The invention discloses a hydrogen-electricity hybrid energy supersonic airliner, and belongs to the technical field of engineering, the aircraft comprises an aerodynamic configuration, a hydrogen-electricity hybrid driven power device and an integral hydrogen tank for storing hydrogen fuel, the aerodynamic configuration comprises a slender fuselage, wings comprising lifting surfaces, an empennage and canards; the power device comprises a gas turbine main engine and an electric propulsion ducted fan; the integral hydrogen tank comprises a pressure-bearing inner tank, a heat insulating layer and a supporting structure, the power device is connected with the fuselage and the wings; the hydrogen tank is connected with the fuselage through a supporting structure. According to the scheme, the high lift-drag ratio and the low sound explosion requirement of the aircraft are guaranteed by adding the lifting force surfaces on the wings, zero carbon emission is achieved by introducing hydrogen energy, meanwhile, in order to increase the hydrogen fuel storage amount of the aircraft, the integral hydrogen tank is adopted, and the voyage requirement of the aircraft is guaranteed.
本发明公开了一种氢电混合能源的超声速客机,属于工程技术领域,该飞机包括:气动外形,氢电混合驱动的动力装置,储存氢燃料的整体式氢罐,其中,所述气动外形包括细长体机身,包含升力面的机翼,尾翼与鸭翼;所述动力装置包括燃气涡轮主发动机和电推进涵道风扇;所述整体式氢罐氢罐包括承压内罐,绝热层,支撑结构;动力装置与机身和机翼连接;氢罐通过支撑结构与机身连接。本发明方案通过在机翼上增加升力面确保飞机的高升阻比与低声爆需求,通过引入氢能源实现零碳排放,同时为了增加飞机的氢燃料储量,采用整体式氢罐,保障了飞机的航程需求。
Hydrogen-electricity hybrid energy supersonic passenger plane
一种氢电混合能源的超声速客机
2025-04-01
Patent
Electronic Resource
Chinese
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