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:

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:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/262 (2006.01); F02K 1/12 (2006.01); F02K 1/15 (2006.01); F02K 3/075 (2006.01);
U.S. Cl.
CPC ...
F02C 7/262 (2013.01); F02K 1/1207 (2013.01); F02K 1/15 (2013.01); F02K 3/075 (2013.01); F05D 2260/85 (2013.01); F05D 2270/092 (2013.01);
Abstract

An example turbofan engine restarting system includes a core nacelle housing, a compressor, and a turbine. The core nacelle is disposed within a fan nacelle. A bypass flowpath downstream from the turbofan is arranged between the two nacelles. A controller is programmed to manipulate the nozzle exit area of the bypass flowpath to facilitate startup of the engine. In one example, the controller manipulates the nozzle exit area using hinged flaps in response to an engine shutdown condition. The flaps open and close to adjust the nozzle exit area and the associated bypass flow rate, the mass flow rate of the air through the core nacelle and the rotational speed of the compressor rotor.


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