Low-temperature invisible multi-nozzle aircraft

An aircraft and multi-nozzle technology, applied in the field of aircraft, can solve problems such as difficulty in stealth, achieve the effects of reducing heat radiation, good safety, and reducing high-temperature environmental pollution

Active Publication Date: 2020-08-11
中国北方工业有限公司 +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a low-temperature stealth multi-jet aircraft based on multiple directions and multiple jets, so as to avoid air crashes caused by failures of flaps, ailerons, elevators and rudders, while reducing heat radiation and solving existing problems. Various jet aircraft are difficult to stealth due to high temperature radiation

Method used

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Embodiment Construction

[0027] In order to make the purpose, content and advantages of the present invention clearer, the specific embodiments of the present invention will be described in further detail below with reference to the accompanying drawings and embodiments.

[0028] refer to Figure 1 to Figure 3 As shown, the low-temperature stealth multi-nozzle aircraft of this embodiment includes: the aircraft body 1, the power system 2, the control system 3, the bottom nozzle 4, the vertical nozzle 5, the horizontal nozzle 6, the pitch nozzle 7, the tail nozzle 8, the gas pipeline 9, the nozzle Valve 10 and cooling and boosting device 11.

[0029] The aircraft main body 1 described in this embodiment is the main body that carries all the system components of the aircraft, and is the main body that generates flight lift. The aircraft main body 1 of the present embodiment uses the aerodynamic shape of the American B2 stealth bomber as an aerodynamic model, and the present embodiment is demonstrated an...

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Abstract

The invention belongs to the field of aircrafts and discloses a low-temperature invisible multi-nozzle aircraft. The aircraft comprises an aircraft main body, a power system, a control system, a bottom nozzle, a vertical nozzle, a horizontal nozzle, a pitching nozzle, a tail nozzle, a gas pipeline, a nozzle valve and a cooling and pressurizing device; the cooling and pressurizing device is locatedin the middle of the aircraft body and used for sucking, compressing and cooling part of air entering an air inlet in the front end of the power system, storing the air and supplying the air to all the nozzles so as to change the flight attitude of the aircraft; the stored air is further supplied to the tail nozzle and is mixed with high-temperature, high-pressure and high-speed gas flow generated by the power system to form low-temperature, high-pressure and high-speed gas flow to be sprayed out backwards, so that pushing force is provided for the forward high-speed flight of the aircraft. Air crash caused by the faults of flaps, ailerons, elevators and rudders can be avoided, meanwhile, heat radiation is reduced, and the problem that existing various jet aircrafts are difficult to hidedue to high-temperature radiation is solved.

Description

technical field [0001] The invention belongs to the technical field of aircraft, and relates to a low-temperature stealth multi-nozzle aircraft. Background technique [0002] In the existing aircraft, the fixed-wing aircraft needs to use flaps, ailerons, horizontal tails, elevators, vertical tails, rudders, etc. to control the flight attitude of the aircraft, and it is easy to cause air accidents due to flaps, ailerons, elevators, and rudder failures. ; On the other hand, the heat radiation is high and it is difficult to be invisible. SUMMARY OF THE INVENTION [0003] (1) Purpose of the invention [0004] The purpose of the present invention is to provide a low-temperature stealth multi-nozzle aircraft based on multiple directions and multiple jets, so as to avoid air accidents caused by failures of flaps, ailerons, elevators, and rudders, reduce thermal radiation, and solve the problem of existing Various jets are difficult to stealth due to high temperature radiation. ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C15/02
CPCB64C15/02
Inventor 温江波甄灵许新芳雷超张春华章百宝董宇光周军赖武文
Owner 中国北方工业有限公司
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