The invention discloses a fluid thrust vectoring nozzle and wing integrated aircraft. The fluid thrust vectoring nozzle and wing integrated aircraft comprises a flight-launch integrated wing section, an engine, an engine tail nozzle and a fluid thrust vectoring nozzle, the engine is embedded in the flying and launching integrated airfoil profile, and a tail nozzle of the engine is preset to be upwards inclined. According to the fluid thrust vectoring nozzle and wing integrated aircraft disclosed by the invention, the thickness of the rear edge of the wing is effectively reduced, so that the resistance of a rear body in the flying process is reduced; the structure weight is light, the number of movable parts is small, the deflection response is fast, and the controllable pitching moment can be provided in the cruise attack angle of the aircraft; the lift coefficient and the control torque are improved; and the infrared stealth performance of the aircraft is enhanced.
本发明公开了一种流体推力矢量喷管与机翼一体化的飞行器,包括飞发一体化翼型、发动机、发动机尾喷口和流体推力矢量喷管;所述发动机内埋于所述飞发一体化翼型内,所述发动机尾喷口预置上偏。本发明公开的一种流体推力矢量喷管与机翼一体化的飞行器,有效降低了机翼后缘的厚度,从而减小了飞行过程中的后体阻力;结构重量轻,活动部件少,偏转响应快,可在飞行器巡航迎角内提供可操纵的俯仰力矩;提高了升力系数和控制力矩;增强了飞行器红外隐身性能。
Fluid thrust vectoring nozzle and wing integrated aircraft
一种流体推力矢量喷管与机翼一体化的飞行器
2024-01-30
Patent
Electronic Resource
Chinese
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