Title:
吸気口
Document Type and Number:
Japanese Patent JP6813950
Kind Code:
B2
Abstract:
An apparatus is formed of a cowl and a flow inlet formed on an interior surface of the cowl. The flow inlet has a supersonic compression section attached to a subsonic diffusion section at a throat. The supersonic compression section includes an at least partially elliptical compression ramp which extends along an approximately 180 degree arc along the interior surface. The flow inlet may form part of an aircraft. A method of air flow using the flow inlet is also disclosed.
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Inventors:
Adamson, Eric E.
Hoogal, Spencer Robert
Hoogal, Spencer Robert
Application Number:
JP2016021511A
Publication Date:
January 13, 2021
Filing Date:
February 08, 2016
Export Citation:
Assignee:
The Boeing Company
International Classes:
F02C7/04; B64C30/00; B64D33/02; F02C7/00
Domestic Patent References:
| JP2003534960A | ||||
| JP2004526619A | ||||
| JP2009520142A |
Foreign References:
| US20080223978 | ||||
| US20050258307 | ||||
| CN101798961A | ||||
| US20090107557 | ||||
| US20130199621 |
Attorney, Agent or Firm:
Sonoda/Kobayashi Patent Business Corporation