CN205186517U - Folding mechanism that unmanned aerial vehicle used - Google Patents
Folding mechanism that unmanned aerial vehicle used Download PDFInfo
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- CN205186517U CN205186517U CN201520838367.0U CN201520838367U CN205186517U CN 205186517 U CN205186517 U CN 205186517U CN 201520838367 U CN201520838367 U CN 201520838367U CN 205186517 U CN205186517 U CN 205186517U
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- unmanned plane
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Abstract
The utility model discloses a folding mechanism that unmanned aerial vehicle used. Including fixed base plate (14), the lower surface of fixed base plate (14) is equipped with runing rest (15), and runing rest (15) are connected with arm hoop (16), other be equipped with horizontal fixation clamp (17) of arm hoop (16), arm hoop (16) including base (18), the both ends of base (18) all are equipped with rotation axis core (20), rotation axis core (20) are connected with runing rest (15), still are equipped with two arc fixed arm (21) on base (18). The utility model has the characteristics of effectively reduced unmanned aerial vehicle occupation space, reduce the traffic -induced damage risk, the principle is simple and low in manufacturing cost.
Description
Technical field
The utility model relates to a kind of fold mechanism of unmanned plane of field of taking photo by plane, particularly a kind of fold mechanism of unmanned plane.
Background technology
Along with the development of society, the application of unmanned plane is more and more wider, current use unmanned plane is taken photo by plane and is also come in the life of average family, the universal of its use has benefited from, use take photo by plane helicopter aerial photography of comparing of unmanned plane with low cost, and the personnel of taking photo by plane stand in ground can manipulate unmanned plane by remote controller and complete shooting, not only simple to operate, and without the need to the personnel's of taking photo by plane operation aloft, add the safety factor of shooting process.But mainly there is large, that transport the is inconvenient shortcoming that takes up room in the unmanned plane used of taking photo by plane at present.In order to solve the problem, applicant devises a kind of unmanned plane with folder function, this unmanned plane efficiently solves the problems referred to above, but guarantee that this unmanned function takes up room little and conveniently transports, also need a kind of fold mechanism with the use of just guaranteeing that the hold-down arm of unmanned plane normally folds, but do not find this kind of fold mechanism at present.
Summary of the invention
The purpose of this utility model is, provides a kind of fold mechanism of unmanned plane.The utility model have effectively reduce the taking up room of unmanned plane, reduce traffic-induced damage risk, the feature of the simple and low cost of manufacture of principle.
The technical solution of the utility model: a kind of fold mechanism of unmanned plane, comprises fixing base, the lower surface of fixing base is provided with swinging strut, and swinging strut is connected with arm hoop, and arm hoop is other is provided with horizontal geometrical clamp; Described arm hoop comprises base, and the two ends of base are equipped with S. A. core, and S. A. core is connected with swinging strut, base is also provided with two arc fixed arms.
In the fold mechanism of aforesaid unmanned plane, the head end of two described arc fixed arms connects through fix screw.
In the fold mechanism of aforesaid unmanned plane, described horizontal geometrical clamp comprises horizontal fixed end, and the lower surface of horizontal fixed end is provided with two horizontal free ends, and be provided with between two horizontal free ends and laterally clamp mouth, the upper surface of horizontal fixed end is connected with fixing base.
In the fold mechanism of aforesaid unmanned plane, described fixing base is also connected with vertical supporting plate, and vertical supporting plate is provided with vertical geometrical clamp; Described vertical geometrical clamp comprises vertical fixed end, and a surface of vertical fixed end is provided with two vertical free ends, is provided with and vertically clamps mouth between two vertical free ends, and another surface of vertical fixed end is connected with vertical supporting plate.
Compared with prior art, the utility model arranges swinging strut at fixing base lower surface, and swinging strut is connected with arm hoop through S. A. core, and arm hoop is provided with two arc fixed arms, and arm hoop is other is provided with horizontal geometrical clamp; In use, fixing base is fixed on the pedestal of unmanned plane, between two the arc fixed arms hold-down arm end of unmanned plane being snapped in arm hoop, now hold-down arm can rotate around the axis of S. A. core, when hold-down arm turns to level attitude, the transverse direction snapping in horizontal geometrical clamp clamps in mouth to complete fixes the level of hold-down arm, then enables unmanned plane normal flight, when depositing or transport, draw in by hold-down arm disengaging horizontal clamping mouth and around the axis rotation of S. A. core to vertical direction; Taking up room of unmanned plane is effectively reduced by this structure; The utility model is also provided with vertical geometrical clamp, when hold-down arm vertically draws in, snaps in the vertical clamping mouth internal fixtion of vertical geometrical clamp, avoids the hold-down arm when transporting and produces the situation of rocking, thus reduce unmanned plane with carry in the risk damaged.The utility model is fixed to time horizontal or vertical by rotating the hold-down arm of unmanned plane, completes the folding of unmanned plane, the simple low cost of manufacture of its principle.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the connection structure schematic diagram of the utility model and hold-down arm;
Fig. 3 is the structural representation of unmanned plane;
Fig. 4 is the structural representation that unmanned plane overlooks direction.
