Structure of controlling flying posture of aircraft

A technology of flight attitude and aircraft, applied in the field of aircraft, can solve the problems that the control of flight attitude bothers designers, cannot realize fast and sensitive control, and has high requirements for aircraft structure and structure, and achieves simple control, sensitive response, and simple operation Effect

Inactive Publication Date: 2003-03-26
金洪奎
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  • Abstract
  • Description
  • Claims
  • Application Information

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

Method used

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  • Structure of controlling flying posture of aircraft
  • Structure of controlling flying posture of aircraft
  • Structure of controlling flying posture of aircraft

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Embodiment Construction

[0027] See attached figure 1 ∽9, the front end of the body 01 of the aircraft of the present invention is provided with an air inlet 1, and the engine 2 is connected between the air inlet 1 and the main exhaust pipe 3; the straight main exhaust pipe 3 runs along the center of the body 01 Setting; in the horizontal direction, both sides of the main exhaust duct 3 are symmetrically connected with the exhaust duct 5 that controls the aircraft to turn left and right with the main exhaust duct 3. Exhaust pipe 3 is vertically distributed; its exhaust port 51 outlet direction is downward (also can be upward); a control valve is arranged at the connection; when the control valve on the left side is opened, the exhaust pipe 5 on the left side Exhaust downward, so that the left side of the aircraft is raised relative to the right side, otherwise the right side is raised relative to the left side; Therefore, the attitude of the aircraft can be changed extremely sensitively and quickly. ...

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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...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C15/02
Inventor 金洪奎
Owner 金洪奎
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