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:
May. 03, 2016

Filed:

Oct. 12, 2006
Applicants:

Constantine Baltas, Manchester, CT (US);

Amr Ali, Windsor, CT (US);

Inventors:

Constantine Baltas, Manchester, CT (US);

Amr Ali, Windsor, CT (US);

Assignee:

United Technologies Corporation, Hartford, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02K 3/00 (2006.01); F02K 3/075 (2006.01); F02K 1/08 (2006.01); F02K 1/38 (2006.01); F03G 7/06 (2006.01); B64C 9/38 (2006.01); F02K 1/12 (2006.01); F02K 3/04 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02K 3/075 (2013.01); F02K 1/08 (2013.01); F02K 1/085 (2013.01); F02K 1/386 (2013.01); F03G 7/065 (2013.01); B64C 9/38 (2013.01); F02K 1/12 (2013.01); F02K 1/1207 (2013.01); F02K 3/00 (2013.01); F02K 3/04 (2013.01); F02K 3/06 (2013.01); F05D 2300/505 (2013.01);
Abstract

A gas turbine engine () includes a fan (), a nacelle () arranged about the fan, and an engine core at least partially within the nacelle. A fan bypass passage () downstream of the fan between the nacelle and the gas turbine engine conveys a bypass airflow () from the fan. A nozzle () associated with the fan bypass passage is operative to control the bypass airflow. The nozzle includes a shape memory material having a first solid state phase that corresponds to a first nozzle position and a second solid state phase that corresponds to a second nozzle position.


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