CN212401583U - A removable component for unmanned aerial vehicle - Google Patents
A removable component for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN212401583U CN212401583U CN202020190069.6U CN202020190069U CN212401583U CN 212401583 U CN212401583 U CN 212401583U CN 202020190069 U CN202020190069 U CN 202020190069U CN 212401583 U CN212401583 U CN 212401583U
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- China
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- unmanned aerial
- aerial vehicle
- subassembly
- vehicle body
- dismantle
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- Expired - Fee Related
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Abstract
The utility model discloses a can dismantle subassembly for unmanned aerial vehicle, include the unmanned aerial vehicle body and can dismantle the subassembly of connecting in this unmanned aerial vehicle body, the subassembly is provided with the spring buckle, be provided with the draw-in groove that matches with this spring buckle on the unmanned aerial vehicle body, be provided with external connector on the subassembly. The utility model discloses a can dismantle the subassembly of connecting in this unmanned aerial vehicle body and realize crossing the plug-in replacement, install different plug-in components through external ware, for example camera equipment, empty gas detection survey equipment, material throw equipment etc. all can connect through external ware, and external ware sets up the device of being connected with it according to actual conditions, the subassembly passes through the spring buckle and is connected and fixed, safe and reliable, convenient to use with unmanned aerial vehicle.
Description
Technical Field
The utility model relates to a technical field such as unmanned aerial vehicle technique, mechanical part, concretely relates to a can dismantle subassembly for unmanned aerial vehicle.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer.
Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Unmanned aerial vehicle's control technology adopts automatic data adjustment or manual control more, and under the relevant technological rapid development of unmanned aerial vehicle, the kind of unmanned aerial vehicle system also increases gradually, the usage characteristics are distinct, and according to flight platform configuration classification, unmanned aerial vehicle can divide into fixed wing unmanned aerial vehicle, rotor unmanned aerial vehicle, unmanned airship, umbrella wing unmanned aerial vehicle, flapping wing unmanned aerial vehicle etc.. The rotor unmanned aerial vehicle is the most widely used one, but the shortcoming of rotor unmanned aerial vehicle is still many, and the place that needs to improve is also many.
SUMMERY OF THE UTILITY MODEL
To the defect among the prior art, the utility model provides a can dismantle subassembly for unmanned aerial vehicle to increase unmanned aerial vehicle's use scene, install more plug-ins through can dismantling the subassembly.
A can dismantle subassembly for unmanned aerial vehicle, include the unmanned aerial vehicle body and can dismantle the subassembly of connecting in this unmanned aerial vehicle body, the subassembly is provided with the spring buckle, be provided with the draw-in groove that matches with this spring buckle on the unmanned aerial vehicle body, be provided with external connector on the subassembly.
The utility model discloses a can dismantle the subassembly of connecting in this unmanned aerial vehicle body and realize crossing the plug-in replacement, install different plug-in components through external ware, for example camera equipment, empty gas detection survey equipment, material throw equipment etc. all can connect through external ware, and external ware sets up the device of being connected with it according to actual conditions, the subassembly passes through the spring buckle and is connected and fixed, safe and reliable, convenient to use with unmanned aerial vehicle.
Further, set up two subassemblies at least, the unit mount is in both ends around the unmanned aerial vehicle body.
Further, set up two subassemblies at least, the unit mount is in both ends about the unmanned aerial vehicle body.
Further, in order to improve stability, the spring buckle is a spring pressing type buckle.
Further, be provided with data interface, connecting piece and pilot lamp on the external connector, wherein data interface adopt data interface such as USB commonly used can, the connecting piece is confirmed according to the plug-in components that external connector will be connected, and the pilot lamp mainly used judges whether the subassembly is connected successfully, the power of pilot lamp passes through unmanned aerial vehicle and provides, and with unmanned aerial vehicle's electric connection, can be connected through the electric shock, also can be through spring buckle and unmanned aerial vehicle circular telegram.
The beneficial effects of the utility model are embodied in:
the utility model discloses a can dismantle the subassembly of connecting in this unmanned aerial vehicle body and realize crossing the plug-in replacement, install different plug-in components through external ware, for example camera equipment, empty gas detection survey equipment, material throw equipment etc. all can connect through external ware, and external ware sets up the device of being connected with it according to actual conditions, the subassembly passes through the spring buckle and is connected and fixed, safe and reliable, convenient to use with unmanned aerial vehicle.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the technical solutions in the prior art will be briefly described below. Throughout the drawings, like elements or portions are generally identified by like reference numerals. In the drawings, elements or portions are not necessarily drawn to scale.
