Structure of controlling flying posture of aircraft

Abstract

The invention relates to a flying vehicle with a structure capable of controlling and regulating its flying form simply, quickly and flexibly. Its technical scheme is as follows; it has an exhaust piping which is connected with main exhaust piping and uses the main exhaust piping as shaft to control leftward and rightward turnover of flying vehicle, an exhaust piping for controlling leftward and rightward steering of flying vehicle and an exhaust pipe for controlling upward and downward flight of the flying vehicle. Said invention is easy to control and flexible, so that it can be extensively used in the fields of civil aviation, military affairs, flight model and toy, etc.

Description

Technical field: [0001] The invention relates to the technical fields of aerospace, aviation, flight models and toys, in particular to an aircraft that can adjust the flight attitude simply, quickly and sensitively. Background technique: [0002] For aviation, aerospace, flight models, toys and other equipment, the control of its flight attitude has always been a problem for designers; at present, most of the above-mentioned equipment, the control of its flight attitude is generally realized by changing its own shape; Such as the aircraft widely used commercially at present, when needing to change the flight attitude, it is realized by adjusting the position state of the horizontal wing, the horizontal tail, and the vertical tail relative to the aircraft body; The structural requirements are relatively high, the structure is relatively complex, and the cost is high; and the sensitivity of the control is also low, and it is impossible to achieve fast and sensitive control...

AI Technical Summary

Problems solved by technology

[0002] For aviation, aerospace, flight models, toys and other equipment, the control of its flight attitude has always been a problem for designers; at present, most of the above-mentioned equipment, the control of its flight attitude is generally realized by changing its own shape; Such as the aircraft widely used commercially at present, when needing to change the flight attitude, it is realized by adjusting the position state of the horizontal wing, the horizontal tail, and the vertical tail relative to the aircraft body; The structural requirements are high, the structure is more complicated, and the cost is high; and the sensitivity of the control is also low, and it is impossible to achieve fast and sensitive control

Images