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:
Sep. 22, 2026

Filed:

May. 14, 2024
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Craig W Bemment, Derby, GB;

Benjamin J Keeler, Chesterfield, GB;

Kevin R Mcnally, Derby, GB;

Andrea Minelli, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/14 (2006.01); F02C 7/36 (2006.01); F23K 5/20 (2006.01);
U.S. Cl.
CPC ...
F02C 7/14 (2013.01); F02C 7/36 (2013.01); F23K 5/20 (2013.01); F05D 2260/20 (2013.01); F23K 2300/204 (2020.05);
Abstract

A gas turbine includes an engine core with a turbine, a compressor, a combustor to combust a fuel, and a core shaft connecting the turbine to the compressor; a fan located upstream of the engine core; a fan shaft; a main gearbox that receives an input from the core shaft and outputs drive to the fan via the fan shaft; a primary oil loop system arranged to supply oil to lubricate the main gearbox; and a heat exchange system arranged to transfer heat between the oil and the fuel, the oil having an average temperature of at least 180° C. on entry to the heat exchange system at cruise conditions. A method of operating the turbine includes transferring heat from the oil to the fuel so as to lower the fuel viscosity to a value of less than or equal to 0.58 mm/s on entry to the combustor at cruise conditions.


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