A buoy for water drones with weak interference
A technology of interference force and unmanned aerial vehicle, applied in the direction of floats, aircraft parts, convertible landing gear, etc., can solve the problems of small payload, inconvenient recovery, crash, etc., to avoid water pressure breakthrough and reduce draft depth , the effect of reducing resistance
Active Publication Date: 2022-04-05
湖南浩天翼航空技术有限公司
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Problems solved by technology
[0002] At present, UAV technology is developing rapidly and has been widely used in many fields such as military and civil affairs. Existing UAVs generally use landing gear recovery and net recovery. If a suitable landing environment cannot be found, the UAV will crash when its energy is exhausted. Therefore, traditional UAVs face problems such as being unable to take off and land on the water surface, and inconvenient to recover when sailing at sea. At the same time, they also have the weight of the body. Disadvantages such as large size and small payload
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[0023] In order to make the technical means, creative features, goals and effects achieved by the present invention easy to understand, the present invention will be further described below in conjunction with specific embodiments.
[0024] In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "another end" The orientation or positional relationship indicated by etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the referred device or element must have a specific orientation, use a specific Azimuth configuration and operation, therefore, should not be construed as limiting the invention. In addition, the terms "first" and "second" are used for descriptive purposes only, and should not be understood ...
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The invention discloses a buoy for a water unmanned aerial vehicle with weak interference, which includes a frame, high-mounted engines are fixedly fixed on the top of the left and right sides of the frame, and a ship-shaped bilge is fixedly installed in the middle of the bottom of the frame. The middle of the left and right sides of the ship-shaped bilge is symmetrically equipped with buoys, and the left and right sides of the bottom of the two buoys are symmetrically fixed and connected with fixed columns. A connecting mechanism is provided, and the bottoms of the two support sleeves are symmetrically provided with arc-shaped sliding plates. A buoy for a water unmanned aerial vehicle with weak interference force described in the present invention, the design of the buoys on both sides of the frame can increase the buoyancy in the water of the unmanned aerial vehicle and reduce the draft of the unmanned aerial vehicle; at the same time, the two buoys are separated left and right , its buoyancy in water can provide a stabilizing moment in the rolling direction, offsetting the instability in the rolling direction caused by the upward movement of the center of gravity of the fuselage due to the high position of the engine and wings.
Description
technical field [0001] The invention relates to the field of water drones, in particular to a buoy for water drones with weak interference. Background technique [0002] At present, UAV technology is developing rapidly and has been widely used in many fields such as military and civil affairs. Existing UAVs generally use landing gear recovery and net recovery. If a suitable landing environment cannot be found, the UAV will crash when its energy is exhausted. Therefore, traditional UAVs face problems such as being unable to take off and land on the water surface, and inconvenient to recover when sailing at sea. At the same time, they also have the weight of the body. Large, small payload and other disadvantages. Contents of the invention [0003] The main purpose of the present invention is to provide a buoy for a water unmanned aerial vehicle with weak interference, which can effectively solve the problems in the background technology. [0004] In order to achieve the ab...
Claims
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IPC IPC(8): B64C25/54B64C25/66B64C25/62
CPCB64C25/54B64C25/66B64C25/62
Inventor 刘彦海
Owner 湖南浩天翼航空技术有限公司