CN204979215U - Foldable unmanned aerial vehicle - Google Patents
Foldable unmanned aerial vehicle Download PDFInfo
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- CN204979215U CN204979215U CN201520540316.XU CN201520540316U CN204979215U CN 204979215 U CN204979215 U CN 204979215U CN 201520540316 U CN201520540316 U CN 201520540316U CN 204979215 U CN204979215 U CN 204979215U
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Abstract
The utility model relates to an unmanned aerial vehicle designs technical field, concretely relates to foldable unmanned aerial vehicle. Foldable unmanned aerial vehicle includes: the organism is I -shapedly, camera cloud platform sets up the bottom side at the organism head, battery pack and flight control all set up inside the organism, the undercarriage rotationally evenly sets up at bottom of the body, four at least horns and take drive arrangement's screw, the one end of four horns articulates four angles at I -shaped organism respectively, horn locking device for when horn rotation to reservation is opened or is booked the closed condition, lock the horn. The utility model discloses a foldable unmanned aerial vehicle, when the horn rotated to predetermined closed condition, the chamber that holds in this side was accomodate completely to two horns that are arranged in the organism homonymy to through the locking of horn locking device, make unmanned aerial vehicle fold back compact structure, the size is less, more conveniently carries, when needs use, can also expand fast, reach the state of flight rapidly.
Description
Technical field
The utility model relates to unmanned aerial vehicle design technical field, is specifically related to a kind of folding unmanned plane.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.Unmanned plane can carry multiple load and complete various complex task, specifically has extensive use in multiple fields such as photography, pesticide spraying, fire protection and rescue, communication, public security anti-terrorism, drug law enforcement anti-smugglings.
But, unmanned plane structure design described in prior art is unreasonable, scantling of structure is larger, a lot of unmanned plane adopts cross layout, horn cannot fold, and most electronics package and battery component etc. are all positioned at the cavity in the middle part of cross layout, stacked on top, take up room large, whole unmanned plane is made to be inconvenient to receive, carry, go out with large-sized knapsack or to be transported by instruments such as automobiles, dismounting parts turn increase Operating Complexity, electrical connector bad contact is easily there is when repeating dismounting, physical construction such as not to lock at the reliability that hidden danger reduces unmanned plane, and waste time and energy.
Summary of the invention
The purpose of this utility model is to provide a kind of folding unmanned plane, to solve above-mentioned at least one technical matters.
The technical solution of the utility model is:
A kind of folding unmanned plane, comprising:
Body, left and right side is all recessed to form as left and right container cavity, and when unmanned plane horizontal positioned, the projection in the horizontal plane of described body is I-shape;
Camera head, is arranged on the bottom side of described body head;
Battery component and flight control system, be all arranged on described internal body;
Alighting gear, is evenly arranged on described organism bottom rotationally;
Horn, comprise at least four, one end of four described horns is hinged on four angles of described double-tee body respectively, each described horn pivot center falls in the upper and lower surface of described body, and be positioned at two described horns on the left of described body with two the described horns be positioned on the right side of described body with the front and back axis of described body for axis of symmetry is symmetrical, in addition, the other end of each described horn is provided with the screw propeller of band actuating device;
Horn latching device, be arranged on position hinged with described horn on described body, during for turning to predetermined unlatching or predetermined closed condition at described horn, described horn is locked, in addition, when described horn turns to described predetermined closed condition, two the described horns being arranged in described body homonymy are accommodated in the described container cavity of this side completely.
Alternatively, the distance of the hinge-point of two described horns on described body of homonymy, is less than the length sum of two described horns, and when described horn turns to described predetermined closed condition, the axis of two described horns of homonymy parallels.
Alternatively, described body comprises upper casing and lower casing;
Upwards caving in the front end of described lower casing is the first resettlement section, for holding the picture pick-up device bottom described camera head and described camera head.
Alternatively,
The front end of described upper casing has the second resettlement section, and the top of described camera head is run through described adapter plate and is fixed by the anchor fitting be arranged in described second resettlement section;
Described second top, resettlement section is provided with the The Cloud Terrace lid that matches, and is fixedly connected with described upper casing, and the header field of described second resettlement section and described first resettlement section is separated into independently the first cavity.
Alternatively, described picture pick-up device is camera.
Alternatively, described battery component is arranged in described internal body cavity, and the rear being positioned at described camera head is near described body tail position;
Described flight control system, is arranged in described internal body cavity, and between described camera head and described battery component.
Alternatively, described internal body cavity is the second cavity formed by described upper casing and described lower casing, and at described body afterbody, there is the opening with the second cavity connects, described opening part is provided with the curved surface control desk with described openings snap-fit, and described curved surface control desk also inserts described battery component from described opening part.
