Title:
超音速キャレットインレットシステム
Document Type and Number:
Japanese Patent JP6758835
Kind Code:
B2
Abstract:
An engine inlet (10) for efficient operation in both subsonic and supersonic flight wherein the inlet has a caret configuration, is rotatable about an off-body axis (30) for compression ramp angle and capture area variation and a diffuser (14) is engaged to the inlet in a scrubbing relationship to maintain a seal upon rotation of the inlet.
Inventors:
Huin, Tui
Application Number:
JP2016008389A
Publication Date:
September 23, 2020
Filing Date:
January 20, 2016
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D33/02; B64C30/00; F02C7/00; F02C7/042; F02C7/045; F02K3/06
Domestic Patent References:
| JP45008483Y1 | ||||
| JP2009520142A | ||||
| JP53030006U |
Foreign References:
| US20090114774 | ||||
| GB899625A | ||||
| US2932945 |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation