Tilting mechanism of rotor craft

Abstract

The invention relates to a tilting mechanism of a rotor craft. The tilting mechanism comprises a body, a first motor and a rotor. The rotor is connected with the first motor, and the first motor is arranged on the body. The body comprises an upper bottom plate, a lower bottom plate, a supporting rod and a telescopic part. The supporting rod is arranged between the upper bottom plate and the lower bottom plate and used for connecting the upper bottom plate with the lower bottom plate in a supporting mode. The telescopic part can change the distance between the upper bottom plate and the lower bottom plate, then the tilting direction of the craft can be changed, and the tilting mechanism can control the lift direction of the craft with small tilting force.

Description

technical field [0001] The present disclosure relates to the field of aircraft, in particular to coaxial twin propellers and tiltable aircraft. Background technique [0002] The traditional single-blade aircraft uses the rotation of the rotor to generate upward lift. Its biggest feature is that it has a rotor and a tail rotor to balance the torque. The array environment is very complicated. And the take-off weight of existing common single propeller aircraft is limited, if want to increase take-off weight, will increase rotor length, increase engine speed, these have all increased the mechanical complexity and the weight of rotor system. [0003] Most of the existing tiltable aircraft adopt the tilt rotor structure, which requires a large tilting force to achieve tilting. Contents of the invention [0004] In view of the above problems, the present disclosure provides a tilting mechanism of an aircraft with a simple structure and light weight, and the tilting mechanism ca...

AI Technical Summary

Problems solved by technology

[0002] The traditional single-blade aircraft uses the rotation of the rotor to generate upward lift. Its biggest feature is that it has a rotor and a tail rotor to balance the torque. The array environment is very complicated.

Moreover, the take-off weight of the existing common single-propeller aircraft is limited. If the take-off weight is to be increased, the length of the rotor and the speed of the engine must be increased, which all increase the mechanical complexity and weight of the rotor system.

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