CN205633049U - Collapsible many rotor unmanned aerial vehicle of horn - Google Patents
Collapsible many rotor unmanned aerial vehicle of horn Download PDFInfo
- Publication number
- CN205633049U CN205633049U CN201620290103.0U CN201620290103U CN205633049U CN 205633049 U CN205633049 U CN 205633049U CN 201620290103 U CN201620290103 U CN 201620290103U CN 205633049 U CN205633049 U CN 205633049U
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- horn
- unmanned aerial
- motor
- many rotor
- aerial vehicles
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Abstract
The utility model relates to a collapsible many rotor unmanned aerial vehicle of horn, including well core plate, foot rest, horn, motor cabinet, motor, screw and antenna, core plate below during the foot rest is located, core plate top during the antenna is located, horn one end is passed through joint portion and is linked to each other with well core plate, and the horn other end links to each other with the motor cabinet, and the motor is installed on the motor cabinet, and the screw is installed on the motor, joint portion includes reset spring, card strip and connecting portion, and connecting portion include the connecting plate of two relative settings, and the horn is through round pin axle and two connecting plate hinged, the card strip transversely runs through two connecting plates, be equipped with the guide way on the connecting plate, guide way horizontal migration can be followed to the card strip, is equipped with and blocks the bayonet socket of an adaptation on the horn. The utility model discloses between well horn and well core plate swing joint, when unmanned aerial vehicle collects, the trouble of having avoided the relapse to dismantle has reduced many rotors unmanned aerial vehicle's collection size, has solved the be not convenient for difficult problem of transportation collection of many rotors unmanned aerial vehicle.
Description
Technical field
This utility model relates to field of mechanical technique, particularly relates to a kind of collapsible many rotor wing unmanned aerial vehicles of horn.
Background technology
Many rotor wing unmanned aerial vehicles control multiple propellers by multiple motors and realize flight, be widely used in take photo by plane, monitor, search and rescue, the every field such as resource exploration, agricultural, have that volume is little, lightweight, expense is low, flexible operation and a safety high.Many rotor wing unmanned aerial vehicles have more horn, when collecting unmanned plane, need to twist off screw, are disassembled by horn and could preferably transport, repeatedly dismantle and install and both wasted time, also accelerate the abrasion of part.
Utility model content
This utility model aims to provide a kind of installation and removal collapsible many rotor wing unmanned aerial vehicles of convenient horn.
For reaching above-mentioned purpose, the technical solution adopted in the utility model is as follows:
A kind of collapsible many rotor wing unmanned aerial vehicles of horn, including central plate, foot rest, horn, motor cabinet, motor, propeller and antenna, described foot rest is located at below central plate, described antenna is located at above central plate, described horn one end is connected with central plate by joint portion, the horn other end is connected with motor cabinet, and motor is arranged on motor cabinet, and propeller is arranged on motor；
Described joint portion includes that back-moving spring, card article and connecting portion, described connecting portion include two connecting plates being oppositely arranged, and described horn is hinged by bearing pin and two connecting plates；Card article extends transversely through two connecting plates；Described connecting plate is provided with gathering sill, and card article can move horizontally along gathering sill, and back-moving spring be arranged in parallel with gathering sill, and described back-moving spring one end is connected with card article, and the other end of back-moving spring is connected with connecting portion, and described horn is provided with the bayonet socket adaptive with card article.
Further, the end of described card article is equipped with and pushes away torsion, described in push away the diameter of the torsion vertical size more than gathering sill.
Further, described card article is positioned at inner side above bearing pin.
Preferably, described central plate includes controller and two horizontally disposed flat boards, and two flat boards are connected by column, column and controller between two flat boards, the most at least 3, described horn and column.
Further, it is provided with suspension holdfast bottom described central plate.
Further, described motor cabinet is provided with two motors, and motor is respectively arranged on end face and the bottom surface of motor cabinet.