Alternatively, in the corner of described body and the hinged position of described horn, there is the Ban Bao chamber of a depression respectively, described Ban Bao chamber end face by the upper casing of described body part side inwardly and be upwards recessed to form, bottom surface, described Ban Bao chamber by the lower casing of described body part side inwardly and be recessed to form downwards, one end of described horn is positioned at described Ban Bao chamber.
Alternatively, described Ban Bao chamber end face has column-shaped projection, and also there is coaxial column-shaped projection corresponding position, bottom surface, and both coordinate the turning cylinder as described horn;
The upper casing of described horn and lower casing are equipped with cylindrical dimples, and the column-shaped projection of described Ban Bao chamber end face and the cylindrical dimples of described upper casing match, and the described column-shaped projection of bottom surface and the cylindrical dimples of described lower casing match.
Alternatively, described horn inside has cavity, is provided with electronic governor in cavity.
The beneficial effects of the utility model:
Folding unmanned plane of the present utility model, horn is four angles being hinged on body, can be accommodated in completely in the container cavity of homonymy when horn turns to predetermined closed condition, and locked by horn latching device, make unmanned plane folded configuration of the present utility model compact, size is less, more conveniently carries; When it is desired to be used, can also rapid deployment, reach state of flight rapidly.
Accompanying drawing explanation
Fig. 1 is the block diagram of the utility model folding unmanned plane preferred embodiment;
Fig. 2 is the block diagram of the utility model folding unmanned plane The Cloud Terrace lid embodiment illustrated in fig. 1 when opening;
Fig. 3 is the utility model folding unmanned plane front view embodiment illustrated in fig. 1;
Fig. 4 is the structural representation of the utility model folding unmanned plane horn embodiment illustrated in fig. 1 when being in receiving state;
Fig. 5 is the structural representation of the utility model folding unmanned plane horn embodiment illustrated in fig. 1 when being in deployed condition;
Fig. 6 is that the utility model folding unmanned plane middle horn embodiment illustrated in fig. 1 and body junction adopt the structural representation after analysing and observe;
Fig. 7 is the utility model folding unmanned plane middle horn inner structure schematic diagram embodiment illustrated in fig. 1.
Detailed description of the invention
Here will be described exemplary embodiment in detail, its sample table shows in the accompanying drawings.When description below relates to accompanying drawing, unless otherwise indicated, the same numbers in different accompanying drawing represents same or analogous key element.
As shown in Figure 1 and Figure 7, a kind of folding unmanned plane that the utility model provides, comprises body 1, camera head 4, battery component 6, flight control system 7, alighting gear 5 and horn 2.
The left and right side of body 1 is all recessed to form as left and right container cavity, and when unmanned plane horizontal positioned, body 1 projection is in the horizontal plane I-shape.
Camera head 4 is arranged on the bottom side of body 1 head, for arranging picture pick-up device 41; Battery component 6 and flight control system 7 are all arranged on body 1 inside and are applicable to position.
The quantity of alighting gear 5, shape and connection mode can be chosen as multiple applicable mode as required, and it is evenly arranged on bottom body 1 rotationally.Usually when parking to support unmanned plane, can also rotate when needing and store, be convenient for carrying.
Horn 2 comprises at least four, and concrete quantity can be selected as required.In the present embodiment, be preferably four, one end of four horns 2 is hinged on four angles of double-tee body 1 respectively, and each horn 2 pivot center falls in the upper and lower surface of body 1; Further, two horns 2 be positioned on the left of body 1 are for axis of symmetry is symmetrical with the front and back axis of body 1 with two horns 2 be positioned on the right side of body 1; Further, the other end of each horn 2 is provided with the screw propeller 8 of band actuating device, and driving device structure can adopt multiple applicable structure known at present, can comprise such as motor, belt etc., repeat no more herein.
Horn latching device 3 is arranged on position hinged with horn 2 on body 1 usually, during for turning to predetermined unlatching or predetermined closed condition at horn 2, is locked by horn 2; Equally, horn latching device 3 can adopt multiple applicable shape and structure equally, and the fixed form that such as can directly adopt pin-and-hole to coordinate, repeats no more herein.In addition, in the middle part of body 1, outside and horn 2 outer contoured shape after folding are consistent, the space that horn 2 is folding can be retained, more can ensure that intrinsic control installing space is sufficient, when horn 2 turns to predetermined closed condition, two horns 2 being arranged in body 1 homonymy are accommodated in the container cavity of this side completely.It should be noted that, predetermined opening refer to unmanned plane can normal flight time horn 2 deployed condition, predetermined closed condition refers to that horn 2 is accommodated in the state in the container cavity of this side completely.
