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Pneumatic fixed-wing aircraft

An aircraft and aerodynamic technology, applied in aircraft control, aircraft parts, vertical take-off and landing aircraft, etc., can solve problems such as dangerous use, difficult manipulation, and complexity, and achieve low manufacturing and operating costs, good gliding ability, and fast speed Effect

Pending Publication Date: 2022-03-22
王登森 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Passive generation of lift is a natural defect of traditional fixed-wing aircraft, which has resulted in dangerous, difficult and complicated maneuvers during the use of traditional fixed-wing aircraft, especially during take-off and landing. The short run-up distance, the high take-off speed, the thrilling landing process, the frightening taxiing experience, the flustered and exhausted pilots, coupled with the tragic flight accidents that occur from time to time, warn us that we must fundamentally change this situation

Method used

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  • Pneumatic fixed-wing aircraft
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Embodiment Construction

[0042] In order to make the technical solution of the present invention clearer, the present invention will be described in detail below in conjunction with the accompanying drawings and embodiments. The embodiments here are only used to explain the present invention, not to limit the present invention.

[0043] The fixed-wing helicopter, its body, control system, mechanical structure, size and overall layout of the power plant are basically the same as the traditional fixed-wing aircraft, only the wings have been improved accordingly, and the "autonomous jet wing" technology ; used the mature large ducted turbofan aircraft engine and connecting pipe and docking device technology, this turbofan aircraft engine 11 or 12 is installed in the appropriate position inside the fuselage, and its air intake 1 passes through the pipeline and docking device 10 It communicates with the suction docking port 4 of the autonomous jet wing or its suction port 1 is directly used as the air inta...

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Abstract

The invention discloses a pneumatic fixed-wing aircraft, which is called a fixed-wing helicopter for short, and belongs to a basic invention of an aircraft structure. The mechanical structures, the sizes and the overall layout of the aircraft body, the control system and the power device are basically the same as those of a traditional fixed-wing aircraft. An autonomous jet wing and a mature large-duct turbofan engine technology are adopted, the autonomous jet wing and the mature large-duct turbofan engine technology are correspondingly communicated through a pipeline and a butt joint device, air is sucked in from an air inlet in the front end of the wing or the front end of a fuselage and sprayed out backwards at a high speed along the surface of the wing from an exhaust port in the upper portion of the front end of the wing, and the lift force and thrust of the aircraft are autonomously controlled. An abnormally complex and sensitive mechanical device of a traditional helicopter is abandoned, the difficulty and danger in the take-off and landing process of a traditional fixed-wing aircraft are overcome, and the aircraft is particularly suitable for being used in a wing-body-fused stealth aircraft. Even if an engine flames out, the helicopter can land in a gliding mode, and the helicopter is particularly safe to land in a gliding mode. The LED lamp is suitable for being used in various harsh environments and meets the requirement for multiple purposes.

Description

technical field [0001] The present invention relates to an aerodynamic fixed-wing aircraft (Pneumatic Fixed Wing Aircraft), hereinafter referred to as "Fixed Wing Helicopter (Fixed Wing Helicopter)", which belongs to the basic invention of aircraft structure. Background technique [0002] Traditional fixed-wing aircraft can passively generate enough lift to support the normal flight of the aircraft only when the wings are flowing at high speed relative to the air. Passive generation of lift is a natural defect of traditional fixed-wing aircraft, which has resulted in dangerous, difficult and complicated maneuvers during the use of traditional fixed-wing aircraft, especially during take-off and landing. The short run-up distance, the high take-off speed, the thrilling landing process, the frightening taxiing experience, the flustered and exhausted pilots, coupled with the tragic flight accidents that occur from time to time, warn us that we must fundamentally change this situ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C29/00B64C15/02
CPCB64C29/00B64C15/02
Inventor 王登森王佩楠
Owner 王登森
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