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.
Patent No.:
Date of Patent:
Dec. 25, 2018
Filed:
Dec. 23, 2013
Applicant:
General Electric Company, Schenectady, NY (US);
Inventors:
Assignee:
General Electric Company, Schenectady, NY (US);
Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/18 (2006.01); F02K 1/70 (2006.01); F02K 1/72 (2006.01); F02K 1/76 (2006.01); F02C 6/08 (2006.01); B64D 27/16 (2006.01); B64D 29/00 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F02C 7/185 (2013.01); B64D 27/16 (2013.01); B64D 29/00 (2013.01); F02C 6/08 (2013.01); F02C 7/18 (2013.01); F02K 1/70 (2013.01); F02K 1/72 (2013.01); F02K 1/766 (2013.01); F02K 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2260/20 (2013.01); F05D 2260/232 (2013.01); Y02T 50/676 (2013.01);
Abstract
An aircraft with aturbofan engine assembly having at least one compressor, a nacelle surrounding the turbine engine and defimng an annular bypass duct between the nacelle and the turbine engine, a thrust reverser having at least one moveable control surface, a thrust reverser locking system configured to selectively lock the thrust reverserand an injection cooling system.