily and quickly.This utility model improves the dismounting efficiency of unmanned plane moving component, convenient disassembly, practicality simple to operate, flexible, highly reliable.
Accompanying drawing explanation
In order to be illustrated more clearly that this utility model embodiment or technical scheme of the prior art, the accompanying drawing used required in embodiment or description of the prior art will be briefly described below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the premise not paying creative work, it is also possible to obtain other accompanying drawing according to these accompanying drawings.
Fig. 1 is the overall structure schematic diagram of fixation kit of the present utility model；
Fig. 2 is the overall structure schematic diagram of moving component of the present utility model；
Fig. 3 is the detonation configuration schematic diagram of fixation kit of the present utility model；
Fig. 4 is the detonation configuration schematic diagram of moving component of the present utility model；
Fig. 5 is overall package schematic diagram of the present utility model.
Detailed description of the invention
All features disclosed in this specification, or the step in disclosed all methods or process, except mutually exclusive feature and/or step, all can combine by any way.
This specification (include any accessory claim, summary and accompanying drawing) disclosed in any feature, unless specifically stated otherwise, all can by other equivalences or there is the alternative features of similar purpose replaced.That is, unless specifically stated otherwise, each feature is an example in a series of equivalence or similar characteristics.
As Figure 1-Figure 5, a kind of unmanned plane task device rapid dismounting apparatus of the present utility model, including fixation kit 20 and moving component 30, described fixation kit 20 is connected by screw the bottom being fixed on unmanned plane, and The Cloud Terrace is connected by screw and is fixed on moving component 30；
Described fixation kit includes a fixing housing 1, secure component 2 and button cap 3, the installation cavity of one cylinder is set in described fixing housing 1, the sidewall of fixing housing 1 runs through and arranges a secure component mounting groove, described secure component mounting groove communicates with installing cavity, button cap 3 is connected by screw 5 is fixing with secure component 2, the end face of fixing housing 1 arranges an oval-shaped slot, the upper part of screw 5 is embedded in the oval-shaped slot of fixing housing 1 so that secure component 2 has an extreme position when being moved to the left；
The sidewall of the right-hand end of secure component 2 and fixing housing 1 offsets so that secure component 2 has an extreme position when moving right, and the end face lower surface of fixing housing is provided with two guide pin bushings；
Being provided with two springs 4 in the open slot of fixing housing 1, one end of spring 4 and open slot bottom surface offset, and the other end of spring 4 and secure component offset；
Described moving component 2 includes a movable housing 7, and the upper surface of described movable housing 7 offers a circle rubber draw-in groove, installs a rubber ring 6 in rubber draw-in groove.
In the present embodiment, two guide pin bushing 10 positions of fixing housing 1 are just correspondingly arranged on guide pillar 11 by the upper surface of movable housing 7, and guide pillar 11 coordinates installation with guide pin bushing 10.
In the present embodiment, the upper surface of movable housing 7 is also equipped with two cantilevers 9, the claw 8 that secure component upper end is just being arranged by cantilever 9.
In the present embodiment, rubber ring 6 is bonded in rubber draw-in groove by gum.
During installation activity assembly, connecting the moving component of task apparatus by spacing guide pillar, the bottom-up entrance fixation kit of guide sleeve structure, secure component is first backed down toward vertical direction and compresses spring simultaneously by the cantilever on movable housing.Moving component continues up movement and is compressed by rubber ring a certain amount of again, namely installs and puts in place.Now, secure component its claw of resilience under the action of the spring blocks the cantilever on movable housing, can be fastened by moving component.
During dismounting moving component, secure component is moved right a stroke preset by the cap that presses & hold, and claw departs from the cantilever on movable housing, can dismantle downwards moving component.
It is further to note that this utility model cannot be only used for unmanned plane, it is also possible in automobile, security device etc., without limitation.
The beneficial effects of the utility model are: this utility model patent effectively solve in force existing unmanned plane moving component can not accurately install put in place, can not the problem of automatic fastening.This utility model patent can accurately arrive target location energy automatic fastening；When removing moving component, this utility model patent can realize the dismounting of moving component easily and quickly.This utility model improves the dismounting efficiency of unmanned plane moving component, convenient disassembly, practicality simple to operate, flexible, highly reliable.
