CN207191452U - One kind is used for unmanned plane GPS folding brackets - Google Patents

One kind is used for unmanned plane GPS folding brackets Download PDF

Info

Publication number
CN207191452U
CN207191452U CN201721216479.8U CN201721216479U CN207191452U CN 207191452 U CN207191452 U CN 207191452U CN 201721216479 U CN201721216479 U CN 201721216479U CN 207191452 U CN207191452 U CN 207191452U
Authority
CN
China
Prior art keywords
body plate
unmanned plane
frame
stand frame
reinforcing frame
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
Application number
CN201721216479.8U
Other languages
Chinese (zh)
Inventor
刘银
陈鹏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hubei Pengcheng Cutting-Edge Technology Development Co Ltd
Original Assignee
Hubei Pengcheng Cutting-Edge Technology Development Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Hubei Pengcheng Cutting-Edge Technology Development Co Ltd filed Critical Hubei Pengcheng Cutting-Edge Technology Development Co Ltd
Priority to CN201721216479.8U priority Critical patent/CN207191452U/en
Application granted granted Critical
Publication of CN207191452U publication Critical patent/CN207191452U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Position Fixing By Use Of Radio Waves (AREA)

Abstract

The utility model belongs to unmanned air vehicle technique field, and in particular to one kind is used for unmanned plane GPS folding brackets.This, which is used for unmanned plane GPS folding brackets, includes be hinged reinforcing frame, stand frame and the base of body plate, body plate.One end of stand frame is slidably connected with body plate, the other end of support is provided with base, stand frame is hinged reinforcing frame at middle part close to the side of base, the sliding surface of one end that the jointed shaft of reinforcing frame and body plate is slidably connected parallel to reinforcing frame and the jointed shaft of stand frame, stand frame with body plate is parallel to reinforcing frame and the jointed shaft of body plate.Body plate may be configured as flat board, and the jointed shaft of reinforcing frame and body plate is parallel to body plate.This, which is used for unmanned plane GPS folding brackets, to fold, and can prevent signal interference, again convenient collection and saving space, and overall structure is attractive in appearance, is easy to set.

