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:
Feb. 07, 2017
Filed:
May. 22, 2014
Applicant:
Rolls-royce Deutschland Ltd & CO KG, Blankenfelde-Mahlow, Dahlewitz, DE;
Inventor:
Jürgen Beier, Schulzendorf, DE;
Assignee:
ROLLS-ROYCE DEUTSCHLAND LTD & CO KG, Dahlewitz, DE;
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/20 (2006.01); B64D 27/26 (2006.01); F02C 7/32 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/20 (2013.01); B64D 27/26 (2013.01); F02C 7/32 (2013.01); B64D 2033/024 (2013.01); F05D 2260/20 (2013.01); Y02T 50/672 (2013.01); Y02T 50/676 (2013.01);
Abstract
A gas turbine engine assembly is connected to a pylon for mounting the gas turbine engine to an aircraft. The assembly has a frame supporting at least one accessory independently of the gas turbine engine. The frame is attached to the pylon at forward and rearward engine mounting locations. The frame comprises at least one hollow tube and at least one duct is arranged to supply coolant into the at least one hollow tube and the at least one hollow tube is arranged to supply coolant to the at least one accessory.