Small unmanned aerial vehicle openable-closeable cabin door load lifting mechanism

A technology of small unmanned aerial vehicle and lifting mechanism, which is applied in the direction of aircraft door, power control mechanism, wing fan control mechanism, etc., to achieve the effect of small footprint, guaranteed aerodynamic performance, and improved overall performance

Active Publication Date: 2016-10-12
HIWING AVIATION GENERAL EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

But at present, there is no openable and closable cabin door load lifting mechanism invented for the above-mentioned difficult problems in the industry.

Method used

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  • Small unmanned aerial vehicle openable-closeable cabin door load lifting mechanism
  • Small unmanned aerial vehicle openable-closeable cabin door load lifting mechanism
  • Small unmanned aerial vehicle openable-closeable cabin door load lifting mechanism

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Experimental program
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Effect test

Embodiment Construction

[0033] Embodiments of the present invention will be described below in conjunction with the accompanying drawings.

[0034] The small UAV can open and close the hatch load lifting mechanism, including a remote control system, a load 10 lifting system and a hatch 8 system. The remote control system includes autopilot and signal processing control system, such as figure 1 and figure 2 As shown, after an instruction is given to the autopilot by the ground station or the manual remote controller, the autopilot sends a PWM signal to the signal processing control system, and the signal processing control system controls the lifting platform of the load 10 and the opening and closing of the hatch 8 . Specifically, the first servo motor 7 is fixed on the mechanism through the first servo motor fixing plate 18, and the signal processing control system controls the first servo motor 7 to drive the ball screw 2 to drive the intermediate mounting plate 6 along the ball screw 2 and the c...

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Abstract

The invention discloses an openable-closeable cabin door unmanned aerial vehicle load lifting mechanism. Ascending and descending of a platform and vertical limiting of a pod mounting plate are realized through two ball screws, vertical movement of the platform and horizontal limiting of the pod mounting plate are realized through two carbon tubes. A motor drives the ball screws to run, a synchronous wheel ensures the ball screws to move synchronously, the ball screws drive a middle mounting plate to lift and lower a task load, a servo motor controls opening and closing of a cabin door through a signal processing system, a Hall sensor and a magnetic block control a lifting mechanism to stop moving, and a lock fastener and a lock block ensure stability of the platform after working and being recycled. The task load is connected with the middle mounting plate and can be replaced at any time. By using the mechanism, closing load of the cabin door is unaffected in the process of launching and recycling an unmanned aerial vehicle, and pneumatic performance of the unmanned aerial vehicle can be ensured. The load can be replaced and mounted at any time before the unmanned aerial vehicle takes off, the mechanism is convenient, quick, small in occupied space, light in weight and economically feasible, and overall performance, safety and reliability of the unmanned aerial vehicle are improved greatly.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle load task system, which is especially suitable for the load of micro-miniature unmanned aerial vehicles, which can carry out lifting operation on the task load and realize the opening and closing of the cabin door. Background technique [0002] At present, most of my country's UAVs are micro-miniature UAVs, which can carry small loads and narrow available space. The openings for ordinary loads often have a huge impact on aerodynamic performance. Therefore, it is urgent to design a load lifting mechanism that can install ordinary loads in a narrow load compartment, realize the opening and closing of the hatch to reduce the aerodynamic impact, and at the same time ensure the load weight requirements of the UAV. But, there is no openable and closable hatch door load lifting mechanism invented for the above-mentioned difficult problem in the industry at present. Contents of the invention [0003] The o...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/14B64D9/00E05F15/603
CPCB64C1/1415B64D9/00E05F15/603
Inventor 李迪董泽辉姜鹏飞高文坤罗怡巩春源刘铁军史峰关雅雯江杰
Owner HIWING AVIATION GENERAL EQUIP
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