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:
Dec. 03, 2024

Filed:

Jun. 20, 2023
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Craig W Bemment, Derby, GB;

Alastair G Hobday, Derby, GB;

Benjamin J Keeler, Chesterfield, GB;

Christopher P Madden, Derby, GB;

Andrea Minelli, Derby, GB;

Andrew T Smith, Derby, GB;

Peter Swann, Derby, GB;

Martin K Yates, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/38 (2006.01); F02C 7/14 (2006.01); F02C 7/16 (2006.01); F02C 7/224 (2006.01);
U.S. Cl.
CPC ...
F02C 9/38 (2013.01); F02C 7/14 (2013.01); F02C 7/16 (2013.01); F02C 7/224 (2013.01); F05D 2260/213 (2013.01);
Abstract

A method of operating a gas turbine engine including: a combustor arranged to combust a fuel; and a fuel management system arranged to provide the fuel to the combustor, wherein the fuel management system includes two fuel-oil heat exchangers through which oil and fuel flow, which are arranged to transfer heat between the oil and fuel and include primary and secondary fuel-oil heat exchangers; a fuel pump arranged to deliver the fuel to the combustor, wherein the fuel pump is located between the heat exchangers; and a recirculation valve located downstream of the primary heat exchanger, the recirculation valve arranged to allow a controlled amount of fuel which has passed through the primary heat exchanger to be returned to the inlet. The method includes selecting one or more fuels such that the calorific value of the fuel provided to the gas turbine engine is at least 43.5 MJ/kg.


Find Patent Forward Citations

Loading…