CN204103123U - GPS plug-in holder - Google Patents
GPS plug-in holder Download PDFInfo
- Publication number
- CN204103123U CN204103123U CN201420630560.0U CN201420630560U CN204103123U CN 204103123 U CN204103123 U CN 204103123U CN 201420630560 U CN201420630560 U CN 201420630560U CN 204103123 U CN204103123 U CN 204103123U
- Authority
- CN
- China
- Prior art keywords
- plug
- gps
- pole
- pedestal
- endoporus
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Position Fixing By Use Of Radio Waves (AREA)
Abstract
The utility model discloses a kind of GPS plug-in holder easy to use, structure is simple, quality is light, the GPS plug-in fixture that cost is low, it comprises pedestal, pole, described pedestal is provided with endoporus, described pole one end is provided with disk, disk upper surface installs GPS, its other end is provided with plug, described plug is provided with the copper elastic connecting plug-in unit of swelling-waist shape, through slot is provided with in swelling-waist shape, described plug inserts the locating piece socket location be provided with by the groove in pedestal and plug when pedestal endoporus connects, this gps plug-in holder is used to be collided and to damage.
Description
Technical field
The utility model relates to the holder of GPS, is particularly arranged on the GPS holder in remote controlled rotary-wing aircraft.
Background technology
Technology along with GPS reaches its maturity and extensive use, present remote control multi-rotor aerocraft great majority have all installed capture apparatus, for the enable picture rich in detail photographing place, the correct object in orientation, at remote control multi-rotor aerocraft, GPS device is nearly all being installed, these holders installing GPS device are mostly one fixed structures, the holder of this one fixed structure is arranged on the body plate of remote control multi-rotor aerocraft, when carrying remote control multi-rotor aerocraft, the pole in unavoidable holder is collided and damages.So do technically to improve to this holder, between the pedestal and pole connection of the holder of one fixed structure, adopt bending method, make this holder under GPS not service condition, pole is bent, do not make pole being erected, avoid pole being collided.It also avoid GPS to be like this damaged.But this holder quality that can bend is overweight, complex structure, processing trouble, which adds production cost.
Summary of the invention
Technical problem to be solved in the utility model is to provide the GPS plug-in holder that a kind of structure is simple, easy to process, quality is light.
For solving the problems of the technologies described above, the technical method that the utility model adopts is: a kind of GPS plug-in holder, comprise pedestal 1, pole 3, described pole 3 one end is provided with disk 4, described pedestal 1 is provided with endoporus 1-1, and its upper-end part of driving centre position is provided with detent 1-2, and the other end of described pole 3 is provided with plug 2, position, described plug 2 front end is provided with copper elastic connecting plug-in unit 2-1, and intermediate position is provided with locating piece 2-2.
Described copper elastic connecting plug-in unit 2-1 is in the swelling-waist shape being provided with the through slot 2-11 that is evenly distributed.
Described plug 2 is provided with endoporus 2-3, and this endoporus 2-3 is fixedly connected with one end of pole 3, the endoporus 2-12 of position, described plug 2 front end socket swelling-waist shape copper elastic connecting plug-in unit 2-1.
Detent 1-2 set by described pedestal 1 and the locating piece 2-2 set by described plug 2 coordinate socket, correctly locate during the endoporus 1-1 making the described copper elastic connecting of the swelling-waist shape set by plug 2 plug-in unit 2-1 insert set by described pedestal 1.
The beneficial effect of the utility model GPS plug-in holder is: because pedestal and pole adopt plug-in structure, when remote control multi-rotor aerocraft needs flight, the endoporus that the pole being provided with GPS is inserted in pedestal is connected, when not flying, pole is extracted from the endoporus pedestal and deposits separately, like this carry remote control multi-rotor aerocraft time GPS not wherein.Exempt from it be collided and damage.Pole and pedestal can exchange and patch simultaneously, and a GPS just can use in multi rack remote control multi-rotor aerocraft, saves equipment acquisition expenses.And GPS plug-in holder quality is light, structure is simple, easy to process, simple operation, production cost are low.
Accompanying drawing explanation
Fig. 1 is the utility model general illustration.