In folding unmanned plane of the present utility model, horn 2 is four angles being hinged on body 1, can be accommodated in completely in the container cavity of homonymy when horn 2 turns to predetermined closed condition, and locked by horn latching device 3, make unmanned plane folded configuration of the present utility model compact, size is less, more conveniently carries; Meanwhile, when needing to use, can rapid deployment, reach state of flight rapidly.
In folding unmanned plane of the present utility model, the distance of the hinge-point of two horns 2 on body 1 of homonymy, is less than the length sum of two horns 2, and when horn 2 turns to predetermined closed condition, the axis of two horns 2 of homonymy parallels.Such structure can make the entire length of body 1 reduce, and weight saving, carries more convenient.
When horn 2 launches, folding horn latching device 3 is locked and alighting gear 5 launches time, aircraft can take off at any time, realizes freely taking of camera.When horn 2 folds, folding horn latching device 3 is opened and gear up, and aircraft is in folded state, compact, can receive with oneself, be convenient for carrying.
Body 1 comprises upper casing 16 and lower casing 11; Upwards caving in the front end of lower casing 11 is the first resettlement section 12, for holding the picture pick-up device 41 bottom camera head 4 and camera head 4.Picture pick-up device 41 can be pick up camera, camera etc., is preferably camera in the present embodiment.
Further, have the second resettlement section 9 in the front end of upper casing 16, the top of camera head 4 is run through the top board of the first resettlement section 12 and is fixed by the anchor fitting be arranged in the second resettlement section 9, and anchor fitting can be bolt.
Second top, resettlement section 9 is provided with the The Cloud Terrace lid 13 that matches,
Be fixedly connected with described upper casing 16, and the header field of described second resettlement section 9 and described first resettlement section 12 is separated into independently the first cavity.
Battery component 6 is arranged in body 1 internal cavities, and the rear being positioned at camera head 4 is near body 1 tail position; Further, the second cavity 17 (in I-shape long and narrow flats cavity) is formed by upper casing 16 and lower casing 11 in body 1 inside, battery component 6 is arranged in the second cavity 17, and there is at body 1 afterbody the opening be communicated with the second cavity 17, opening part is provided with the curved surface control desk 61 with openings snap-fit, and curved surface control desk 61 also inserts described battery component 6 from opening part.
Flight control system 7 is arranged in body 1 second cavity 17 equally, and between camera head 4 and battery component 6.Battery component 6 makes unmanned plane integral structure compacter with the set-up mode of flight control system 7, can reduce the volume and weight of unmanned plane.
Further, in the corner of body 1 and the hinged position of horn 2, there is the Ban Bao chamber 18 of a depression respectively, Ban Bao chamber 18 end face by the upper casing 16 of body 1 part side inwardly and be upwards recessed to form, bottom surface, Ban Bao chamber 18 by the lower casing 11 of body 1 part side inwardly and be recessed to form downwards, one end of horn 2 is positioned at described Ban Bao chamber 18.
Ban Bao chamber 18 end face has column-shaped projection 19, and also there is coaxial column-shaped projection 19 corresponding position, bottom surface, and both coordinate the turning cylinder as horn 2; In addition, the cylindrical dimples 21 of column-shaped projection 19 and upper casing 16 that the upper casing 16 of horn 2 and lower casing 11 are equipped with cylindrical dimples 21, Ban Bao chamber 18 end face matches, and the column-shaped projection 19 of bottom surface and the cylindrical dimples 21 of lower casing 11 match, and make structure more firmly compact.
Horn 2 inside of the present utility model has individual cavities, is provided with electronic governor 10 in cavity, and electronic governor 10 and aircraft control system are carried out split design, when occurring damaging, can change separately, reducing maintenance cost; The interference to flying in fuselage to control can be reduced, and save body space, animal economy profile is reduced; Near screw propeller motor arrangement, cabling can be reduced.
The above; be only detailed description of the invention of the present utility model; but protection domain of the present utility model is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that the utility model discloses; the change that can expect easily or replacement, all should be encompassed within protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with the protection domain of described claim.
