Title:
オフデザイン飛行条件で改善された吸気口性能のための超音速カレット吸気口システム前縁スラット
Document Type and Number:
Japanese Patent JP6885673
Kind Code:
B2
Abstract:
An engine inlet for efficient operation at both design Mach number and off-design Mach numbers with an inlet having a caret configuration with rotatably extending effective leading edges on the inlet from a retracted position aligned with a nominal Mach number shock wave to an extended position aligned with an off-design Mach number shock wave.
Inventors:
Huin, Tui
Application Number:
JP2016032739A
Publication Date:
June 16, 2021
Filing Date:
February 24, 2016
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D33/02; B64C30/00
Domestic Patent References:
| JP10306748A | ||||
| JP2000192850A |
Foreign References:
| CN103939217A |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation