The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Oct. 17, 2017

Filed:

Apr. 25, 2014
Applicant:

Rohr, Inc., Chula Vista, CA (US);

Inventors:

Steven M. Kestler, Winchester, CA (US);

Prithvi Sundar, San Jose, CA (US);

Yuan Li, San Jose, CA (US);

Assignee:

ROHR, INC., Chula Vista, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 21/06 (2006.01); B64D 33/02 (2006.01); F02C 7/04 (2006.01); B64D 29/00 (2006.01);
U.S. Cl.
CPC ...
B64C 21/06 (2013.01); B64D 29/00 (2013.01); B64D 33/02 (2013.01); F02C 7/04 (2013.01); B64C 2230/04 (2013.01); B64D 2033/0226 (2013.01); F05D 2270/17 (2013.01); Y02T 50/166 (2013.01); Y02T 50/671 (2013.01);
Abstract

An aircraft inlet comprising an annular air intake structure defined by an inner surface and an outer surface, a plurality of perforations formed in the outer surface of the aircraft inlet, a plenum chamber situated within the aircraft inlet and configured to receive air entering the plurality of perforations, and/or a plurality of sensors disposed about the outer surface of the aircraft inlet, each sensor associated with a region of the plurality of perforations. Each sensor may comprise a hot film anemometer. The aircraft inlet may further comprise a regulator coupled at one end to the plenum chamber and at another end to a pump, wherein the regulator regulates a suction produced by the pump.


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