CN204871622U - Unmanned aerial vehicle GPS device - Google Patents
Unmanned aerial vehicle GPS device Download PDFInfo
- Publication number
- CN204871622U CN204871622U CN201520563846.6U CN201520563846U CN204871622U CN 204871622 U CN204871622 U CN 204871622U CN 201520563846 U CN201520563846 U CN 201520563846U CN 204871622 U CN204871622 U CN 204871622U
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- China
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- gps device
- buckle
- unmanned plane
- lower house
- location division
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Abstract
The utility model discloses an unmanned aerial vehicle GPS device, this GPS device include that the GPS chip still includes casing, location portion, connecting seat, and the GPS chip is fixed to be set up inside the casing, the bottom downwardly extending of casing is provided with the buckle, is provided with the trompil on the connecting seat, the buckle card solid in the trompil, location portion locates casing bottom, the connecting seat top seted up with the solid complex constant head tank of location portion's card. The utility model discloses a GPS device has quick installation, the effect that pinpoints, and its simple structure, low cost.
Description
Technical field
The utility model relates to a kind of GPS device, more specifically, relates to a kind of unmanned plane GPS device.
Background technology
Along with the development of science and technology, the continuous progress of the mankind, the application of unmanned plane in our life is also more and more extensive.Navigate all indispensable at the whole flight course of unmanned plane, only know it particular location we could remote control to next position, so navigation plays a part very important in unmanned plane, and we often use is that gps satellite navigates.And the existing GPS of unmanned plane does not have anchor fitting, usually fixed by adhesive tape, during erection cost, unsightly, and also fixing not firm.
Utility model content
For solving the problems of the prior art, the utility model provides a kind of GPS device with fixed sturcture.
The utility model provides a kind of unmanned plane GPS device, and described GPS device comprises GPS chip (2), and described GPS device also comprises housing, location division (4), Connection Block (5), and GPS chip is fixedly installed on enclosure interior; The bottom of housing is extended downwards buckle (6), and Connection Block is provided with perforate (5-1), buckle is fastened in described perforate; Housing bottom is located in location division, and Connection Block top offers the positioning groove (5-2) fixing with location division and coordinate.
Described housing comprises upper shell (1) and lower house (3), and GPS chip is fixedly connected with lower house, and buckle and location division are arranged at the bottom of lower house.
Described location division comprises accommodating hole (7) and flexure strip (8), and wherein, described accommodating hole is opened in bottom lower house; Described flexure strip is arranged in accommodating hole and parallel with lower house bottom surface, and one end of flexure strip is connected to lower house, and the other end is convexly equipped with protrusion (9) downwards, and described protrusion coordinates and is arranged in described positioning groove.
Described protrusion is rectangular cam, and described positioning groove is run through the rectangular opening being opened in Connection Block top.
Described buckle is provided with two, the symmetrical both sides being positioned at described location division; Described Connection Block is provided with two perforates, and position is relative with described buckle.
Described buckle comprises extension (6-1), and extension lower end is provided with scratching part (6-2); Described perforate is L shape hole, there is the first aperture portion (5-1-1) and second aperture portion (5-1-2) of buckle can be worn, first aperture portion width is less than the second aperture portion, described extension be arranged in the first aperture portion and described scratching part snap fit in the sidewall of the first aperture portion.
Upper shell and lower house are bolted integral.
The bottom of GPS chip is provided with data exposure shell fragment (10).
The beneficial effects of the utility model are: GPS device of the present utility model has Fast Installation, accurately the effect of location, stable connection difficult drop-off, and its structure is simple, with low cost.
Accompanying drawing explanation
Fig. 1 is the structural representation of unmanned plane GPS device of the present utility model:
In figure, 1, upper shell; 2, GPS chip; 3, lower house; 4, location division; 4-1, protrusion; 5, Connection Block; 5-1, perforate; 5-1-1, the first aperture portion; 5-1-2, the second aperture portion; 5-2, positioning groove; 6, buckle; 6-1, extension; 6-2, scratching part; 7, accommodating hole; 8, flexure strip; 9, protrusion; 10, data exposure shell fragment.
Detailed description of the invention
Below in conjunction with drawings and Examples, explanation is explained in detail to structure of the present utility model.
