Invention Grant
- Patent Title: Supersonic air intake passage capable of achieving synchronous adjustment of capturing area and throat area
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Application No.: US16652074Application Date: 2018-08-14
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Publication No.: US11542867B2Publication Date: 2023-01-03
- Inventor: Huijun Tan , Yazhou Liu , Fajia Sheng , Ziyun Wang , Hexia Huang , Yue Zhang
- Applicant: NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS
- Applicant Address: CN Jiangsu
- Assignee: NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS
- Current Assignee: NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS
- Current Assignee Address: CN Jiangsu
- Agency: JCIP Global Inc.
- Priority: CNCN201710906033 20170929
- International Application: PCT/CN2018/100401 WO 20180814
- International Announcement: WO2019/062361 WO 20190404
- Main IPC: F02C7/057
- IPC: F02C7/057 ; B64C1/38 ; F02C7/00 ; F02K1/16

Abstract:
The present invention discloses a supersonic inlet with synchronous adjustment of capture area and throat area, wherein the throat area may be adjusted by providing a movable throat section, while the capture area may be adjusted by providing a movable cowl section at the front end of the cowl lip, thereby realizing the effect that the capture area and the throat area of the inlet may be adjusted in synchronization. Meanwhile, the present invention also provides a control method and a design method of the above-mentioned inlet. The present invention greatly simplifies the actuation system and control system, significantly reduces the weight of the accessory system, and enables the performance of the inlet within a wide envelope range to be maintained in an excellent state.
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