Claims (10)
1. a folding unmanned plane, is characterized in that, comprising:
Body (1), left and right side is all recessed to form as left and right container cavity, and when unmanned plane horizontal positioned, described body (1) projection is in the horizontal plane I-shape;
Camera head (4), is arranged on the bottom side of described body (1) head;
Battery component (6) and flight control system (7), be all arranged on described body (1) inner;
Alighting gear (5), is evenly arranged on described body (1) bottom rotationally;
Horn (2), comprise at least four, one end of four described horns (2) is hinged on four angles of described double-tee body (1) respectively, each described horn (2) pivot center falls in the upper and lower surface of described body (1), and two the described horns (2) being positioned at described body (1) left side are that axis of symmetry is symmetrical with two the described horns (2) be positioned on the right side of described body (1) with the front and back axis of described body (1), in addition, the other end of each described horn (2) is provided with the screw propeller (8) of band actuating device,
Horn latching device (3), be arranged on the position that described body (1) is upper and described horn (2) is hinged, during for turning to predetermined unlatching or predetermined closed condition at described horn (2), described horn (2) is locked, in addition, when described horn (2) turns to described predetermined closed condition, two the described horns (2) being arranged in described body (1) homonymy are accommodated in the described container cavity of this side completely.
2. folding unmanned plane according to claim 1, it is characterized in that, the distance of the hinge-point of two described horns (2) on described body (1) of homonymy is less than the length sum of two described horns (2), and when described horn (2) turns to described predetermined closed condition, the axis of two described horns (2) of homonymy parallels.
3. folding unmanned plane according to claim 1 and 2, is characterized in that, described body (1) comprises upper casing (16) and lower casing (11);
Upwards caving in the front end of described lower casing (11) is the first resettlement section (12), for holding the picture pick-up device (41) of described camera head (4) and described camera head (4) bottom.
4. folding unmanned plane according to claim 3, it is characterized in that, the front end of described upper casing (16) has the second resettlement section (9), and the top of described camera head (4) is run through described adapter plate and is fixed by the anchor fitting be arranged in described second resettlement section (9);
Described second resettlement section (9) top is provided with the The Cloud Terrace lid (13) that matches, be fixedly connected with described upper casing (16), and the header field of described second resettlement section (9) and described first resettlement section (12) is separated into independently the first cavity.
5. folding unmanned plane according to claim 4, is characterized in that, described picture pick-up device (41) is camera.
6. folding unmanned plane according to claim 3, it is characterized in that, described battery component (6) is arranged in described body (1) internal cavities, and the rear being positioned at described camera head (4) is near described body (1) tail position;
Described flight control system (7), is arranged in described body (1) internal cavities, and is positioned between described camera head (4) and described battery component (6).
7. folding unmanned plane according to claim 6, it is characterized in that, described body (1) internal cavities is the second cavity (17) formed by described upper casing (16) and described lower casing (11), and there is at described body (1) afterbody the opening be communicated with the second cavity (17), described opening part is provided with the curved surface control desk (61) with described openings snap-fit, and described curved surface control desk (61) also inserts described battery component (6) from described opening part.
8. folding unmanned plane according to claim 3, it is characterized in that, in the corner of described body (1) and the hinged position of described horn (2), there is the Ban Bao chamber (18) of a depression respectively, described Ban Bao chamber (18) end face by the upper casing (16) of described body (1) part side inwardly and be upwards recessed to form, described Ban Bao chamber (18) bottom surface by the lower casing (11) of described body (1) part side inwardly and be recessed to form downwards.
9. folding unmanned plane according to claim 8, it is characterized in that, described Ban Bao chamber (18) end face has column-shaped projection (19), also there is coaxial column-shaped projection (19) corresponding position, bottom surface, and both coordinate the turning cylinder as described horn (2);
The upper casing (16) of described horn (2) and lower casing (11) are equipped with cylindrical dimples (21), the described column-shaped projection (19) of Ban Bao chamber (18) end face and the cylindrical dimples (21) of described upper casing (16) match, and the described column-shaped projection (19) of bottom surface and the cylindrical dimples (21) of described lower casing (11) match.