Preferably, described flat board is rectangle, and four angles of flat board are equipped with the lug of extension, and with flat board in one plane, described connecting plate is arranged on lug described lug.
Further, described motor cabinet includes the placement ring of top board, base plate and loop configuration, described top board is connected with placing top surface of ring, described base plate is connected with placing ring bottom surface, described placement ring side is provided with the clamping part of tubulose, described top board and base plate are provided with motor installing hole and axis hole, and described clamping part is connected with horn.
Further, described flat board is threadeded with column.
Preferably, described horn has 4, and described column has 8.
Compared with prior art, this utility model has the advantages that
1. this utility model is flexibly connected between horn with central plate; when unmanned plane is collected, by inwardly promoting card article just can draw horn in, it is to avoid the trouble repeatedly dismantled; reduce the collection size of many rotor wing unmanned aerial vehicles, solve a difficult problem for the not readily transportable collection of many rotor wing unmanned aerial vehicles；
2. this utility model simple in construction, easy installation and removal；Its light structure, rationally distributed, greatly reduce the weight of unmanned plane self, add the flight time of unmanned plane；
3. the motor cabinet that this utility model provides, motor is installed on top board and base plate, and top board and base plate are arranged on placement ring, mount and dismount very convenient.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation (horn is in open mode) of joint portion；
Fig. 3 is the structural representation (horn is in rounding state) of joint portion；
Fig. 4 is the structural representation pushing away torsion；
Fig. 5 is the axonometric chart of joint portion；
Fig. 6 is the structural representation of horn；
Fig. 7 is the structural representation of central plate；
Fig. 8 is the structural representation of motor cabinet；
In figure: 1-central plate, 2-foot rest, 3-suspension holdfast, 4-horn, 5-motor cabinet, 6-motor, 7-propeller, 8-antenna, 9-connecting portion, 10-back-moving spring, 11-card article, 12-bayonet socket, 13-bearing pin, 14-gathering sill, 15-pushes away torsion, 17-spring anchor block, 18-flat board, 19-column, 20-lug, 21-base plate, 22-places ring, 23-top board, 24-clamping part, 25-motor installing hole, 26-axis hole 27-groove, 28-mounting lug, 29-cable hole, 30-screwed hole A, 31-screwed hole B, 32-bar hole.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with accompanying drawing, this utility model is further elaborated.
As shown in Figure 1, the collapsible many rotor wing unmanned aerial vehicles of horn disclosed in this utility model, including central plate 1, foot rest 2, horn 4, motor cabinet 5, motor 6, propeller 7 and antenna 8, foot rest 2 is located at below central plate 1, antenna 8 is located at above central plate 1, and horn 4 one end is connected with central plate 1 by joint portion, and horn 4 other end is connected with motor cabinet 5, motor 6 is arranged on motor cabinet 5, and propeller 7 is arranged on motor 6.Further, motor cabinet 5 is provided with two motors 6, and motor 6 is respectively arranged on end face and the bottom surface of motor cabinet 5.The blade of propeller 7 has two.
As shown in Figure 2,3, joint portion includes back-moving spring 10, card article 11 and connecting portion 9, and connecting portion 9 includes two connecting plates being oppositely arranged, and horn 4 is hinged with two connecting plates by bearing pin 13；Card article 11 extends transversely through two connecting plates；Connecting plate is provided with gathering sill 14, card article 11 can move horizontally along gathering sill 14, back-moving spring 10 be arranged in parallel with gathering sill 14, back-moving spring 10 one end is connected with card article 11, the other end of back-moving spring 10 is connected with connecting portion 9, preferably, two connecting plates are provided with spring anchor block 17 away from one end of horn 4, and the other end of back-moving spring 10 is fixed on spring anchor block 17.Horn 4 is provided with and the bayonet socket 12 of card article 11 adaptation.Further, as shown in Figure 4, the end of card article 11 is equipped with and pushes away torsion 15, pushes away the diameter the turning round 15 vertical size more than gathering sill 14.Card article 11 is positioned at inner side above bearing pin 13.