As shown in Figure 1, a kind of unmanned plane GPS device of the present utility model, comprises housing, GPS chip 2, and location division 4, Connection Block 5, GPS chip 2 are fixedly installed on enclosure interior; The bottom of housing is extended downwards buckle 6, and Connection Block 5 is provided with perforate 5-1, buckle 6 is fastened in perforate 5-1; Housing bottom is located in location division 4, and Connection Block 5 top offers and fixes with location division 4 the positioning groove 5-2 coordinated.Match with positioning groove 5-2 and act on and play the effect of location in location division 4.
Housing comprises upper shell 1 and lower house 3, GPS chip 2 is fixedly connected with lower house 3, and buckle 6 and location division 4 are arranged at the bottom of lower house 3.Upper shell 1 and lower house 3 are bolted integral, thus easy for removal and installation.
In a preferred embodiment, location division 4 comprises: accommodating hole 7, is opened in bottom lower house 3; Flexure strip 8, is arranged in accommodating hole 7 and parallel with lower house 3 bottom surface, and one end of flexure strip 8 is connected to lower house 3, and the other end is convexly equipped with protrusion 9 downwards, and protrusion 9 coordinates and is arranged in positioning groove 5-2.To be matched with the positioning groove 5-2 that Connection Block is offered by the protrusion 9 arranged and act on and play the effect of location in location division 4.
In a preferred embodiment, protrusion 9 is rectangular cam, and positioning groove 5-2 runs through the rectangular opening being opened in Connection Block 5 top.Protrusion 9 and positioning groove 5-2 can also be other circular etc. shape.Rectangular cam fixes the effect playing location in rectangular opening.
In a preferred embodiment, buckle 6 is provided with two, the symmetrical both sides being positioned at location division 4; Connection Block 5 is provided with two perforate 5-1, and position is relative with described buckle.Buckle 6 and perforate 5-1 also can be set to three, four etc. multiple.Buckle 6 is identical with the quantity of perforate 5-1, and position is relative.
Buckle 6 comprises extension 6-1, and extension 6-1 lower end is provided with scratching part 6-2; Perforate 5-1 is L shape hole, there is the first aperture portion 5-1-1 and the second aperture portion 5-1-2 of buckle 6 can be worn, first aperture portion 5-1-1 width is less than the second aperture portion 5-1-2, extension 6-1 be arranged in the first aperture portion 5-1-1 and described scratching part 6-2 snap fit in the sidewall of the first aperture portion 5-1-1.
When location division 4 is connected with Connection Block 5, buckle 6 passes the second aperture portion 5-1-2, at this moment, housing is to side action, extension 6-1 moves to the first aperture portion 5-1-1, makes scratching part 6-2 be hooked in the sidewall of the first aperture portion 5-1-1, thus housing is fixed on Connection Block 5.
The bottom of GPS chip 2 is provided with data exposure shell fragment 10.Data exposure shell fragment 10 is connected with lower house 3, and lower house 3 fixes on Connection Block 5, in the frame that Connection Block 5 is consolidated in unmanned plane or one-body molded with the frame of unmanned plane, thus achieves the accurate location of unmanned plane.
The foregoing is only preferred embodiment of the present utility model, not in order to limit the utility model, all do in the utility model flesh and blood any amendment, equivalent to replace and simple modifications etc., all should be included within protection domain of the present utility model.
Claims (8)
1. a unmanned plane GPS device, described GPS device comprises GPS chip (2), it is characterized in that, described GPS device also comprises housing, location division (4), Connection Block (5), and GPS chip is fixedly installed on enclosure interior; The bottom of housing is extended downwards buckle (6), and Connection Block is provided with perforate (5-1), buckle is fastened in described perforate; Housing bottom is located in location division, and Connection Block top offers the positioning groove (5-2) fixing with location division and coordinate.
2. unmanned plane GPS device according to claim 1, is characterized in that, described housing comprises upper shell (1) and lower house (3), and GPS chip is fixedly connected with lower house, and buckle and location division are arranged at the bottom of lower house.
