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:
Jan. 14, 2025

Filed:

Jun. 25, 2024
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Andrea Minelli, Derby, GB;

Craig W Bemment, Derby, GB;

Benjamin J Keeler, Chesterfield, GB;

Kevin R McNally, Derby, GB;

Martin K Yates, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/14 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/14 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F05D 2260/213 (2013.01); F05D 2260/98 (2013.01);
Abstract

A method of operating an aircraft gas turbine engine including: a core including a turbine, a compressor, a combustor to combust fuel, and a core shaft connecting the turbine to the compressor; a fan upstream of the core; a fan shaft; a bearing supporting the fan shaft; an oil loop system supplying oil to the bearing; and a heat exchange system including: an air-oil heat exchanger through which oil in the oil loop system flows; and a fuel-oil heat exchanger through which oil in the oil loop system and fuel flow to transfer heat between the oil and the fuel; and a bypass pipe to allow a proportion of the oil to flow past one of the air-oil and the fuel-oil heat exchanger; and a bypass valve to allow the proportion of the oil sent through the bypass pipe to be varied.


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