Fig. 1 is a schematic structural diagram of an embodiment of the present invention;
fig. 2 is a schematic structural view of the assembly shown in fig. 1.
In the attached drawing, 1-unmanned aerial vehicle body, 2-subassembly, 3-external connector, 4-spring buckle.
Detailed Description
Embodiments of the present invention will be described in detail below with reference to the accompanying drawings. The following examples are only for illustrating the technical solutions of the present invention more clearly, and therefore are only examples, and the protection scope of the present invention is not limited thereby.
It is to be noted that unless otherwise specified, technical or scientific terms used herein shall have the ordinary meaning as understood by those skilled in the art to which the present invention belongs.
Examples
As shown in fig. 1 and 2, a detachable component for unmanned aerial vehicle, include unmanned aerial vehicle body 1 and can dismantle the subassembly 2 of connecting in this unmanned aerial vehicle body 1, subassembly 2 is provided with spring buckle 4, be provided with the draw-in groove that matches with this spring buckle 4 on the unmanned aerial vehicle body 1, be provided with external connector 3 on the subassembly 2.
The utility model discloses a can dismantle and realize the plug-in components replacement in subassembly 2 of this unmanned aerial vehicle body 1, install different plug-in components through external ware 3, for example camera equipment, empty gas detection survey equipment, material throw equipment etc. all can connect through external ware 3, and external ware 3 sets up the device of being connected with it according to actual conditions, subassembly 2 is connected and is fixed safe and reliable, convenient to use through spring buckle 4 and unmanned aerial vehicle. The external plug-in connection mode adopted by the external connector 3 is the existing plug-in connection mode.
In this embodiment, set up two at least subassemblies 2, subassembly 2 is installed both ends around the unmanned aerial vehicle body 1. The tandem arrangement contributes to stability.
In order to improve stability, the spring buckle 4 is a spring pressing type buckle, which can adopt the prior art.
Be provided with data interface, connecting piece and pilot lamp on external connector 3, wherein data interface adopt data interface such as USB commonly used can, the connecting piece is confirmed according to the plug-in components that external connector 3 will be connected, and the pilot lamp mainly used judges whether subassembly 2 is connected successfully, the power of pilot lamp passes through unmanned aerial vehicle and provides, and with unmanned aerial vehicle's electric connection, can be connected through the electric shock, also can switch on with unmanned aerial vehicle through spring buckle 4.
Finally, it should be noted that: the above embodiments are only used to illustrate the technical solution of the present invention, and not to limit the same; although the present invention has been described in detail with reference to the foregoing embodiments, it should be understood by those skilled in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some or all of the technical features may be equivalently replaced; such modifications and substitutions do not substantially depart from the scope of the embodiments of the present invention, and are intended to be covered by the claims and the specification.
Claims (5)
1. A subassembly can dismantle for unmanned aerial vehicle, its characterized in that: including unmanned aerial vehicle body (1) and can dismantle subassembly (2) of connecting in this unmanned aerial vehicle body (1), subassembly (2) are provided with spring buckle (4), be provided with the draw-in groove that matches with this spring buckle (4) on unmanned aerial vehicle body (1), be provided with external ware (3) on subassembly (2).
2. The removable component for drone of claim 1, wherein: set up two at least subassembly (2), install subassembly (2) the front and back both ends of unmanned aerial vehicle body (1).
3. The removable component for drone of claim 1, wherein: set up two at least subassembly (2), install subassembly (2) both ends about unmanned aerial vehicle body (1).
4. The removable component for drone of claim 3, wherein: the spring buckle (4) is a spring pressing type buckle.
5. The removable component for drone of claim 1, wherein: and the external connector (3) is provided with a data interface, a connecting piece and an indicator lamp.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020190069.6U CN212401583U (en) | 2020-02-21 | 2020-02-21 | A removable component for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020190069.6U CN212401583U (en) | 2020-02-21 | 2020-02-21 | A removable component for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212401583U true CN212401583U (en) | 2021-01-26 |
Family
ID=74400225
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020190069.6U Expired - Fee Related CN212401583U (en) | 2020-02-21 | 2020-02-21 | A removable component for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212401583U (en) |
-
2020
- 2020-02-21 CN CN202020190069.6U patent/CN212401583U/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: 20210126 |