CN206202710U - A kind of unmanned plane task device rapid dismounting apparatus - Google Patents
A kind of unmanned plane task device rapid dismounting apparatus Download PDFInfo
- Publication number
- CN206202710U CN206202710U CN201621079847.4U CN201621079847U CN206202710U CN 206202710 U CN206202710 U CN 206202710U CN 201621079847 U CN201621079847 U CN 201621079847U CN 206202710 U CN206202710 U CN 206202710U
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- Prior art keywords
- fixed shell
- secure component
- unmanned plane
- fixed
- component
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- 238000009434 installation Methods 0.000 claims abstract description 8
- 210000000078 claw Anatomy 0.000 claims description 5
- 230000005611 electricity Effects 0.000 claims description 2
- 239000007787 solid Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 5
- 230000000694 effects Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned plane task device rapid dismounting apparatus, including fixation kit and movable component, the fixation kit is connected by screw the bottom for being fixed on unmanned plane, and head is connected by screw and is fixed on movable component；The fixation kit includes a fixed shell, secure component and button cap, the installation cavity of one cylinder is set in the fixed shell, the side wall of fixed shell is through one secure component mounting groove of setting, button cap is fixedly connected with secure component by screw, the movable component includes a movable housing, locating dowel is provided with the movable housing, the second circuit board with hard contact is accurately fixed on movable housing by locating dowel.Head rapid dismounting apparatus lighter in weight of the present utility model, outward appearance beautification, simplifies the Connection Step of head and unmanned plane, realizes unmanned plane movable component disassembly efficiency, convenient disassembly, simple to operate, flexible practical, highly reliable.
Description
Technical field
The utility model belongs to unmanned plane field, and in particular to a kind of unmanned plane task device rapid dismounting apparatus.
Background technology
Existing head rapid dismounting apparatus, head rapid dismounting apparatus can realize two fast assembling-disassemblings of part, but can not
The electric power connector transmission high-definition image contacted between two parts.Need what other single line cable shot video camera on head
High-definition image is transferred to the image relay device in unmanned plane.
Existing head rapid dismounting apparatus are, it is necessary to the high-definition image that extra single line cable shoots video camera on head is transmitted
Image relay device in unmanned plane.Causing head rapid dismounting apparatus weight increases, unsightly, and head and unmanned plane
Connection Step it is cumbersome.
The content of the invention
Technical problem to be solved in the utility model is to provide and a kind of can realize two fast assembling-disassemblings of part, and energy
The electric power connector contacted between two parts transmits the unmanned plane task device rapid dismounting apparatus of high-definition image.
The utility model is achieved through the following technical solutions：A kind of unmanned plane task device rapid dismounting apparatus,
Including fixation kit and movable component, the fixation kit is connected by screw the bottom for being fixed on unmanned plane, and head passes through spiral shell
Nail is fastened on movable component；
The fixation kit includes setting a cylinder in a fixed shell, secure component and button cap, the fixed shell
The installation cavity of shape, the side wall of fixed shell is through one secure component mounting groove of setting, the secure component mounting groove and installation
Cavity is communicated, and button cap is fixedly connected with secure component by screw, and an oval-shaped slot, screw are set on the top surface of fixed shell
Upper part be embedded in the oval-shaped slot of fixed shell so that have an extreme position when secure component is moved to the left；
The right-hand end of secure component offsets with the side wall of fixed shell so that have a limit when secure component moves right
Position, the top surface lower surface of fixed shell is provided with two guide pin bushings；
Two springs are installed, one end and the opening groove bottom of spring offset in the open slot of fixed shell, spring it is another
One end offsets with secure component；
4 screw holes are provided with fixed shell, the first circuit board for being welded with electric power connector passes through four screw holes
Accurately it is fixed in fixed shell.
The movable component includes a movable housing, and locating dowel is provided with the movable housing, with hard contact the
Two circuit boards are accurately fixed on movable housing by locating dowel.
Used as preferred technical scheme, the upper surface of movable housing is just correspondingly arranged to two guide pin bushing positions of fixed shell
There is guide pillar, guide pillar coordinates with guide pin bushing to be installed.
Used as preferred technical scheme, the upper surface of movable housing is also equipped with two cantilevers, and cantilever is just to secure component
The claw that upper end is set.
The beneficial effects of the utility model are：Head rapid dismounting apparatus lighter in weight of the present utility model, outward appearance beautification,
Simplify the Connection Step of head and unmanned plane, realize unmanned plane movable component disassembly efficiency, convenient disassembly, it is simple to operate,
It is flexibly practical, highly reliable.
Brief description of the drawings
In order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the overall structure diagram of fixation kit of the present utility model；
Fig. 2 is the overall structure diagram of movable component of the present utility model；
Fig. 3 is the configuration schematic diagram of fixation kit of the present utility model；
Fig. 4 is the configuration schematic diagram of movable component of the present utility model；
Fig. 5 is overall package schematic diagram of the present utility model.
Specific embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive
Feature and/or step beyond, can combine by any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), except non-specifically is chatted
State, can alternative features equivalent by other or with similar purpose replaced.I.e., unless specifically stated otherwise, each feature
It is an example in a series of equivalent or similar characteristics.