10. folding unmanned plane according to claim 1, is characterized in that, described horn (2) inside has cavity, is provided with electronic governor (10) in cavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520540316.XU CN204979215U (en) | 2015-07-23 | 2015-07-23 | Foldable unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520540316.XU CN204979215U (en) | 2015-07-23 | 2015-07-23 | Foldable unmanned aerial vehicle |
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| Publication Number | Publication Date |
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| CN204979215U true CN204979215U (en) | 2016-01-20 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520540316.XU Withdrawn - After Issue CN204979215U (en) | 2015-07-23 | 2015-07-23 | Foldable unmanned aerial vehicle |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105059528A (en) * | 2015-07-23 | 2015-11-18 | 致导科技（北京）有限公司 | Foldable unmanned aerial vehicle |
| WO2017128317A1 (en) * | 2016-01-29 | 2017-08-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and aerial photographing method for unmanned aerial vehicle |
| CN107079090A (en) * | 2016-04-21 | 2017-08-18 | 深圳市大疆创新科技有限公司 | Unmanned plane and camera assembly |
| WO2017143643A1 (en) * | 2016-02-22 | 2017-08-31 | 深圳市大疆创新科技有限公司 | Frame of unmanned aerial vehicle, unmanned aerial vehicle, and use method therefor |
| EP3272652A4 (en) * | 2016-05-27 | 2018-05-23 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| WO2018112798A1 (en) * | 2016-12-21 | 2018-06-28 | XDynamics Limited | Unmanned aerial vehicle |
| CN108495786A (en) * | 2017-08-31 | 2018-09-04 | 深圳市大疆创新科技有限公司 | The deformation rack and aircraft of aircraft |
| US10093418B2 (en) | 2016-05-27 | 2018-10-09 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| WO2019037242A1 (en) * | 2017-08-25 | 2019-02-28 | 深圳市大疆创新科技有限公司 | Arm assembly, frame, and unmanned aerial vehicle |
| CN117446233A (en) * | 2023-09-21 | 2024-01-26 | 彭阳县自然资源局 | Measurement device for urban and rural planning and design |
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2015
- 2015-07-23 CN CN201520540316.XU patent/CN204979215U/en not_active Withdrawn - After Issue
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN105059528A (en) * | 2015-07-23 | 2015-11-18 | 致导科技（北京）有限公司 | Foldable unmanned aerial vehicle |
| CN105059528B (en) * | 2015-07-23 | 2017-12-12 | 致导科技（北京）有限公司 | A kind of folding unmanned plane |
| WO2017128317A1 (en) * | 2016-01-29 | 2017-08-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and aerial photographing method for unmanned aerial vehicle |
| US11427319B2 (en) | 2016-02-22 | 2022-08-30 | SZ DJI Technology Co., Ltd. | Foldable multi-rotor aerial vehicle |
| WO2017143643A1 (en) * | 2016-02-22 | 2017-08-31 | 深圳市大疆创新科技有限公司 | Frame of unmanned aerial vehicle, unmanned aerial vehicle, and use method therefor |
| WO2017143501A1 (en) * | 2016-02-22 | 2017-08-31 | SZ DJI Technology Co., Ltd. | Foldable multi-rotor aerial vehicle |
| WO2017143645A1 (en) * | 2016-02-22 | 2017-08-31 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and frame thereof, kit, assembly method, and operation method |
| US10625855B2 (en) | 2016-02-22 | 2020-04-21 | SZ DJI Technology Co., Ltd. | Foldable multi-rotor aerial vehicle |
| WO2017181387A1 (en) * | 2016-04-21 | 2017-10-26 | 深圳市大疆创新科技有限公司 | Unmanned aircraft and camera assembly |
| CN107079090B (en) * | 2016-04-21 | 2019-03-08 | 深圳市大疆创新科技有限公司 | Unmanned plane and camera assembly |
| CN107079090A (en) * | 2016-04-21 | 2017-08-18 | 深圳市大疆创新科技有限公司 | Unmanned plane and camera assembly |
| EP3272652A4 (en) * | 2016-05-27 | 2018-05-23 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| US10093418B2 (en) | 2016-05-27 | 2018-10-09 | Uvify Co., Ltd. | Unmanned aerial vehicle |
| WO2018112798A1 (en) * | 2016-12-21 | 2018-06-28 | XDynamics Limited | Unmanned aerial vehicle |
| CN110382350A (en) * | 2017-08-25 | 2019-10-25 | 深圳市大疆创新科技有限公司 | Horn component, rack and unmanned vehicle |
| WO2019037242A1 (en) * | 2017-08-25 | 2019-02-28 | 深圳市大疆创新科技有限公司 | Arm assembly, frame, and unmanned aerial vehicle |
| WO2019041221A1 (en) * | 2017-08-31 | 2019-03-07 | 深圳市大疆创新科技有限公司 | Deformable frame of aerial vehicle and aerial vehicle |
| CN108495786B (en) * | 2017-08-31 | 2022-01-28 | 深圳市大疆创新科技有限公司 | Deformation frame of aircraft and aircraft |
| CN108495786A (en) * | 2017-08-31 | 2018-09-04 | 深圳市大疆创新科技有限公司 | The deformation rack and aircraft of aircraft |
| CN117446233A (en) * | 2023-09-21 | 2024-01-26 | 彭阳县自然资源局 | Measurement device for urban and rural planning and design |
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| C14 | Grant of patent or utility model | ||
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| AV01 | Patent right actively abandoned |
Granted publication date: 20160120 Effective date of abandoning: 20171212 |
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| AV01 | Patent right actively abandoned |