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:
Jul. 17, 2018

Filed:

Sep. 16, 2014
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Robert Goulds, Derby, GB;

Brian Richard Lace, Derby, GB;

Richard Peace, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 7/32 (2006.01); F01D 25/12 (2006.01); F01D 25/14 (2006.01); F02C 7/24 (2006.01); F02C 7/12 (2006.01); F01D 25/08 (2006.01); F02C 7/25 (2006.01); F02C 7/28 (2006.01); F16C 1/10 (2006.01); F16C 1/26 (2006.01); F02C 3/14 (2006.01); F02C 7/18 (2006.01); F02C 6/04 (2006.01); F02C 6/06 (2006.01); F02C 6/08 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); F01D 25/08 (2013.01); F01D 25/12 (2013.01); F01D 25/14 (2013.01); F01D 25/145 (2013.01); F02C 3/14 (2013.01); F02C 7/12 (2013.01); F02C 7/125 (2013.01); F02C 7/18 (2013.01); F02C 7/24 (2013.01); F02C 7/25 (2013.01); F02C 7/28 (2013.01); F16C 1/10 (2013.01); F16C 1/262 (2013.01); F02C 6/04 (2013.01); F02C 6/06 (2013.01); F02C 6/08 (2013.01); F05D 2260/20 (2013.01); F05D 2260/50 (2013.01); F16C 1/103 (2013.01); F16C 2360/23 (2013.01);
Abstract

A gas turbine engine having a fire wall configured to provide a fire resistant barrier between a first zone and a second zone in the gas turbine engine, the second zone being hotter than the first zone. The gas turbine engine also has: (i) an actuator located in the first zone, (ii) an actuatable device that is located in the second zone, (iii) a bypass duct, (iv) an off-take device to extract cooling air from the bypass duct in the gas turbine engine and to supply the extracted cooling air into the elongate housing/shell, the off-take device having a first passage and a second passage, and (v) a mechanical force transmitting device that extends from the actuator to the actuatable device via a hole in the fire wall. The mechanical force transmitting device is configured to actuate the actuatable device by transmitting a mechanical force to the actuatable device.


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