Power balance mechanism for unmanned aerial vehicle
A technology of power balance and unmanned aerial vehicles, which is applied to aircraft parts, aircraft control, aircraft stability, etc., can solve the problems of falling, equipment weight difference, poor shooting effect, etc., and achieve the effect of wide range, easy operation, and convenient adjustment
Inactive Publication Date: 2018-07-17
CHENGDU RAINPOO TECH CO LTD
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Problems solved by technology
However, due to the different application fields of electric drones, the weight of the equipment carried by them will vary greatly
For example, installing a digital camera or a professional video camera at the nose position will affect the center of gravity of the single-rotor electric UAV, thereby affecting the balance of the electric UAV during flight.
If it is light, the shooting effect will not be good, and if it is serious, it will affect the normal flight of the UAV and cause it to fall
Method used
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[0013] In order to have a clearer understanding of the technical features, purposes and effects of the present invention, the specific implementation manners of the present invention will now be described with reference to the accompanying drawings.
[0014] Such as figure 1 As shown, a power balance mechanism for an unmanned aerial vehicle, the unmanned aerial vehicle includes a fuselage 1 and an empennage fixed to the rear end of the fuselage 1 through a connector 2, the front end of the fuselage 1 is connected with a carrying device 3, and the The rear end of the fuselage 1 is fixedly connected with a connecting part 4, and one end of the connecting part 2 is fixedly connected with the empennage. distribution of positioning holes, the connecting piece 2 is placed in the cavity inside the connecting part 4, and the connecting piece 2 and the connecting part 4 are fixed through the positioning hole through the fastener. The dynamic balance mechanism also includes a balance d...
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The invention discloses a power balance mechanism for an unmanned aerial vehicle. The unmanned aerial vehicle comprises an unmanned aerial vehicle body and an empennage fixed at the rear end of the unmanned aerial vehicle body through a connector, loading equipment is connected to the front end of the unmanned aerial vehicle body, a connecting part is fixedly connected to the rear end of the unmanned aerial vehicle body, one end of the connector is fixedly connected with the empennage, the connecting part and the connector are cylindrical pieces, and the surfaces of the connecting part and theconnector are provided with positioning holes evenly distributed; the power balance mechanism for the unmanned aerial vehicle further includes a balance device, the balance device includes a fixing plate, an electromagnetic control mechanism and a balancing weight, the lower portion of the unmanned aerial vehicle body is provided with a groove, the fixing plate is rotatably mounted in the groove,the lower surface of the fixing plate is fixedly connected with an electromagnetic linear driving device, the electromagnetic linear driving device comprises a control rod, and the control rod is inthreaded connection with the balancing weight. The power balance mechanism is simple in structure, and the normal flight of the unmanned aerial vehicle is ensured.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicle balance adjustment, in particular to a power balance mechanism for an unmanned aerial vehicle. Background technique [0002] When the single-rotor electric UAV is not equipped with other equipment, its center of gravity is located on the central axis of the fuselage, so as to achieve the balance of the electric UAV during flight. However, due to the different application fields of electric drones, the weight of the equipment carried by them will vary greatly. For example, installing a digital camera or a professional video camera at the nose position will affect the center of gravity of the single-rotor electric UAV, thereby affecting the balance of the electric UAV during flight. If it is light, the shooting effect will not be good, and if it is serious, it will affect the normal flight of the UAV and cause it to fall. Contents of the invention [0003] In order to solve the a...
Claims
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IPC IPC(8): B64C17/02B64C5/10
CPCB64C17/02B64C5/10
Inventor 杨润朱鸿颖涛何世雄李小龙
Owner CHENGDU RAINPOO TECH CO LTD