As Figure 1-Figure 5, including fixation kit 20 and movable component 30, the fixation kit 20 is connected by screw solid
The bottom of unmanned plane is scheduled on, head is connected by screw and is fixed on movable component 30；
The fixation kit includes setting one in a fixed shell 1, secure component 2 and button cap 3, the fixed shell 1
The installation cavity of cylinder, the side wall of fixed shell 1 through setting a secure component mounting groove, the secure component mounting groove with
Installation cavity is communicated, and button cap 3 is fixedly connected with secure component 2 by screw 5, one is set on the top surface of fixed shell 1 oval
Shape groove, the upper part of screw 5 is embedded in the oval-shaped slot of fixed shell 1 so that secure component 2 has one when being moved to the left
Extreme position；
The right-hand end of secure component 2 offsets with the side wall of fixed shell 1 so that secure component 2 has one when moving right
Extreme position, the top surface lower surface of fixed shell is provided with two guide pin bushings；
Two springs 4 are installed, one end and the opening groove bottom of spring 4 offset, spring 4 in the open slot of fixed shell 1
The other end offseted with secure component；
4 screw holes are provided with fixed shell 1, the first circuit board 12 for being welded with electric power connector 13 passes through four spiral shells
Silk hole is accurately fixed in fixed shell 1.
The movable component includes a movable housing 7, locating dowel is provided with the movable housing 7, with hard contact
Second circuit board 6 is accurately fixed on movable housing 7 by locating dowel.
In the present embodiment, the upper surface of movable housing 7 is just correspondingly arranged on to two positions of guide pin bushing 10 of fixed shell 1 and leads
Post 8, guide pillar 8 coordinates with guide pin bushing 10 to be installed.
In the present embodiment, the upper surface of movable housing 7 is also equipped with two cantilevers 9, and cantilever 9 just sets to secure component upper end
The claw 11 put.
In addition, in the present embodiment, electric power connector 13 is provided with first circuit board, metal is provided with second circuit board
Contact, when mounted, as shown in figure 5, electric power connector can be contacted directly with hard contact, completes conducting, without using electricity
Source line, simplifies structure.
During installation activity component, connect the movable component of task apparatus by spacing guide pillar, guide sleeve structure it is bottom-up enter
Enter fixation kit, the cantilever on movable housing first opens and while compression spring secure component toward vertical direction top.Movable component
Continuation up moves a certain amount of, that is, be installed in place.Now, its claw of resilience blocks active shell to secure component under the action of the spring
Cantilever on body, you can fasten movable component.Meanwhile, electric power connector 13 each play it is each on pin and second circuit board 6
Individual hard contact accurately connects one to one.
During dismounting movable component, the cap that presses ＆ hold moves right a default stroke, claw disengaging activity secure component
Cantilever on housing, you can dismantle movable component downwards.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work should all be covered within protection domain of the present utility model.
Therefore, protection domain of the present utility model should be determined by the scope of protection defined in the claims.
Claims (3)
1. a kind of unmanned plane task device rapid dismounting apparatus, it is characterised in that：It is described solid including fixation kit and movable component
Determine component and be connected by screw the bottom for being fixed on unmanned plane, head is connected by screw and is fixed on movable component；
The fixation kit includes setting a cylinder in a fixed shell, secure component and button cap, the fixed shell
Installation cavity, the side wall of fixed shell is through one secure component mounting groove of setting, the secure component mounting groove and installation cavity
Communicate, button cap is fixedly connected with secure component by screw, an oval-shaped slot be set on the top surface of fixed shell, screw it is upper
End part is embedded in the oval-shaped slot of fixed shell so that have an extreme position when secure component is moved to the left；
The right-hand end of secure component offsets with the side wall of fixed shell so that have the limit position when secure component moves right
Put, the top surface lower surface of fixed shell is provided with two guide pin bushings；
Two springs are installed, one end and the opening groove bottom of spring offset, the other end of spring in the open slot of fixed shell
Offseted with secure component；
4 screw holes are provided with fixed shell, the first circuit board for being welded with electric power connector is accurate by four screw holes
It is fixed in fixed shell；
The movable component includes a movable housing, and locating dowel is provided with the movable housing, the second electricity with hard contact
Road plate is accurately fixed on movable housing by locating dowel.
2. unmanned plane task device rapid dismounting apparatus as claimed in claim 1, it is characterised in that：The upper surface of movable housing
Two guide pin bushing positions just to fixed shell are correspondingly arranged on guide pillar, and guide pillar coordinates with guide pin bushing to be installed.
3. unmanned plane task device rapid dismounting apparatus as claimed in claim 1, it is characterised in that：The upper surface of movable housing
It is also equipped with two cantilevers, the claw that cantilever is just being set to secure component upper end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621079847.4U CN206202710U (en) | 2016-09-26 | 2016-09-26 | A kind of unmanned plane task device rapid dismounting apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621079847.4U CN206202710U (en) | 2016-09-26 | 2016-09-26 | A kind of unmanned plane task device rapid dismounting apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206202710U true CN206202710U (en) | 2017-05-31 |
Family
ID=58762528
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621079847.4U Expired - Fee Related CN206202710U (en) | 2016-09-26 | 2016-09-26 | A kind of unmanned plane task device rapid dismounting apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206202710U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108110453A (en) * | 2017-11-17 | 2018-06-01 | 深圳市科比特航空科技有限公司 | Connector construction and carry unmanned plane |
| CN112840153A (en) * | 2020-07-17 | 2021-05-25 | 深圳市大疆创新科技有限公司 | External device, handheld cloud platform subassembly and handheld cloud platform |
-
2016
- 2016-09-26 CN CN201621079847.4U patent/CN206202710U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108110453A (en) * | 2017-11-17 | 2018-06-01 | 深圳市科比特航空科技有限公司 | Connector construction and carry unmanned plane |
| CN112840153A (en) * | 2020-07-17 | 2021-05-25 | 深圳市大疆创新科技有限公司 | External device, handheld cloud platform subassembly and handheld cloud platform |
| WO2022011670A1 (en) * | 2020-07-17 | 2022-01-20 | 深圳市大疆创新科技有限公司 | External device, handheld gimbal assembly, and handheld gimbal |
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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: 20170531 |