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:
Nov. 04, 2014

Filed:

Jun. 30, 2010
Applicants:

Donald George Lachapelle, Cincinnati, OH (US);

Christopher Charles Glynn, Lawrenceburg, IN (US);

Donald Lee Gardner, West Chester, OH (US);

Stephen Craig Mitchell, West Chester, OH (US);

Mullahalli Venkataramaniah Srinivas, Mason, OH (US);

Edward Atwood Rainous, Cincinnati, OH (US);

David Lance Pennekamp, Hamilton, OH (US);

Inventors:

Donald George LaChapelle, Cincinnati, OH (US);

Christopher Charles Glynn, Lawrenceburg, IN (US);

Donald Lee Gardner, West Chester, OH (US);

Stephen Craig Mitchell, West Chester, OH (US);

Mullahalli Venkataramaniah Srinivas, Mason, OH (US);

Edward Atwood Rainous, Cincinnati, OH (US);

David Lance Pennekamp, Hamilton, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); F02C 7/20 (2006.01); B64D 27/18 (2006.01); B64D 27/26 (2006.01);
U.S. Cl.
CPC ...
B64D 27/26 (2013.01); B64D 27/18 (2013.01); B64D 2027/268 (2013.01); B64D 2027/266 (2013.01); B64D 2027/264 (2013.01);
Abstract

An assembly includes a unitary nacelle structure and an integrated fan housing for a gas turbine engine assembly. The unitary nacelle structure includes an inlet region and a fan cowl region, and is configured to at least partially circumscribe the integrated fan housing. The integrated fan housing comprises an integral composite structure and includes a fan case sized and configured for encircling a fan blade assembly of an associated gas turbine engine, a fan hub, and a plurality of fan outlet guide vanes. The unitary nacelle structure cooperates with the integrated fan housing to transfer static and dynamic loads directly to a support structure, rather than through the engine core, to minimize backbone bending.


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