The above, be only detailed description of the invention of the present utility model, but protection domain of the present utility model be not limited thereto, any change expected without creative work or replacement, all should be encompassed within protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with claims protection defined.
Claims (4)
1. a unmanned plane task device rapid dismounting apparatus, it is characterised in that: including fixation kit and moving component, described fixation kit is connected by screw the bottom being fixed on unmanned plane, and The Cloud Terrace is connected by screw and is fixed on moving component；
Described fixation kit includes a fixing housing, secure component and button cap, the installation cavity of one cylinder is set in described set casing body, the sidewall of fixing housing runs through and arranges a secure component mounting groove, described secure component mounting groove communicates with installing cavity, button cap is connected by screw is fixing with secure component, arranging an oval-shaped slot on the end face of fixing housing, the upper part of screw is embedded in the oval-shaped slot of fixing housing so that have an extreme position when secure component is moved to the left；
The sidewall of the right-hand end of secure component and fixing housing offsets so that have an extreme position when secure component moves right, and the end face lower surface of fixing housing is provided with two guide pin bushings；
Being provided with two springs in the open slot of fixing housing, one end of spring and open slot bottom surface offset, and the other end of spring and secure component offset；
Described moving component includes a movable housing, and the upper surface of described movable housing offers a circle rubber draw-in groove, installs a rubber ring in rubber draw-in groove.
2. unmanned plane task device rapid dismounting apparatus according to claim 1, it is characterised in that: two guide pin bushing positions of fixing housing are just correspondingly arranged on guide pillar by the upper surface of described movable housing, and guide pillar coordinates installation with guide pin bushing.
3. unmanned plane task device rapid dismounting apparatus according to claim 1, it is characterised in that: the upper surface of described movable housing is also equipped with two cantilevers, the claw that secure component upper end is just being arranged by cantilever.
4. unmanned plane task device rapid dismounting apparatus according to claim 1, it is characterised in that: described rubber ring is bonded in rubber draw-in groove by gum.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620113799.XU CN205381412U (en) | 2016-02-04 | 2016-02-04 | Unmanned aerial vehicle mission equipment quick assembly disassembly device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620113799.XU CN205381412U (en) | 2016-02-04 | 2016-02-04 | Unmanned aerial vehicle mission equipment quick assembly disassembly device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205381412U true CN205381412U (en) | 2016-07-13 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620113799.XU Expired - Fee Related CN205381412U (en) | 2016-02-04 | 2016-02-04 | Unmanned aerial vehicle mission equipment quick assembly disassembly device |
Country Status (1)
| Country | Link |
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| CN (1) | CN205381412U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107013913A (en) * | 2017-05-11 | 2017-08-04 | 国网江苏省电力公司苏州供电公司 | Quickly dismantled flame projector and apply its high-voltage line barrier clearing device |
-
2016
- 2016-02-04 CN CN201620113799.XU patent/CN205381412U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107013913A (en) * | 2017-05-11 | 2017-08-04 | 国网江苏省电力公司苏州供电公司 | Quickly dismantled flame projector and apply its high-voltage line barrier clearing device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170313 Address after: 518000 Guangdong Province, Shenzhen City Shilong Baoan District Shiyan Street Community Yihe Road No. 1 Corbett aviation science and Technology Park Building 3 (Yuan Jin Dahua Industrial Zone) Patentee after: Bit science and technology of aviation Co., Ltd of section of Shenzhen Address before: 518000 A District, R2 District, Nanshan District high tech park, Guangdong, Shenzhen, China Patentee before: Liu Wei |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20171012 Address after: Jiaxing City, Zhejiang province Jiashan County 314100 street to Luoxing Valley Park Business Center D block 4 Building Patentee after: Zhejiang kebit Technology Co. Ltd. Address before: 518000 Guangdong Province, Shenzhen City Shilong Baoan District Shiyan Street Community Yihe Road No. 1 Corbett aviation science and Technology Park Building 3 (Yuan Jin Dahua Industrial Zone) Patentee before: Bit science and technology of aviation Co., Ltd of section of Shenzhen |
|
| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160713 Termination date: 20210204 |
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| CF01 | Termination of patent right due to non-payment of annual fee |