Aircraft gravity center dynamic balancing device

Abstract

The invention proposes a dynamic balancing device for the center of gravity of an aircraft, which includes a battery, a movable seat, a slide rail and a lead screw. By moving the device with higher mass density in the original aircraft, the center of gravity of the trim due to the movement of the mechanism is changed. This device is simple to install and uses less materials, and the trim device is made of in-situ materials with less load and will not Increases excessive fuel consumption and power consumption, and solves the defect of the aircraft's center of gravity moving forward or backward.

Description

Technical field [0001] The invention belongs to the technical field of aviation aircraft, in particular to a dynamic trim device for the center of gravity of the aircraft. Background technique [0002] At present, the aviation field is emerging. With the aid of aircraft as a carrier, many modern equipment can work in extreme environments to help people complete tasks. Among the many load equipment, there is a class of sports equipment, such as robotic arms, extension rods, Rotating mechanisms, etc., will cause the entire aircraft's center of gravity to change during movement, and the normal flight of the aircraft will be disturbed by the change of center of gravity. This leads to the incoordination between such mechanisms and the aircraft body, which affects the normal flight of the aircraft and is difficult to be practical. [0003] The automatic trim is completed by the automatic trim system without the driver's participation. The automatic trim system includes an automatic rod ...

AI Technical Summary

Problems solved by technology

[0004] The above two trimming methods will increase fuel consumption or power consumption during operation, thereby reducing flight time. This is a great waste in the field of unm

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