Unmanned aerial vehicle frame structure
A machine frame and column technology, applied in the field of drone frame structure, can solve the problems of increased damage to drones and cameras, high impact force, etc., and achieve the effect of prolonging the service life and reducing the possibility of damage
Inactive Publication Date: 2017-11-24
广州市妙伊莲科技有限公司
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Problems solved by technology
[0004] Aiming at the deficiencies in the prior art, the purpose of the present invention is to provide a UAV frame structure to solve the problem that the existing UAV frame structure has a large impact force when the UAV lands, and the increase of UAV and camera The question of the possibility of damage
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[0018] 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.
[0019] see Figure 1-Figure 2 , the present invention provides a technical solution: an unmanned aerial vehicle frame structure, which structure includes a cross bar 1, a column 2, a ground contact bar 3, a rail bar 4, a support bar 5, a connecting plate 6, a camera mounting hole 7, Damping plate 8, bracket 9, the upper and lower end faces of the bracket 9 are parallel to each other, the inner cavity of the bracket 9 is connected to each other, the cross section of the bracket 9 is rectangular, and the upper end surface of the bracket 9 is provided with a cross bar 1, so The horizontal bar 1 and the column 2 are movably connected in an interference fit mode, the column 2 and the ground contact rod 3 are interference fit, the column 2 is connected ...
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The invention discloses an unmanned aerial vehicle frame structure. The unmanned aerial vehicle frame structure comprises transverse rods, stand columns, a grounding rod, a guide rail rod, a supporting rod, a connecting plate, a camera mounting hole, a vibration damping plate and supports, the upper and lower end surfaces of the supports are mutually parallel to each other, every support is an inner chamber interpenetration structure, the cross section of every support is rectangular, the upper end surface of every support is provided with one of the transverse rods, the transverse rods are movably connected with the stand columns in an interference fit manner, the stand columns are in interference fit with the grounding rod, the stand columns are connected with the supporting rod, the contact surfaces of the stand columns and the supporting rod have rectangular shapes having the same diameter, the lower end surface of the supporting rod is provided with the guide rail rod, and the guide rail rod is in transition fit with the connecting plate. The vibration damping plate is arranged, the vibration damping plate is arranged on the lower end surface of the connecting plate, the vibration damping plate and the grounding rod are positioned on the same horizontal plane, the impact fore during landing of an unmanned aerial vehicle is reduced through the elastic damping of damping balls, so the damage possibility of the unmanned aerial vehicle and the camera is reduced, and the service life of the unmanned aerial vehicle frame structure is prolonged.
Description
technical field [0001] The invention relates to an unmanned aerial vehicle frame structure, which belongs to the technical field of unmanned aerial vehicles. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with a parach...
Claims
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IPC IPC(8): B64C25/64B64D47/08
CPCB64C25/64B64D47/08
Inventor 广小芳
Owner 广州市妙伊莲科技有限公司