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:
Aug. 30, 2022

Filed:

Jan. 22, 2020
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Gareth L Jones, Calidicot, GB;

Daniel J Williams, Bristol, GB;

Natalie C Wong, Bristol, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 21/02 (2006.01); F02K 3/10 (2006.01); F02C 9/48 (2006.01);
U.S. Cl.
CPC ...
F01D 21/02 (2013.01); F02K 3/10 (2013.01); F02C 9/48 (2013.01); F05D 2220/323 (2013.01); F05D 2240/60 (2013.01); F05D 2270/021 (2013.01); F05D 2270/023 (2013.01); F05D 2270/051 (2013.01); F05D 2270/304 (2013.01);
Abstract

A method is provided of controlling a gas turbine having a shaft connecting a compressor to a turbine, as well as having a reheat system, and a gas turbine. The method includes the steps of: operating the engine using the reheat system to provide a mass flow rate of reheat fuel into a gas flow of the gas turbine engine downstream of an exit of the turbine; detecting a shaft break event in the shaft; and in response to this detection, maintaining the mass flow rate of the reheat fuel being provided into the gas flow downstream of the turbine exit, whereby the maintained mass flow rate of reheat fuel raises a back pressure downstream of the turbine and thereby reduces a rotational speed of the turbine.


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