As shown in Figure 5,6, the parallel contiguous block 16 being provided with two tabulars in the end of horn 4 one end, contiguous block 16 is provided with and the axis hole of bearing pin 11 adaptation.During use, holding and push away torsion and 15 inwardly promotes card article 11 along gathering sill 14, card article 11 exits from bayonet socket 12, and horn 4 rotates down around bearing pin 13 under self gravitation effect, and horn 11 is heart gathering in unmanned plane.Contiguous block 16 end face is arc, when needing to strut horn 1, hold horn 4, being rotated up horn 4, the curved end of contiguous block 16 promotes card article to move along gathering sill 14, when horn 4 is parallel with gathering sill 14, elastic force due to back-moving spring 10, in card article 11 automatic clamping card inlet 16, under the barrier effect of back-moving spring and card article 11, horn 4 cannot rotate.
Preferably, as it is shown in fig. 7, central plate 1 includes that controller and two horizontally disposed flat boards 18, two flat boards 18 are connected by column 19, column 19 and controller, between two flat boards 18, can be placed circuit board etc. between two flat boards 18, save space；The most at least 3, horn 4 and column 19, it is preferred that horn 4 has 4, and column 19 has 8.For convenience of Fast Installation, flat board 18 can be threaded connection with column 19.Further, it is provided with suspension holdfast 3 bottom central plate 1.Preferably, flat board 18 is rectangle, and four angles of flat board 18 are equipped with the lug 20 of extension, and with flat board 18 in one plane, connecting plate is connected lug 20 with lug 20, it is preferred that connecting plate is connected with lug 20 bolt.
Further, as shown in Figure 8, motor cabinet 5 includes the placement ring 22 of top board 23, base plate 21 and loop configuration, top board 23 is connected with placing ring 22 end face, and base plate 21 is connected with placing ring 22 bottom surface, places ring 22 side and is provided with the clamping part 24 of tubulose, top board 23 and base plate 21 are provided with motor installing hole 25 and axis hole 26, motor installing hole 25 has 4, and motor installing hole 25 is distributed on axis hole 26 periphery, and clamping part 24 is connected with horn 4.
Two motors 6 are separately mounted on top board 23 and base plate 21；Motor 6 is mounted remotely from
The side of clamping part 24.The front and back of clamping part 24 is respectively equipped with a groove 27, and groove 27 runs through the outer face of clamping part 24, the axis of clamping part 24 and two grooves 27 and is positioned at same level；The outer end of groove 27 is provided with a pair mounting lug 28, two mounting lugs 28 are respectively arranged on the upper side and lower side of groove 27, and mounting lug 28 is provided with screwed hole, is provided with bolt in screwed hole, looser a bolt during use, tight a bolt again after clamping part 24 is enclosed within horn 4.The front and back placing ring 22 is provided with bar hole 32, with heat radiation；Top board 23 and base plate 21 are provided with cable hole 29；The material of top board 23 and base plate 21 is carbon fibre, and the material placing ring 22 is aluminium alloy.
Top board 23 and base plate 21 are connected with placing ring 22 screw.Preferably, motor cabinet 5 outer face is cylinder, motor cabinet 5 inner face is plane, outer face is bigger than the horizontal size of inner face, it is respectively equipped with a screwed hole A30 at four angles of top board 23 and base plate 21, places ring 22 end face and bottom surface is provided with the screwed hole B31 adaptive with screwed hole A30, motor 6 is arranged on top board 23 and base plate 21 during use, top board 23 and base plate 21 being arranged on placement ring 22 with screw, installation and removal are quite convenient to.
Certainly; this utility model also can have other numerous embodiments; in the case of without departing substantially from this utility model spirit and essence thereof; those of ordinary skill in the art can make various corresponding change and deformation according to this utility model, but these change accordingly and deformation all should belong to the scope of the claims appended by this utility model.
