Air-launching decoy aircraft

A decoy machine and air-launched technology, which is applied in the direction of motor vehicles, aircraft parts, launch devices, etc., can solve the problems of not being able to adapt to confrontation, and unable to conduct radar deception at the same time, and achieve the effect of good deception effect.

Inactive Publication Date: 2017-08-18
CHENGDU AIRCRAFT INDUSTRY GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The disadvantage of the above method is that radar decoy and infrared decoy cannot be carried out at the same time, so it cannot adapt to the confrontation with advanced anti-jamming technology

Method used

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  • Air-launching decoy aircraft
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Embodiment Construction

[0020] The present invention will be further described below in conjunction with an example of the present invention and accompanying drawings.

[0021] see figure 1 , figure 2 , the air-launched bait machine of the present invention is to be installed in Y-shaped distribution empennage 3 that is positioned at fuselage 1 afterbody 1 tail by 1 fuselage 1, 2 swept backs, 3 of 1 The engine 4 of fuselage 1 afterbody, 1 electronic decoy 5 installed in fuselage 1 front, 1 energy device 6 etc. that are installed in fuselage 1 middle part are composed.

[0022] After the air-launched bait machine is released, the lift generated by wing 2 is balanced with the gravity of the air-launched bait machine to maintain the air-launched bait machine in level flight; the dihedral angle of wing 2 is 15° to provide enough roll for the air-launched bait machine Stability, the empennage 3 provides sufficient heading stability and pitch stability for the air-launched bait machine; the thrust gener...

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PUM

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Abstract

The invention discloses an air-launching decoy aircraft comprising a fuselage (1), aerofoils (2), empennages (3), an engine and an electronic decoy (5). The air-launching decoy aircraft is characterized in that the aerofoils (2) are positioned at the middle of the fuselage (1), and used for providing lift for the air-launching decoy aircraft during flight; the empennages (3) are fixed to the tail of the fuselage (1); the electronic decoy (5) is installed in the fuselage (1) and used for transmitting radio signals after being powered-on; the engine is installed at the tail of the fuselage (1); each aerofoil (2) has an anhedral, and the anhedral is within the range of 0-15 degrees. A high temperature tail flame (9) generated by the engine serves as the infrared decoy. The air-launching decoy aircraft is simple in principle and high in implementability. The stability of the aircraft is maintained without a control system, costs are favorably reduced, radar decoying and infrared decoying are simultaneously realized, and the air-launching decoy aircraft can be used as a decoy in batches.

Description

technical field [0001] The invention belongs to the specialty of aircraft design, and relates to an aircraft design and a decoy method. Background technique [0002] At present, the way for aircraft to deceive radio or infrared detection is to carry electronic interference equipment or release interference bombs outside the aircraft. The disadvantage of the above method is that radar decoy and infrared decoy cannot be performed at the same time, so it cannot adapt to the confrontation with advanced anti-jamming technology. Contents of the invention [0003] The purpose of the present invention is to overcome the deficiencies in the prior art, and propose an air-launched bait machine with effective thinking, low cost and engineering. Taking into account the needs of radar decoy and infrared decoy. [0004] The technical scheme that the present invention realizes above-mentioned purpose is: [0005] An air-launched decoy aircraft, including a fuselage, wings, empennage, e...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D1/02
CPCB64C39/02B64D1/02
Inventor 许云飞冯文梁邓建张志坚周萍
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
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