Active aircraft side rod improving aircraft control quality

Abstract

The invention discloses an active aircraft side rod improving aircraft control quality. The active aircraft side rod improving aircraft control quality comprises a main body and further comprises a mounting mechanism, a fixing mechanism and a protective mechanism, the front surface of the main body is fixedly connected with an operation rod bearing seat, the top of the operation rod bearing seat is fixedly connected with an operation rod protective top cover and an operation bearing rod, and the mounting mechanism is located at the joint of the operation rod bearing seat and the operation rodprotective top cover. A fixed tooth plate is designed and mounted at the joint of the operation rod bearing seat and the operation rod protective top cover, a reinforced tooth plate is designed and mounted on one side of the operation rod protective top cover, thus the operation rod bearing seat and the operation rod protective top cover are fixed, meanwhile a concave limiting groove is designed and mounted on the inner side of the operation rod bearing seat, waggling is avoided when the operation rod bearing seat and the operation rod protective top cover are connected, and the problem that the operation rod bearing seat and the operation rod protective top cover are not convenient to assemble is solved.

Description

technical field [0001] The invention belongs to the technical field of aircraft side sticks, and in particular relates to an active aircraft side stick which improves the handling quality of the aircraft. Background technique [0002] Active aircraft side stick refers to the control rod or disc used by the pilot to control the aircraft elevator and aileron. Deflect downward, and the aircraft lowers its head; pull the lever back, and the elevator deflects upward, raising the nose; push the stick or turntable to the right, the aileron goes up and down left, and the airplane turns right; push the stick or turntable to the left, the airplane turns left, the control stick and control The surface connections are mechanical, hydraulic and fly-by-wire. [0003] The existing active aircraft side sticks have many inner parts when in use, and the active aircraft side sticks are mostly assembled by bolts, which are extremely stable, but it is extremely inconvenient to disassemble and o...

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide an active aircraft sidestick that improves the quality of aircraft handling, to solve the problem that the active aircraft sidestick proposed in the above background technology has many inner parts during use, and the active aircraft sidestick is mostly through Assembled with bolts, the stability is extremely strong, but it is extremely inconvenient to disassemble and overhaul. At the same time, the general snap-in mechanism is poor in stability, cannot be generally implemented, has low practicability, and high cost of use.

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