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A low-temperature stealth multi-jet aircraft

An aircraft and multi-nozzle technology, applied in the field of aircraft, can solve problems such as difficulty in stealth, and achieve the effects of reducing heat radiation, large load range, and good safety

Active Publication Date: 2021-12-07
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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  • A low-temperature stealth multi-jet aircraft
  • A low-temperature stealth multi-jet aircraft
  • A low-temperature stealth multi-jet aircraft

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Embodiment Construction

[0027] In order to make the purpose, content and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with 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: aircraft main body 1, power system 2, control system 3, bottom nozzle 4, vertical nozzle 5, horizontal nozzle 6, pitch nozzle 7, tail nozzle 8, gas pipeline 9, nozzle A valve 10 and a cooling and supercharging 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 U.S. B2 stealth bomber as a kind of aerodynamic model, and the present embodiment is demonstrated.

[0030] I...

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Abstract

The invention belongs to the field of aircraft and discloses a low-temperature stealth multi-nozzle aircraft, which includes: aircraft main body, power system, control system, bottom nozzle, vertical nozzle, horizontal nozzle, pitch nozzle, tail nozzle, gas pipeline, nozzle valve and cooling Supercharging device, the cooling and supercharging device is located in the middle of the main body of the aircraft, which is used to inhale, compress, cool down and store a part of the air entering the front air inlet of the power system, and supply it to each nozzle to change the flight attitude of the aircraft; The stored gas is also supplied to the tail nozzle for mixing with the high-temperature, high-pressure, and high-speed airflow generated by the power system to form a low-temperature, high-pressure, and high-speed airflow that is ejected backward, providing propulsion for the aircraft to fly forward at high speed. The invention can avoid air accidents caused by failures of flaps, ailerons, elevators and rudders, reduce heat radiation, and solve the problem that various existing jet aircraft are difficult to hide due to high-temperature radiation.

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] Among existing aircraft, fixed-wing aircraft need to use flaps, ailerons, horizontal tail, elevator, vertical tail, rudder, etc. to control the flight attitude of the aircraft, which is prone to cause air crashes due to failures of flaps, ailerons, elevators, and rudders. ; On the other hand, the heat radiation is high and it is difficult to be invisible. Contents of the invention [0003] (1) Purpose of the invention [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 because of high temperature radiation. ...

Claims

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Application Information

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Patent Type & Authority Patents(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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