Fig. 2 is the structure for amplifying schematic diagram of plug.
Embodiment
As shown in Figure 1 and Figure 2, an embodiment of the utility model GPS plug-in holder, GPS plug-in holder, comprises pedestal 1, pole 3, and described pole 3 one end is provided with disk 4, at disk 4 upper surface fixed installation GPS, described pedestal 1 is provided with endoporus 1-1, and its upper-end part of driving centre position is provided with detent 1-2, and the other end of described pole 3 is provided with plug 2, position, described plug 2 front end is provided with copper elastic connecting plug-in unit 2-1, and intermediate position is provided with locating piece 2-2.Described copper elastic connecting plug-in unit 2-1 is in the swelling-waist shape being provided with the through slot 2-11 that is evenly distributed.Described plug 2 is provided with endoporus 2-3, and this endoporus 2-3 is fixedly connected with the other end of pole 3, the endoporus 2-12 of position, described plug 2 front end socket swelling-waist shape copper elastic connecting plug-in unit 2-1.The endoporus 1-1 be provided with in the swelling-waist shape copper elastic connecting plug-in unit 2-1 precision-fit pedestal 1 that described plug 2 is provided with inserts or therefrom extracts.Detent 1-2 set by described pedestal 1 and the locating piece 2-2 set by described plug 2 coordinate socket, correctly locate during the endoporus 1-1 making the described copper elastic connecting of the swelling-waist shape set by plug 2 plug-in unit 2-1 insert set by described pedestal 1.
Described pedestal is fixedly mounted on the body plate of remote control multi-rotor aerocraft, when remote control multi-rotor aerocraft needs flight, the endoporus that the plug be installed with in the pole of gps inserts in pedestal connects, when remote control multi-rotor aerocraft does not fly, plug in pole is extracted from the endoporus pedestal and preserves separately, when carrying remote control multi-rotor aerocraft, gps and pole would not be collided and damage like this, and the plug in this pole can exchange pedestal patches use.The utility model GPS plug-in holder is easy to use, and structure is simple, and quality is light, and cost is low.
Claims (4)
1. GPS plug-in holder, comprise pedestal (1), pole (3), described pole (3) one end is provided with disk (4), it is characterized in that: described pedestal (1) is provided with endoporus (1-1), its upper-end part of driving centre position is provided with detent (1-2), the other end of described pole (3) is provided with plug (2), described plug (2) position, front end is provided with copper elastic connecting plug-in unit (2-1), and intermediate position is provided with locating piece (2-2).
2. GPS plug-in holder according to claim 1, is characterized in that: described copper elastic connecting plug-in unit (2-1) is in the swelling-waist shape being provided with the through slot that is evenly distributed (2-11).
3. GPS plug-in holder according to claim 1, it is characterized in that: described plug (2) is provided with endoporus (2-3), this endoporus (2-3) is fixedly connected with the other end of pole (3), the endoporus (2-12) of the copper elastic connecting plug-in unit (2-1) of described plug (2) position, front end socket swelling-waist shape.
4. GPS plug-in holder according to claim 1, it is characterized in that: the detent (1-2) set by described pedestal (1) and the locating piece (2-2) set by described plug (2) coordinate socket, correctly locate time endoporus (1-1) that make described swelling-waist shape copper elastic connecting plug-in unit (2-1) set by plug (2) insert set by described pedestal (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420630560.0U CN204103123U (en) | 2014-10-29 | 2014-10-29 | GPS plug-in holder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420630560.0U CN204103123U (en) | 2014-10-29 | 2014-10-29 | GPS plug-in holder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204103123U true CN204103123U (en) | 2015-01-14 |
Family
ID=52271527
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420630560.0U Expired - Fee Related CN204103123U (en) | 2014-10-29 | 2014-10-29 | GPS plug-in holder |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204103123U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163218A (en) * | 2017-12-29 | 2018-06-15 | 顺丰科技有限公司 | Navigate stent |
-
2014
- 2014-10-29 CN CN201420630560.0U patent/CN204103123U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108163218A (en) * | 2017-12-29 | 2018-06-15 | 顺丰科技有限公司 | Navigate stent |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150114 Termination date: 20171029 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |