CN205076042U - Many rotor unmanned aerial vehicle box structure horn - Google Patents
Many rotor unmanned aerial vehicle box structure horn Download PDFInfo
- Publication number
- CN205076042U CN205076042U CN201520778027.3U CN201520778027U CN205076042U CN 205076042 U CN205076042 U CN 205076042U CN 201520778027 U CN201520778027 U CN 201520778027U CN 205076042 U CN205076042 U CN 205076042U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- many rotor
- horn
- arm body
- aerial vehicle
- 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
Links
Abstract
The utility model relates to a many rotor unmanned aerial vehicle's horn specifically is a many rotor unmanned aerial vehicle box structure horn. The utility model provides a current many rotor unmanned aerial vehicle's the problem that the horn bearing capacity is less, connection structure is more complicated, manufacturing cost is higher, anti -torque performance is relatively poor. Many rotor unmanned aerial vehicle box structure horn is including centre plate, the rectangle tubulose arm body, wherein, it is individual that rectangle tubulose arm figure physically is 2N, and N is the positive integer, each rectangle tubulose arm body is radial equidistance to be arranged, and the tail end of each rectangle tubulose arm body passes through, and the centre plate is fixed is in the same place, the motor is all installed to the head end of each rectangle tubulose arm body, all be connected with the screw on each motor. The utility model is suitable for a many rotor unmanned aerial vehicle.
Description
Technical field
The utility model relates to the horn of many rotor wing unmanned aerial vehicles, specifically a kind of many rotor wing unmanned aerial vehicles box-structure horn.
Background technology
Many rotor wing unmanned aerial vehicles are excellent with its flight controlling, can in the hovering of any spatial point, landing without the need to features such as place supports, be widely used in taking photo by plane by every profession and trade, plant protection, the various fields such as monitoring.As the horn of many rotor wing unmanned aerial vehicles support system, its performance is directly connected to the overall performance of many rotor wing unmanned aerial vehicles.The horn of existing many rotor wing unmanned aerial vehicles all adopts round tube shape structure, cause the following problem of its ubiquity: one, the horn bearing capacity of existing many rotor wing unmanned aerial vehicles is less, causes the complete machine load-carrying ability of many rotor wing unmanned aerial vehicles limited, causes the field of application of many rotor wing unmanned aerial vehicles limited thus.Its two, the connection structure more complicated (needing to use intermetallic composite coating attaching parts respectively at horn two ends) between the horn of existing many rotor wing unmanned aerial vehicles and center plate and electrical motor, causes that the part of many rotor wing unmanned aerial vehicles is more, productive costs is higher.Its three, in order to reduce the complete machine weight of many rotor wing unmanned aerial vehicles, the horn of existing many rotor wing unmanned aerial vehicles adopts thin wall type carbon fiber pipe to make mostly, causes its manufacturing cost higher, causes the productive costs of many rotor wing unmanned aerial vehicles higher thus.They are four years old, the torsional property of the horn of existing many rotor wing unmanned aerial vehicles is poor, when causing many rotor wing unmanned aerial vehicles to run into IFR conditions (as strong wind) in flight course, can mild distortion be there is in horn, cause many rotor wing unmanned aerial vehicles to be shaken thus, thus affect the flight stability of many rotor wing unmanned aerial vehicles.Based on this, be necessary the horn inventing a kind of many rotor wing unmanned aerial vehicles completely newly, the problems referred to above existed with the horn solving existing many rotor wing unmanned aerial vehicles.
Summary of the invention
The utility model, in order to the problem that the horn bearing capacity solving existing many rotor wing unmanned aerial vehicles is less, connection structure is more complicated, manufacturing cost is higher, torsional property is poor, provides a kind of many rotor wing unmanned aerial vehicles box-structure horn.
The utility model adopts following technical scheme to realize: many rotor wing unmanned aerial vehicles box-structure horn, comprises center plate, rectangular tubular arm body; Wherein, the number of described rectangular tubular arm body is 2N, and N is positive integer; Each rectangular tubular arm body radially equidistant arrangement, and the tail end of each rectangular tubular arm body is fixed together by center plate; The head end of each rectangular tubular arm body is all provided with electrical motor; Each electrical motor is all connected with screw propeller.
During use, at the upper surface of center plate, battery pack and control setup are installed, form electronic machine storehouse at the lower surface carry application apparatus of center plate, many rotor wing unmanned aerial vehicles can be formed, as shown in Figure 4.When transporting many rotor wing unmanned aerial vehicles, each screw propeller can be removed, thus convenient transport.Before many rotor wing unmanned aerial vehicles take off, each screw propeller is in place, ensures that many rotor wing unmanned aerial vehicles normally take off thus.
Based on said process, compared with the horn of existing many rotor wing unmanned aerial vehicles, many rotor wing unmanned aerial vehicles box-structure horn described in the utility model possesses following advantage: one, many rotor wing unmanned aerial vehicles box-structure horn described in the utility model is by utilizing the mechanical characteristic of square-section, effectively improve self stress performance and structural strength, increase effectively self bearing capacity thus, thus effectively enhance the complete machine load-carrying ability of many rotor wing unmanned aerial vehicles, and then effectively expand the field of application of many rotor wing unmanned aerial vehicles.They are two years old, many rotor wing unmanned aerial vehicles box-structure horn described in the utility model is by adopting rectangular tubular structure, effectively simplify self with between center plate and electrical motor connection structure (with can realize face between center plate and electrical motor and contact, and without the need to processing attaching parts at horn two ends), effectively reduce the part of many rotor wing unmanned aerial vehicles thus, effectively reduce the productive costs of many rotor wing unmanned aerial vehicles.Its three, many rotor wing unmanned aerial vehicles box-structure horn described in the utility model adopts aluminum alloy or carbon fiber to make, and effectively reduces self manufacturing cost thus, thus effectively reduces the productive costs of many rotor wing unmanned aerial vehicles.They are four years old, many rotor wing unmanned aerial vehicles box-structure horn described in the utility model is by utilizing the mechanical characteristic of square-section, effectively enhance self torsional property, effectively prevent thus when self running into IFR conditions (as strong wind) and mild distortion occurs, thus effectively prevent many rotor wing unmanned aerial vehicles and shake, and then effectively ensure that the flight stability of many rotor wing unmanned aerial vehicles.
The utility model structure is simple, reasonable in design, efficiently solves the problem that horn bearing capacity is less, connection structure is more complicated, manufacturing cost is higher, torsional property is poor of existing many rotor wing unmanned aerial vehicles, is applicable to many rotor wing unmanned aerial vehicles.
Accompanying drawing explanation
Fig. 1 is the first structural representation of the present utility model.
Fig. 2 is the second structural representation of the present utility model.
Fig. 3 is the third structural representation of the present utility model.
Fig. 4 is using state reference diagram of the present utility model.
Fig. 5 is the section structure schematic diagram of rectangular tubular arm body of the present utility model.
In figure: 1-center plate, 2-rectangular tubular arm body, 3-electrical motor, 4-screw propeller, 5-battery pack, 6-electronic machine storehouse.
Detailed description of the invention
Many rotor wing unmanned aerial vehicles box-structure horn, comprises center plate 1, rectangular tubular arm body 2; Wherein, the number of described rectangular tubular arm body 2 is 2N, and N is positive integer; Each rectangular tubular arm body 2 radially equidistant arrangement, and the tail end of each rectangular tubular arm body 2 is fixed together by center plate 1; The head end of each rectangular tubular arm body 2 is all provided with electrical motor 3; Each electrical motor 3 is all connected with screw propeller 4.
Each rectangular tubular arm body 2 all adopts aluminum alloy or carbon fiber to make.
During concrete enforcement, the number of rectangular tubular arm body 2 is four (as shown in Figure 1) or six (as shown in Figure 2) or eight (as shown in Figure 3).
Claims (1)
1. the box-structure of rotor wing unmanned aerial vehicle a more than horn, is characterized in that: comprise center plate (1), rectangular tubular arm body (2); Wherein, the number of described rectangular tubular arm body (2) is 2N, and N is positive integer; Each rectangular tubular arm body (2) radially equidistant arrangement, and the tail end of each rectangular tubular arm body (2) is fixed together by center plate (1); The head end of each rectangular tubular arm body (2) is all provided with electrical motor (3); Each electrical motor (3) is all connected with screw propeller (4); Each rectangular tubular arm body (2) all adopts aluminum alloy or carbon fiber to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520778027.3U CN205076042U (en) | 2015-10-09 | 2015-10-09 | Many rotor unmanned aerial vehicle box structure horn |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520778027.3U CN205076042U (en) | 2015-10-09 | 2015-10-09 | Many rotor unmanned aerial vehicle box structure horn |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205076042U true CN205076042U (en) | 2016-03-09 |
Family
ID=55428465
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520778027.3U Expired - Fee Related CN205076042U (en) | 2015-10-09 | 2015-10-09 | Many rotor unmanned aerial vehicle box structure horn |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205076042U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275404A (en) * | 2016-08-31 | 2017-01-04 | 深圳市莲花百川科技有限公司 | The double cross arm structure of many rotor wing unmanned aerial vehicles |
-
2015
- 2015-10-09 CN CN201520778027.3U patent/CN205076042U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275404A (en) * | 2016-08-31 | 2017-01-04 | 深圳市莲花百川科技有限公司 | The double cross arm structure of many rotor wing unmanned aerial vehicles |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN204173154U (en) | A kind of modularized combination type unmanned plane | |
| CN104443431A (en) | Triangular satellite configuration and system and assembly method | |
| CA2893338A1 (en) | Fuselage structure of an unmanned helicopter | |
| CN203612209U (en) | Agricultural aircraft | |
| CN105438460A (en) | Dual-power synergistically driven unmanned aerial vehicle | |
| CN202609078U (en) | Tail control system for unmanned helicopter | |
| CN104276276A (en) | Modularized handling unmanned aerial vehicle layout | |
| CN107891973A (en) | A kind of unmanned plane support foot rest | |
| CN203593161U (en) | Variable multi-rotor UAV (unmanned aerial vehicle) | |
| CN205076042U (en) | Many rotor unmanned aerial vehicle box structure horn | |
| CN106081059A (en) | A kind of many rotor wing unmanned aerial vehicles | |
| CN106741907A (en) | A kind of multi-rotor aerocraft | |
| CN204916169U (en) | Many rotor unmanned aerial vehicle | |
| CN204895850U (en) | Six rotor crafts | |
| CN204481527U (en) | The stake of rotor wing unmanned aerial vehicle recharging | |
| CN206218217U (en) | A kind of eight rotor electric power unwrapping wire unmanned planes | |
| CN205499341U (en) | Undercarriage for unmanned aerial vehicle | |
| CN205087140U (en) | Oil moves six coaxial rotor unmanned aerial vehicle frame systems of displacement | |
| CN206374990U (en) | A kind of new unmanned plane motor cabinet | |
| CN204737029U (en) | Unmanned plant protection aircraft of many screws | |
| CN208102333U (en) | The double-deck rotor wings frame in a kind of unmanned plane | |
| CN204688414U (en) | Horn assembly, frame and unmanned plane | |
| CN204998757U (en) | Undercarriage that topples is prevented to many rotor crafts | |
| CN203593162U (en) | Aircraft with eight coaxial rotary wings | |
| CN210882601U (en) | Surveying and mapping unmanned aerial vehicle with foldable rotor wings |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 030603, Shanxi Jinzhong District, Yuci Yingbin West Street and Tian commercial building 5 Patentee after: Shanxi Shipule General Aviation Technology Co. Ltd. Address before: 030603, Shanxi Jinzhong District, Yuci Yingbin West Street and Tian commercial building 5 Patentee before: SHANXI SHIPULE AVIATION PLANT PROTECTION TECHNOLOGY CO., LTD. |
|
| 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: 20160309 Termination date: 20171009 |