The invention relates to the field of aviation. A multi-functional supersonic single-engine aircraft comprises a fuselage, conical wings, a full-moving V-shaped empennage, extended side beams, lower lateral engine air inlets located below a front section of the fuselage and having a duct extending along a centerline of the aircraft, central and lateral payload cabins, a single-engine power plant comprising an engine, the engine has a rotatable propulsion nozzle disposed along the aircraft centerline. The aircraft design provides reduced aircraft size and lower weight, reduced aerodynamic drag, reduced RCS and radar features, high aircraft performance and maneuvering characteristics, excellent stability and controllability characteristics, increased payload cabin volume, multifunction large load capacity, and multifunction capacity of the aircraft.
本发明涉及航空领域。一种多功能超音速单发动机飞行器包括机身、锥形机翼、全动式V形尾翼、延长的侧梁、位于机身前部部段下方的具有沿着飞行器中心线延伸的管道的下部侧向发动机进气口、中央和侧向有效载荷舱、包括发动机的单发动机动力装置,所述发动机具有沿着所述飞行器中心线布置的可旋转推进喷嘴。所述飞行器设计提供减小的飞行器尺寸和较低的重量、减小的气动阻力、减小的RCS和雷达特征、高的飞行器性能和机动特性、优秀的稳定性和可控性特性、增大的有效载荷舱体积、多功能大型载荷能力、以及飞行器的多功能能力。
Multifunctional supersonic single-engine aircraft
多功能超音速单发动机飞行器
2024-03-26
Patent
Electronic Resource
Chinese