Being labeled as in accompanying drawing: 1-pedestal, 2-antenna, 3-flies to control device, 4-battery bracket, 5-power brick, 6-digital high-definition figure passes, 7-tri-axle The Cloud Terrace, 8-high-definition camera, 9-fold mechanism, 10-lift unit, 11-hold-down arm, 12-lift motor, 13-screw propeller, 14-fixing base, 15-swinging strut, 16-arm hoop, the horizontal geometrical clamp of 17-, 18-base, 19-vertically clamps mouth, 20-S. A. core, 21-arc fixed arm, 22-fix screw, the horizontal fixed end of 23-, the horizontal free end of 24-, 25-laterally clamps mouth, 26-vertical supporting plate, the vertical geometrical clamp of 27-, the vertical fixed end of 28-, the vertical free end of 29-.
Detailed description of the invention
Below in conjunction with drawings and Examples, the utility model is further described, but not as the foundation limited the utility model.
Embodiment.A fold mechanism for unmanned plane, this fold mechanism 9 forms as shown in Figure 1, comprises fixing base 14, and the lower surface of fixing base 14 is provided with swinging strut 15, and swinging strut 15 is connected with arm hoop 16, and arm hoop 16 is other is provided with horizontal geometrical clamp 17; Described arm hoop 16 comprises base 18, and the two ends of base 18 are equipped with S. A. core 20, and S. A. core 20 is connected with swinging strut 15, base 18 is also provided with two arc fixed arms 21.By this structure, clamped by two arc fixed arms 21 by the end of hold-down arm 11 and make the end of hold-down arm 11 be fixed on arm hoop 16, hold-down arm 11 just can rotate around the axis of S. A. core 20, and then realizes the horizontal spreading of hold-down arm 11 and vertically draw in.
The head end of aforesaid two arc fixed arms 21 connects through fix screw 22.Fix screw 22 can tighten up two arc fixed arms 21, hold-down arm 11 is held tighter, prevents from coming off.
Aforesaid horizontal geometrical clamp 17 comprises horizontal fixed end 23, and the lower surface of horizontal fixed end 23 is provided with between two horizontal free ends 24 of horizontal free end 24, two and is provided with laterally clamping mouth 25, and the upper surface of horizontal fixed end 23 is connected with fixing base 14.By this structure, hold-down arm 11 is entered into by horizontal free end 24 and laterally clamps in mouth 25, and is jammed, and then makes hold-down arm 11 keep horizontality; When drawing hold-down arm 11 in, hold-down arm 11 departs from horizontal clamping mouth 25 and axis around S. A. core 20 rotates to vertical direction.
Aforesaid fixing base 14 is also connected with vertical supporting plate 26, and vertical supporting plate 26 is provided with vertical geometrical clamp 27; Described vertical geometrical clamp 27 comprises vertical fixed end 28, and a surface of vertical fixed end 28 is provided with between two vertical free ends 29 of vertical free end 29, two and is provided with vertical clamping mouth 19, and another surface of vertical fixed end 28 is connected with vertical supporting plate 26.When hold-down arm 11 is in vertical state, it is interior and clamped that hold-down arm 11 enters vertical clamping mouth 19 by two vertical free ends 29, by this structure, avoid the hold-down arm 11 when transporting and produce the situation of rocking, thus reduce unmanned plane with carry in the risk damaged.
