CN205633035U - Many rotor unmanned aerial vehicle's wing - Google Patents
Many rotor unmanned aerial vehicle's wing Download PDFInfo
- Publication number
- CN205633035U CN205633035U CN201620245511.4U CN201620245511U CN205633035U CN 205633035 U CN205633035 U CN 205633035U CN 201620245511 U CN201620245511 U CN 201620245511U CN 205633035 U CN205633035 U CN 205633035U
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- China
- Prior art keywords
- motor
- unmanned aerial
- wing
- ring
- many rotor
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- Expired - Fee Related
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Abstract
The utility model relates to a many rotor unmanned aerial vehicle's wing, including screw, motor and motor cabinet, the motor is installed on the motor cabinet, and the screw is installed on the motor, and motor and screw have two, the motor cabinet includes the frame body, and the frame body includes the ring of placing of roof, bottom plate and loop configuration, the roof with place the top surface of ring and be connected, the bottom plate with place the ring bottom surface and be connected, the side of placing the ring is equipped with pipy clamping part, is equipped with the motor mounting hole on roof and the bottom plate, two motors pass through the motor mounting hole and install respectively on roof and bottom plate. The utility model discloses an install two motors on the individual motor cabinet, two screws of two motor separately -driven have improved the stability of unmanned aerial vehicle flight, and two motors are installed respectively on the roof and bottom plate of motor cabinet moreover, and roof and gasket -mounted are on placing the ring, and the installation is very convenient with the dismantlement.
Description
Technical field
This utility model relates to field of mechanical technique, particularly relates to the wing of a kind of many rotor wing unmanned aerial vehicles.
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, and each horn is provided with a motor, and a motor drives a propeller, when one of them motor damage, all can affect the stability of this unmanned plane, cause the unmanned plane can not normal flight.
Utility model content
This utility model aims to provide the wing of a kind of many rotor wing unmanned aerial vehicles, even if one of them motor damage, unmanned plane remains able to normal flight.
For reaching above-mentioned purpose, the technical solution adopted in the utility model is as follows:
The wing of a kind of many rotor wing unmanned aerial vehicles, including propeller, motor and motor cabinet, described motor is arranged on motor cabinet, and described propeller is arranged on motor, and described motor and propeller have two, and two motors are respectively arranged on end face and the bottom surface of motor cabinet；Described motor cabinet includes machine base body, described machine base body 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, and described top board and base plate are provided with motor installing hole.
Further, described machine base body is rectangle, is respectively equipped with a screwed hole A at four drift angles of described top board and base plate, and described placement top surface of ring and bottom surface are provided with the screwed hole B adaptive with screwed hole A.
Further, the clamping part end face of described tubulose and bottom surface are respectively equipped with a groove, and groove runs through the outer face of clamping part, and the axis of clamping part and two grooves are positioned at same level；The outer end of described groove is provided with a pair lug, and two lugs are respectively arranged on the both sides of groove.
Further, described motor is mounted remotely from the side of clamping part.
Further, the material of described top board and base plate is carbon fibre.
Further, the material of described placement ring is aluminium alloy.
Further, the front and back of described placement ring is provided with groove.
Further, the blade of described propeller has two.
Compared with prior art, this utility model has the advantages that
The wing that this utility model provides, a motor cabinet is provided with two motors, and two motors drive two propellers respectively, improve the stability of unmanned plane during flying；And two motors are separately mounted on top board and the base plate of motor cabinet, 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 of motor cabinet；
Fig. 3 is the structural representation of motor；
In figure: 1-places ring, 2-clamping part, 3-motor installing hole, 4-top board, 5-base plate, 6-screwed hole A, 7-screwed hole B, 8-bar hole, 9-groove, 10-lug, 11-groove, 12-motor, 13-propeller, 14-axis hole, 15-louvre.
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.
Such as Fig. 1, the wing of many rotor wing unmanned aerial vehicles disclosed in this utility model, including propeller 13, motor 12 and motor cabinet, motor 12 is arranged on motor cabinet, propeller 13 is arranged on motor 12, motor 12 and propeller 13 have two, and two motors 12 are respectively arranged on the end face of motor cabinet and bottom surface is preferred, and the blade of propeller 13 has two.As it is shown on figure 3, motor is provided with louvre 15 and axis hole 14, axis hole 14 is located at motor center, and louvre 15 is distributed on axis hole 14 periphery.