3. unmanned plane GPS device according to claim 2, is characterized in that, described location division comprises accommodating hole (7) and flexure strip (8), wherein,
Described accommodating hole is opened in bottom lower house;
Described flexure strip is arranged in accommodating hole and parallel with lower house bottom surface, and one end of flexure strip is connected to lower house, and the other end is convexly equipped with protrusion (9) downwards, and described protrusion coordinates and is arranged in described positioning groove.
4. unmanned plane GPS device according to claim 3, is characterized in that, described protrusion is rectangular cam, and described positioning groove is run through the rectangular opening being opened in Connection Block top.
5. unmanned plane GPS device according to claim 2, is characterized in that, described buckle is provided with two, the symmetrical both sides being positioned at described location division; Described Connection Block is provided with two perforates, and position is relative with described buckle.
6. the unmanned plane GPS device according to any one of claim 2-5, is characterized in that, described buckle comprises extension (6-1), and extension lower end is provided with scratching part (6-2);
Described perforate is L shape hole, there is the first aperture portion (5-1-1) and second aperture portion (5-1-2) of buckle can be worn, first aperture portion width is less than the second aperture portion, described extension be arranged in the first aperture portion and described scratching part snap fit in the sidewall of the first aperture portion.
7. unmanned plane GPS device according to claim 2, is characterized in that, upper shell and lower house are bolted integral.
8. unmanned plane GPS device according to claim 1, is characterized in that, the bottom of GPS chip is provided with data exposure shell fragment (10).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520563846.6U CN204871622U (en) | 2015-07-30 | 2015-07-30 | Unmanned aerial vehicle GPS device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520563846.6U CN204871622U (en) | 2015-07-30 | 2015-07-30 | Unmanned aerial vehicle GPS device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204871622U true CN204871622U (en) | 2015-12-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520563846.6U Active CN204871622U (en) | 2015-07-30 | 2015-07-30 | Unmanned aerial vehicle GPS device |
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| CN (1) | CN204871622U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323656A (en) * | 2017-08-23 | 2017-11-07 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of high definition is taken photo by plane unmanned plane undercarriage protector and the localization method that rises and falls |
| US10814980B2 (en) | 2017-09-02 | 2020-10-27 | Precision Drone Services Intellectual Property, Llc | Distribution assembly for an aerial vehicle |
| US11242147B2 (en) | 2017-08-31 | 2022-02-08 | Precision Drone Services Intellectual Property, Llc | Aerial vehicle implement hitch assembly |
-
2015
- 2015-07-30 CN CN201520563846.6U patent/CN204871622U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107323656A (en) * | 2017-08-23 | 2017-11-07 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of high definition is taken photo by plane unmanned plane undercarriage protector and the localization method that rises and falls |
| US11242147B2 (en) | 2017-08-31 | 2022-02-08 | Precision Drone Services Intellectual Property, Llc | Aerial vehicle implement hitch assembly |
| US10814980B2 (en) | 2017-09-02 | 2020-10-27 | Precision Drone Services Intellectual Property, Llc | Distribution assembly for an aerial vehicle |
| US11718400B2 (en) | 2017-09-02 | 2023-08-08 | Precision Drone Services Intellectual Property, Llc | Distribution assembly for an aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160725 Address after: 401121 Chongqing Yubei District City Longxing Street Ying Long Road No. 19 Patentee after: CHONGQING ZERO INTELLIGENT CONTROL TECHNOLOGY CO.,LTD. Address before: 100094 Beijing, Haidian District, northeast Wang West Road, No. 8 Zhongguancun Software Park, building 9, 203 Patentee before: ZEROTECH (BEIJING) INTELLIGENCE TECHNOLOGY Co.,Ltd. |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Unmanned aerial vehicle GPS device Effective date of registration: 20180102 Granted publication date: 20151216 Pledgee: XinDa national equity investment fund (Shanghai) partnership (L.P.) Pledgor: ZEROTECH (BEIJING) INTELLIGENCE TECHNOLOGY Co.,Ltd.|CHONGQING ZERO INTELLIGENT CONTROL TECHNOLOGY CO.,LTD. Registration number: 2017990001217 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20221008 Granted publication date: 20151216 Pledgee: XinDa national equity investment fund (Shanghai) partnership (L.P.) Pledgor: CHONGQING ZERO INTELLIGENT CONTROL TECHNOLOGY CO.,LTD. Registration number: 2017990001217 |