Aforesaid fold mechanism 9 is arranged on to be had in the unmanned plane of folder function, this unmanned plane (as in Figure 2-4) also includes pedestal 1, pedestal 1 is connected with antenna 2, be provided with above pedestal 1 and fly to control device 3, be provided with battery bracket 4 below pedestal 1, battery bracket 4 is provided with power brick 5, is provided with digital high-definition figure and passes 6 below battery bracket 4, battery bracket 4 side is provided with three axle The Cloud Terrace 7, three axle The Cloud Terraces 7 and is provided with high-definition camera 8; Described pedestal 1 is also connected with lift unit 10 through fold mechanism 9; Described lift unit 10 comprises hold-down arm 11, and the head end of hold-down arm 11 is provided with lift motor 12, and lift motor 12 is connected with screw propeller 13, and the end of hold-down arm 11 is connected with fold mechanism 9.
The upper surface of aforesaid fixing base 14 is connected with pedestal 1.
When taking photo by plane, snapped in by hold-down arm 11 in horizontal geometrical clamp 17 and make hold-down arm 11 maintenance level, then make screw propeller 13 maintenance level, remote controller starts lift motor 12 and makes screw propeller 13 rotarily drive unmanned plane lift-off to take photo by plane afterwards; In taking photo by plane, controlled by the heading flying to control device 3 pairs of unmanned planes, flying control device 3 can be GPS (american global positioning system), GLONASS (GLONASS satellite navigation) or COMPASS (Chinese Beidou navigation); The shooting attitude of high-definition camera 8 is adjusted, to photograph better picture by three axle The Cloud Terraces 7; Pass 6 by digital high-definition figure and the picture that high-definition camera 8 is taken is passed to ground in real time, the personnel that conveniently take photo by plane adjust the shooting attitude of unmanned plane during flying attitude and high-definition camera 8 according to real-time pictures.
Claims (4)
1. the fold mechanism of a unmanned plane, it is characterized in that: comprise fixing base (14), the lower surface of fixing base (14) is provided with swinging strut (15), and swinging strut (15) is connected with arm hoop (16), and arm hoop (16) is other is provided with horizontal geometrical clamp (17); Described arm hoop (16) comprises base (18), and the two ends of base (18) are equipped with S. A. core (20), and S. A. core (20) is connected with swinging strut (15), base (18) is also provided with two arc fixed arms (21).
2. the fold mechanism of unmanned plane according to claim 1, is characterized in that: the head end of two described arc fixed arms (21) connects through fix screw (22).
3. the fold mechanism of unmanned plane according to claim 1 and 2, it is characterized in that: described horizontal geometrical clamp (17) comprises horizontal fixed end (23), the lower surface of horizontal fixed end (23) is provided with two horizontal free ends (24), be provided with between two horizontal free ends (24) and laterally clamp mouth (25), the upper surface of horizontal fixed end (23) is connected with fixing base (14).
4. the fold mechanism of unmanned plane according to claim 1 and 2, is characterized in that: described fixing base (14) is also connected with vertical supporting plate (26), and vertical supporting plate (26) is provided with vertical geometrical clamp (27); Described vertical geometrical clamp (27) comprises vertical fixed end (28), a surface of vertical fixed end (28) is provided with two vertical free ends (29), be provided with between two vertical free ends (29) and vertically clamp mouth (19), another surface of vertical fixed end (28) is connected with vertical supporting plate (26).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520838367.0U CN205186517U (en) | 2015-10-27 | 2015-10-27 | Folding mechanism that unmanned aerial vehicle used |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520838367.0U CN205186517U (en) | 2015-10-27 | 2015-10-27 | Folding mechanism that unmanned aerial vehicle used |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205186517U true CN205186517U (en) | 2016-04-27 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520838367.0U Expired - Fee Related CN205186517U (en) | 2015-10-27 | 2015-10-27 | Folding mechanism that unmanned aerial vehicle used |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205186517U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110466736A (en) * | 2019-09-26 | 2019-11-19 | 吉林大学 | A kind of unmanned plane horn folding device and unmanned plane |
-
2015
- 2015-10-27 CN CN201520838367.0U patent/CN205186517U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110466736A (en) * | 2019-09-26 | 2019-11-19 | 吉林大学 | A kind of unmanned plane horn folding device and unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Folding mechanism that unmanned aerial vehicle used Effective date of registration: 20171024 Granted publication date: 20160427 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: GUIZHOU SKYVIEW TECHNOLOGY CO.,LTD. Registration number: 2017990000983 |
|
| PE01 | Entry into force 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: 20190104 Granted publication date: 20160427 Pledgee: Bank of Guiyang Limited by Share Ltd. high tech branch Pledgor: GUIZHOU SKYVIEW TECHNOLOGY CO.,LTD. Registration number: 2017990000983 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160427 Termination date: 20211027 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |