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:
Jan. 05, 2016

Filed:

Jul. 02, 2007
Applicants:

Ashok K. Jain, Tempe, AZ (US);

Michael Winter, New Haven, CT (US);

Inventors:

Ashok K. Jain, Tempe, AZ (US);

Michael Winter, New Haven, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/042 (2006.01); F02K 3/06 (2006.01); B64D 33/02 (2006.01); F02C 7/045 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); B64D 33/02 (2013.01); F02C 7/042 (2013.01); F02C 7/045 (2013.01); F05D 2270/62 (2013.01); F05D 2270/64 (2013.01); F05D 2300/505 (2013.01); Y02T 50/671 (2013.01); Y10T 137/0645 (2015.04);
Abstract

A gas turbine engine includes a compressor section, a combustor section, a turbine section and a nacelle assembly which at least partially surrounds the compressor section, the combustor section and the turbine section. At least a portion of the nacelle assembly includes an adjustable contour. The portion of the nacelle assembly including the adjustable contour is selectively moveable between a first portion and a second position to influence the adjustable contour of the nacelle assembly. A controller identifies an abnormal aircraft operating condition and selectively moves the portion of the nacelle assembly including the adjustable contour between the first position and the second position in response to detecting the abnormal aircraft operating condition.


Find Patent Forward Citations

Loading…