Description

One kind is used for unmanned plane GPS folding brackets
Technical field
The utility model belongs to unmanned air vehicle technique field, and in particular to one kind is used for unmanned plane GPS folding brackets.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself The not manned aircraft that presetting apparatus manipulates.It can be divided into from technical standpoint definition:Depopulated helicopter, unmanned fixed-wing aircraft, Unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc..By the remote control to unmanned plane, it can be made extensively should For the every field such as taking photo by plane, rescuing.Unmanned plane application fortune is transported, it is necessary to unmanned plane is correspondingly improved, set up Related function, wherein, just include the setting to GPS device, it is necessary to corresponding support or base.Although have one in the prior art A little GPS are fixed or the technical scheme of mounting bracket discloses, and still, the GPS folding brackets for unmanned plane temporarily have no related Technical scheme discloses.
Utility model content
To solve the deficiencies in the prior art, the utility model provides one kind and is used for unmanned plane GPS folding brackets.Should It can be folded for unmanned plane GPS folding brackets, signal interference can be prevented, convenient collection and saving space, overall again Structure is attractive in appearance, is easy to set.
Technical scheme provided by the utility model is as follows:
One kind is used for unmanned plane GPS folding brackets, comprises at least:
Body plate;
Reinforcing frame, the reinforcing frame are hinged with the body plate;
Stand frame, one end of the stand frame are slidably connected with the body plate, and the other end of the stand frame is provided with Base, the stand frame are hinged the reinforcing frame, the reinforcing frame and the body plate at middle part close to the side of the base Jointed shaft parallel to the reinforcing frame and the jointed shaft of the stand frame, what the stand frame was slidably connected with the body plate The sliding surface of one end is parallel to the reinforcing frame and the jointed shaft of the body plate.
What above-mentioned technical proposal was provided is installed on unmanned plane for unmanned plane GPS folding brackets, can be in base Upper setting GPS device.With the rotation of reinforcing frame and stand frame, support can be folded, so change GPS device position and Direction, so as to prevent signal interference, again convenient to collect and save space, overall structure is attractive in appearance, is easy to set.
Further, the base is provided with loading end, and the loading end rotates with the rotation of the stand frame, institute Stand frame is stated perpendicular to the body plate, the loading end is parallel to the body plate;The stand frame is parallel to the fuselage Plate, the loading end is perpendicular to the body plate.
Above-mentioned technical proposal can be used in unmanned plane GPS folding brackets use and folding space it is compact.
Further, the loading end is perpendicular to the stand frame.
Further, the base is L-shaped, and the face pedestal perpendicular to the loading end is fixedly connected on the stand frame On.
Further, the body plate for flat board, the jointed shaft of the reinforcing frame and the body plate is parallel to described Body plate.
Further, the reinforcing frame is included for the hollow reinforcement side lever that is routed through, the body plate be provided with The passage for Gong being routed through corresponding to the reinforcement side lever.
Above-mentioned technical proposal can realize the connection of GPS device and unmanned plane body.
Generally, it is provided by the utility model to be installed on unmanned plane for unmanned plane GPS folding brackets, can be GPS device is set on base.With the rotation of reinforcing frame and stand frame, support can be folded, and then change the position of GPS device Put and direction, so as to prevent signal interference, and can uses and folding space is compact, to facilitate collection and save space. Device overall structure is attractive in appearance, is easy to set, and is set suitable for unmanned plane GPS device.
Brief description of the drawings
Fig. 1 is the side view provided by the utility model for unmanned plane GPS folding bracket unfoldable shapes.
Fig. 2 is the front view provided by the utility model for unmanned plane GPS folding bracket unfoldable shapes.
Fig. 3 is the rearview provided by the utility model for unmanned plane GPS folding bracket unfoldable shapes.
Fig. 4 is the upward view provided by the utility model for unmanned plane GPS folding bracket unfoldable shapes.
Fig. 5 is the top view provided by the utility model for unmanned plane GPS folding bracket unfoldable shapes.
Fig. 6 is the side view provided by the utility model for unmanned plane GPS folding bracket retracted configurations.
Fig. 7 is the front view provided by the utility model for unmanned plane GPS folding bracket retracted configurations.
Fig. 8 is the rearview provided by the utility model for unmanned plane GPS folding bracket retracted configurations.
Fig. 9 is the upward view provided by the utility model for unmanned plane GPS folding bracket retracted configurations.
Figure 10 is the top view provided by the utility model for unmanned plane GPS folding bracket retracted configurations.
Figure 11 is the side view provided by the utility model for unmanned plane GPS folding bracket folded forms.
Figure 12 is the front view provided by the utility model for unmanned plane GPS folding bracket folded forms.
Figure 13 is the rearview provided by the utility model for unmanned plane GPS folding bracket folded forms.
Figure 14 is the upward view provided by the utility model for unmanned plane GPS folding bracket folded forms.
Figure 15 is the top view provided by the utility model for unmanned plane GPS folding bracket folded forms.
In accompanying drawing 1,2,3,4,5,6,7,8,9,10,11,12,13,14,15, the structure list representated by each label is as follows:
1st, body plate, 2, reinforcing frame, 3, stand frame, 4, base.
Embodiment
Principle of the present utility model and feature are described below, illustrated embodiment is served only for explaining the utility model, It is not intended to limit the scope of the utility model.
In a detailed embodiment, as shown in Fig. 1,6,11, fuselage is included for unmanned plane GPS folding brackets Plate 1, body plate 1 be hinged reinforcing frame 2, stand frame 3 and base 4.
One end of stand frame 3 is slidably connected with body plate 1, and the other end of stand frame 3 is provided with base 4, and stand frame 3 is in Portion is hinged reinforcing frame 2 close to the side of base 4, and the jointed shaft of reinforcing frame 2 and body plate 1 is parallel to reinforcing frame 2 and stand frame 3 Jointed shaft, the sliding surface of one end that stand frame 3 is slidably connected with body plate 1 is parallel to reinforcing frame 2 and the jointed shaft of body plate 1. Body plate 1 may be configured as flat board, and the jointed shaft of reinforcing frame 2 and body plate 1 is parallel to body plate 1.
Base 4 is L-shaped, including the loading end perpendicular to stand frame 3.Loading end rotates with the rotation of stand frame 3, branch Frame frame 3 is perpendicular to body plate 1, and loading end is parallel to body plate 1;Stand frame 3 is parallel to body plate 1, and loading end is perpendicular to fuselage Plate 1.A face pedestal perpendicular to loading end is then fixedly connected on stand frame 3
Reinforcing frame 2 includes the hollow reinforcement side lever for being routed through, and body plate 1 is provided with supply corresponding with strengthening side lever The passage being routed through.So as to realize the connection of GPS device and unmanned plane body.
Generally, it is provided by the utility model to be installed on unmanned plane for unmanned plane GPS folding brackets, can be GPS device is set on base.With the rotation of reinforcing frame and stand frame, support can be folded, and then change the position of GPS device Put and direction, so as to prevent signal interference, and can uses and folding space is compact, to facilitate collection and save space. Device overall structure is attractive in appearance, is easy to set, and is set suitable for unmanned plane GPS device.
As shown in Fig. 1,2,3,4,5, for for unmanned plane GPS folding bracket unfoldable shape structure charts.Stand frame 3 is perpendicular Directly, loading end is horizontal.
As shown in Fig. 6,7,8,9,10, for for unmanned plane GPS folding bracket retracted configuration structure charts.With support The rotation of frame 3 and reinforcing frame 2, carry and shunk towards body plate direction.
As shown in Figure 11,12,13,14,15, for for unmanned plane GPS folding bracket folded form structure charts.Support Frame 3 and reinforcing frame 2 are turned to parallel to body plate, and loading end is rotated to bottom, and now loading end is perpendicular to body plate.
Preferred embodiment of the present utility model is the foregoing is only, it is all in this practicality not to limit the utility model Within new spirit and principle, any modification, equivalent substitution and improvements made etc., guarantor of the present utility model should be included in Within the scope of shield.

Claims (6)

1. one kind is used for unmanned plane GPS folding brackets, it is characterised in that comprises at least:
Body plate (1);
Reinforcing frame (2), one end of the reinforcing frame (2) and the body plate (1) are be hinged;
Stand frame (3), one end and the body plate (1) of the stand frame (3) are slidably connected, the stand frame (3) it is another End is provided with base (4), and the stand frame (3) is hinged the another of the reinforcing frame (2) at middle part close to the side of the base (4) One end, the jointed shaft of the reinforcing frame (2) and the body plate (1) is parallel to the reinforcing frame (2) and the stand frame (3) Jointed shaft, the sliding surface of one end that the stand frame (3) is slidably connected with the body plate (1) is parallel to the reinforcing frame (2) With the jointed shaft of the body plate (1).
2. according to claim 1 be used for unmanned plane GPS folding brackets, it is characterised in that:The base (4) is set Have loading end, the loading end rotates with the rotation of the stand frame (3), when the stand frame (3) turn to perpendicular to During body plate (1), the loading end is parallel to the body plate (1);When the stand frame (3) is turned to parallel to described During body plate (1), the loading end is perpendicular to the body plate (1).
3. according to claim 2 be used for unmanned plane GPS folding brackets, it is characterised in that:The loading end is vertical In the stand frame (3).
4. according to claim 2 be used for unmanned plane GPS folding brackets, it is characterised in that:The base (4) is L Shape, its one end are arranged to the loading end, and the other end is fixedly connected on the stand frame (3).
5. according to claim 1 be used for unmanned plane GPS folding brackets, it is characterised in that:The body plate (1) is The jointed shaft of flat board, the reinforcing frame (2) and the body plate (1) is parallel to the body plate (1).
6. it is used for unmanned plane GPS folding brackets according to one of claim 1 to 5, it is characterised in that:The reinforcement Frame (2) is included for the hollow reinforcement side lever that is routed through, and the body plate (1) is provided with strengthens that side lever is corresponding to be supplied with described The passage being routed through.
CN201721216479.8U 2017-09-21 2017-09-21 One kind is used for unmanned plane GPS folding brackets Expired - Fee Related CN207191452U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721216479.8U CN207191452U (en) 2017-09-21 2017-09-21 One kind is used for unmanned plane GPS folding brackets

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721216479.8U CN207191452U (en) 2017-09-21 2017-09-21 One kind is used for unmanned plane GPS folding brackets

Publications (1)

Publication Number Publication Date
CN207191452U true CN207191452U (en) 2018-04-06

Family

ID=61786112

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721216479.8U Expired - Fee Related CN207191452U (en) 2017-09-21 2017-09-21 One kind is used for unmanned plane GPS folding brackets

Country Status (1)

Country Link
CN (1) CN207191452U (en)

Similar Documents

Publication Publication Date Title
CN106892128A (en) The multi-functional landing platform of rotor wing unmanned aerial vehicle
CN207997972U (en) A kind of foldable unmanned plane
CN104260873B (en) A kind of delta-wing aircraft
CN106347625A (en) Unmanned aerial vehicle linkage folding mechanism
CN106444734A (en) Portable ground station
CN206654205U (en) The multi-functional landing platform of rotor wing unmanned aerial vehicle
CN207191452U (en) One kind is used for unmanned plane GPS folding brackets
CN207997975U (en) A kind of undercarriage keeping unmanned plane level
CN205273841U (en) Foot rest subassembly and aircraft
CN209938948U (en) Coaxial rotor unmanned aerial vehicle of folded cascade
CN206107543U (en) Unmanned aerial vehicle folding mechanism that links
CN208102325U (en) Power wing body multi-rotor unmanned aerial vehicle
CN206664930U (en) Collapsible unmanned plane
CN206782066U (en) A kind of horn structure for being used to combine gyroplane
CN209441629U (en) A kind of compact unmanned plane
CN107757898A (en) One kind is taken photo by plane folding wings unmanned plane
CN210235307U (en) Airplane with folding tail wing
CN107472515A (en) Six rotors are taken photo by plane unmanned plane and its wing arm Fast detachable unit
CN205524956U (en) Portable aircraft
CN205738080U (en) A kind of unmanned plane attaching to vertical
CN205499343U (en) Flat electronic foot rest of formula of rolling over
CN208963311U (en) A kind of tail pushes away rotor mixed layout unmanned plane
CN203246484U (en) Novel luggage barrow
CN208264571U (en) It is a kind of for hanging the unmanned plane for sending operation
CN207106307U (en) A kind of draw off gear of vehicle-mounted unmanned aerial vehicle

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: 20180406