Claims (10)
1. the collapsible many rotor wing unmanned aerial vehicles of horn, it is characterized in that: include central plate (1), foot rest (2), horn (4), motor cabinet (5), motor (6), propeller (7) and antenna (8), central plate (1) lower section is located at by described foot rest (2), central plate (1) top is located at by described antenna (8), described horn (4) one end is connected with central plate (1) by joint portion, horn (4) other end is connected with motor cabinet (5), motor (6) is arranged on motor cabinet (5), propeller (7) is arranged on motor (6)；
Described joint portion includes back-moving spring (10), card article (11) and connecting portion (9), described connecting portion (9) includes two connecting plates being oppositely arranged, and described horn (4) is hinged with two connecting plates by bearing pin (13)；Card article (11) extends transversely through two connecting plates；Described connecting plate is provided with gathering sill (14), card article (11) can move horizontally along gathering sill (14), back-moving spring (10) be arranged in parallel with gathering sill (14), described back-moving spring (10) one end is connected with card article (11), the other end of back-moving spring (10) is connected with connecting portion (9), and described horn (4) is provided with the bayonet socket (12) adaptive with card article (11).
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: the end of described card article (11) is equipped with and pushes away torsion (15), described in push away the diameter of torsion (15) the vertical size more than gathering sill (14).
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: described card article (11) is positioned at inside bearing pin (13) top.
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterized in that: described central plate (1) includes controller and two horizontally disposed flat boards (18), two flat boards (18) are connected by column (19), column (19) and controller are positioned between two flat boards (18), described horn (4) and the most at least 3, column (19).
5. according to the many rotor wing unmanned aerial vehicles described in claim 1 or 4, it is characterised in that: described central plate (1) bottom is provided with suspension holdfast (3).
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: described motor cabinet (5) is provided with two motors (6), and motor (6) is respectively arranged on end face and the bottom surface of motor cabinet (5).
Many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterized in that: described flat board (18) is rectangle, the lug (20) of extension it is equipped with on four angles of flat board (18), with flat board (18) in one plane, described connecting plate is arranged on lug (20) described lug (20).
Many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterized in that: described motor cabinet (5) includes top board (23), the placement ring (22) of base plate (21) and loop configuration, described top board (23) is connected with placing ring (22) end face, described base plate (21) is connected with placing ring (22) bottom surface, described placement ring (22) side is provided with the clamping part (24) of tubulose, described top board (23) and base plate (21) are provided with motor installing hole (25) and axis hole (26), described clamping part (24) is connected with horn (4).
Many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterised in that: described flat board (18) is threadeded with column (19).
Many rotor wing unmanned aerial vehicles the most according to claim 4, it is characterised in that: described horn (4) has 4, and described column (19) has 8.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620290103.0U CN205633049U (en) | 2016-04-08 | 2016-04-08 | Collapsible many rotor unmanned aerial vehicle of horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620290103.0U CN205633049U (en) | 2016-04-08 | 2016-04-08 | Collapsible many rotor unmanned aerial vehicle of horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205633049U true CN205633049U (en) | 2016-10-12 |
