-
公开(公告)号:US12253049B2
公开(公告)日:2025-03-18
申请号:US18556356
申请日:2022-03-21
Applicant: NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS , BEIJING AEROSPACE TECHNOLOGY INSTITUTE
Inventor: Hexia Huang , Zhengkang Lin , Xuebin Tang , Yuan Qin , Huijun Tan , Hang Zhang , Ziren Wang , Chao Li , Xiru Xu
Abstract: The present invention provides a hypersonic large internal contraction ratio air inlet channel having stepless adjustable air release valve, including an air inlet channel front body, an air-discharging slit cover plate, sidewalls, a lip cover, air-discharging cavities, valve plates, partition plates, a rotatable shaft, an expansion section and a driver. The valve plates are rotated through the driver according to the actual working conditions of air inlet channel, the minimum cross-section of the air discharging flow path is thus changed, and a stepless dynamic adjustment of the air discharging flow of the air inlet channel can be realized, so that the aerodynamic performance of the air inlet channel is improved, and the air discharging resistance of the air vehicle is reduced.
-
2.
公开(公告)号:US20240174371A1
公开(公告)日:2024-05-30
申请号:US18556356
申请日:2022-03-21
Applicant: NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS , BEIJING AEROSPACE TECHNOLOGY INSTITUTE
Inventor: Hexia HUANG , Zhengkang LIN , Xuebin TANG , Yuan QIN , Huijun TAN , Hang ZHANG , Ziren WANG , Chao LI , Xiru XU
IPC: B64D33/02
CPC classification number: B64D33/02 , B64D2033/026
Abstract: The present invention provides a hypersonic large internal contraction ratio air inlet channel having stepless adjustable air release valve, including an air inlet channel front body, an air-discharging slit cover plate, sidewalls, a lip cover, air-discharging cavities, valve plates, partition plates, a rotatable shaft, an expansion section and a driver. The valve plates are rotated through the driver according to the actual working conditions of air inlet channel, the minimum cross-section of the air discharging flow path is thus changed, and a stepless dynamic adjustment of the air discharging flow of the air inlet channel can be realized, so that the aerodynamic performance of the air inlet channel is improved, and the air discharging resistance of the air vehicle is reduced.
-