A wing fixing structure of an unmanned aerial vehicle
A fixed structure, unmanned aerial vehicle technology, applied in the direction of unmanned aerial vehicle, fuselage, rotorcraft, etc., can solve the problems of inconvenient carrying, low strength, difficult disassembly and assembly, etc.
Inactive Publication Date: 2018-12-11
梁小燕
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AI Technical Summary
Problems solved by technology
It is generally believed that the larger the number of propellers, the smoother the flight and the easier the operation. The wings of traditional drones are fixed with carbon fiber plates, which is difficult to disassemble and assemble, and has low strength. Detachable drone wings Tools such as screwdrivers are required for disassembly and assembly. When working in the field, disassembly tools need to be carried, which can easily cause loss of tools and is inconvenient to carry
Method used
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Embodiment Construction
[0020] The present invention will be further described below in conjunction with the accompanying drawings.
[0021] Such as Figures 1 to 3 As shown, a kind of unmanned aerial vehicle wing fixing structure described in the present invention, it comprises unmanned aerial vehicle installation total box 1 and wing connecting rod 8; Described wing connecting rod 8 one ends are provided with propeller 9; The other end of the propeller 9 is provided with a circular mounting shaft 6; the general box 1 for the installation of the drone is provided with a support plate 101; the support plate 101 is fixed with a guide sleeve 7; The shaft of the wing connecting rod 8 matches; the installation sleeve 2 is fixed on the general installation box 1 of the drone; the circular installation shaft 6 passes through the guide sleeve 7 and is inserted into the installation sleeve 2; the wing The connecting rod 8 is inserted into the guide sleeve 7; after the wing connecting rod 8 is inserted into ...
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The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to a wing fixing structure of the unmanned aerial vehicle, wherein a support plate is arranged on a general box of the unmanned aerial vehicle. A guide sleeve is fixed on the support plate; The circular mounting shaft is inserted into the mounting sleeve after passing through the guide sleeve; The wingconnecting rod is inserted into the guide sleeve; One end of the sliding sleeve is inserted into the outer side wall of the inner mounting sleeve of the mounting sleeve and is provided with an annular mounting groove; The bottom of the ball mounting hole is provided with a hemispherical slot hole; The bottom end of the hemispherical slot hole is provided with a circular through hole; The diameterof the ball is equal to the diameter of the hemispherical slot; The diameter of the circular through hole is less than the diameter of the ball; A rubber ring is sleeved in the annular mounting groove; The inner torus of the rubber ring is pressed against the surface of the ball; One end of the ball passes through the circular through-hole and is inserted into the annular groove. When the invention is used, the connecting structure does not need to use additional tools, the disassembly and assembly are more convenient, and the disassembly and assembly steps of the unmanned aerial vehicle wingare simple and the disassembly and assembly efficiency is high.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicle equipment, in particular to an unmanned aerial vehicle wing fixing structure. Background technique [0002] UAV is an unmanned aircraft operated by radio remote control equipment and self-contained program control device. UAVs are actually a general term for unmanned aerial vehicles. From a technical point of view, they can be divided into: unmanned helicopters, unmanned fixed-wing aircraft, unmanned multi-rotor aircraft, unmanned airships, and unmanned parawing aircraft. . Compared with manned aircraft, it has the advantages of small size, low cost, convenient use, low environmental requirements, and strong survivability. Aerial UAV is a remote control aircraft integrated with high-definition photography and camera devices. The system mainly includes: carrier aircraft, flight control, gyro pan, video transmission, ground station and communication system, etc. The flying height...
Claims
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Patent Timeline
Login to View More IPC IPC(8): B64C27/08B64C1/26
CPCB64C1/26B64C27/08B64U30/20B64U10/10
Inventor 梁小燕
Owner 梁小燕