Family
ID=57067716
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620290103.0U Expired - Fee Related CN205633049U (en) | 2016-04-08 | 2016-04-08 | Collapsible many rotor unmanned aerial vehicle of horn |
Country Status (1)
| Country | Link |
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| CN (1) | CN205633049U (en) |
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857604A (en) * | 2016-04-08 | 2016-08-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor unmanned aerial vehicle with foldable vehicle arms |
| WO2018157833A1 (en) * | 2017-03-02 | 2018-09-07 | 亿航智能设备（广州）有限公司 | Novel unmanned aerial vehicle |
| CN108528707A (en) * | 2017-03-02 | 2018-09-14 | 洛克希德·马丁公司 | Transfer coaxial helicopter linkage |
| CN108545190A (en) * | 2018-06-15 | 2018-09-18 | 芜湖万户航空航天科技有限公司 | Miniature drone |
| CN108609169A (en) * | 2018-06-15 | 2018-10-02 | 芜湖万户航空航天科技有限公司 | The unmanned plane of folding can be stablized |
| CN108773480A (en) * | 2018-06-15 | 2018-11-09 | 芜湖万户航空航天科技有限公司 | Unmanned plane |
| CN108791854A (en) * | 2018-06-15 | 2018-11-13 | 芜湖万户航空航天科技有限公司 | Fold unmanned plane |
| CN108860586A (en) * | 2018-06-15 | 2018-11-23 | 芜湖万户航空航天科技有限公司 | Novel unmanned plane |
| WO2019029387A1 (en) * | 2017-08-10 | 2019-02-14 | 深圳市道通智能航空技术有限公司 | Aerial vehicle and arm assembly and frame thereof |
| CN109573037A (en) * | 2019-01-24 | 2019-04-05 | 吉林大学 | A kind of power-line patrolling unmanned plane and patrolling method based on VR and multisensor |
| CN110606190A (en) * | 2019-09-24 | 2019-12-24 | 复旦大学 | Four rotor unmanned aerial vehicle of collapsible arm |
| CN111942568A (en) * | 2020-08-25 | 2020-11-17 | 浙江点辰航空科技有限公司 | Turning device for unmanned aerial vehicle |
| RU2790211C1 (en) * | 2022-09-24 | 2023-02-15 | Ооо "Финко" | Folding multicopter |
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2016
- 2016-04-08 CN CN201620290103.0U patent/CN205633049U/en not_active Expired - Fee Related
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105857604A (en) * | 2016-04-08 | 2016-08-17 | 四川克瑞斯航空科技有限公司 | Multi-rotor unmanned aerial vehicle with foldable vehicle arms |
| WO2018157833A1 (en) * | 2017-03-02 | 2018-09-07 | 亿航智能设备（广州）有限公司 | Novel unmanned aerial vehicle |
| CN108528707A (en) * | 2017-03-02 | 2018-09-14 | 洛克希德·马丁公司 | Transfer coaxial helicopter linkage |
| WO2019029387A1 (en) * | 2017-08-10 | 2019-02-14 | 深圳市道通智能航空技术有限公司 | Aerial vehicle and arm assembly and frame thereof |
| CN108791854A (en) * | 2018-06-15 | 2018-11-13 | 芜湖万户航空航天科技有限公司 | Fold unmanned plane |
| CN108773480A (en) * | 2018-06-15 | 2018-11-09 | 芜湖万户航空航天科技有限公司 | Unmanned plane |
| CN108609169A (en) * | 2018-06-15 | 2018-10-02 | 芜湖万户航空航天科技有限公司 | The unmanned plane of folding can be stablized |
| CN108860586A (en) * | 2018-06-15 | 2018-11-23 | 芜湖万户航空航天科技有限公司 | Novel unmanned plane |
| CN108545190A (en) * | 2018-06-15 | 2018-09-18 | 芜湖万户航空航天科技有限公司 | Miniature drone |
| CN109573037A (en) * | 2019-01-24 | 2019-04-05 | 吉林大学 | A kind of power-line patrolling unmanned plane and patrolling method based on VR and multisensor |
| CN110606190A (en) * | 2019-09-24 | 2019-12-24 | 复旦大学 | Four rotor unmanned aerial vehicle of collapsible arm |
| CN111942568A (en) * | 2020-08-25 | 2020-11-17 | 浙江点辰航空科技有限公司 | Turning device for unmanned aerial vehicle |
| CN111942568B (en) * | 2020-08-25 | 2023-12-22 | 国网福建省电力有限公司三明市沙县区供电公司 | Unmanned aerial vehicle is with turning device |
| RU2790211C1 (en) * | 2022-09-24 | 2023-02-15 | Ооо "Финко" | Folding multicopter |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161012 Termination date: 20190408 |