As shown in Figure 2, motor cabinet includes machine base body, machine base body includes the placement ring 1 of top board 4, base plate 5 and loop configuration, top board 4 is connected with placement ring 1 end face of loop configuration, base plate 5 is connected with placement ring 1 bottom surface of loop configuration, the one side placing ring 1 is provided with the clamping part 2 of tubulose, and top board 4 and base plate 5 are provided with motor installing hole 3, and two motors 12 are separately mounted on top board 4 and base plate 5 by motor installing hole 3.Motor 12 is mounted remotely from the side of clamping part 2.
Top board 4 and base plate 5 with place ring 1 thread connection.Preferably, machine base body is rectangle, it is respectively equipped with a screwed hole A6 at four drift angles of top board 4 and base plate 5, place ring 1 end face and bottom surface is provided with the screwed hole B7 adaptive with screwed hole A6, during use, motor is arranged on top board 4 and base plate 5, top board 4 and base plate 5 being arranged on placement ring 1 with screw, installation and removal are quite convenient to.Further, clamping part 2 end face of tubulose and bottom surface are respectively equipped with a groove 9, and groove 9 runs through the outer face of clamping part 2, the axis of clamping part 2 and two grooves 9 and is positioned at same level；The outer end of groove 9 is provided with a pair lug 10, and two lugs 10 are respectively arranged on the both sides of groove 9.The front and back placing ring 1 is provided with groove 11, to alleviate the weight of motor cabinet.Top board 4 and base plate 5 are provided with bar hole 8, are used for dispelling the heat.The material of top board 4 and base plate 5 is carbon fibre, and the material placing ring 1 is aluminium alloy.
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 (8)
1. the wing of rotor wing unmanned aerial vehicle more than a kind, it is characterized in that: include propeller (13), motor (12) and motor cabinet, described motor (12) is arranged on motor cabinet, described propeller (13) is arranged on motor (12), and described motor (12) and propeller (13) have two；Described motor cabinet includes machine base body, described machine base body includes top board (4), the placement ring (1) of base plate (5) and loop configuration, described top board (4) is connected with placing ring (1) end face, described base plate (5) is connected with placing ring (1) bottom surface, the side of described placement ring (1) is provided with the clamping part (2) of tubulose, described top board (4) and base plate (5) are provided with motor installing hole (3), said two motor (12) is separately mounted on top board (4) and base plate (5) by motor installing hole (3).
The wing of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterized in that: described machine base body is rectangle, being respectively equipped with a screwed hole A (6) at four drift angles of described top board (4) and base plate (5), described placement ring (1) end face and bottom surface are provided with the screwed hole B (7) adaptive with screwed hole A (6).
The wing of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterized in that: clamping part (2) end face of described tubulose and bottom surface are respectively equipped with a groove (9), groove (9) runs through the outer face of clamping part (2), and axis and two grooves (9) of clamping part (2) are positioned at same level；The outer end of described groove (9) is provided with a pair lug (10), and two lugs (10) are respectively arranged on the both sides of groove (9).
4. according to the wing of the many rotor wing unmanned aerial vehicles described in claim 1 or 3, it is characterised in that: described motor (12) is mounted remotely from the side of clamping part (2).
The wing of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: the material of described top board (4) and base plate (5) is carbon fibre.
The wing of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: the material of described placement ring (1) is aluminium alloy.
The wing of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: the front and back of described placement ring (1) is provided with groove (11).
The wing of many rotor wing unmanned aerial vehicles the most according to claim 1, it is characterised in that: the blade of described propeller (13) has two.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620245511.4U CN205633035U (en) | 2016-03-25 | 2016-03-25 | Many rotor unmanned aerial vehicle's wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620245511.4U CN205633035U (en) | 2016-03-25 | 2016-03-25 | Many rotor unmanned aerial vehicle's wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205633035U true CN205633035U (en) | 2016-10-12 |
Family
ID=57075475
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620245511.4U Expired - Fee Related CN205633035U (en) | 2016-03-25 | 2016-03-25 | Many rotor unmanned aerial vehicle's wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205633035U (en) |
-
2016
- 2016-03-25 CN CN201620245511.4U patent/CN205633035U/en not_active Expired - Fee Related
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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: 20161012 Termination date: 20170325 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |