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公开(公告)号:US20240191658A1
公开(公告)日:2024-06-13
申请号:US18512999
申请日:2023-11-17
Applicant: Rolls-Royce plc
Inventor: David M. Donnelly , Derek S. Wall , Jonathan Wieland
CPC classification number: F02C7/12 , F01D21/003 , F01D21/12 , F05D2260/20
Abstract: A method of operating a gas turbine engine having a spool includes executing, by a controller, a pre-shutdown procedure. The pre-shutdown procedure includes: determining a parameter associated with a thermal condition of the gas turbine engine; and calculating an idle period for an idle rotation operation to be performed in a shutdown procedure. Calculation of the idle period is based on the determined parameter.
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公开(公告)号:US12286935B2
公开(公告)日:2025-04-29
申请号:US18176777
申请日:2023-03-01
Applicant: ROLLS-ROYCE plc
Inventor: Derek S. Wall , Asad Mustafa , Robert Johnson , Jonathan Wieland
IPC: F02C9/00
Abstract: Disclosed is a computer-implemented method for controlling an engine system of a vehicle comprising: determining an operating condition of the vehicle; determining one or more contextual conditions relevant to the vehicle; selecting, based upon both the determined operating condition and the determined one or more contextual conditions, a control profile for the engine system from a directory comprising a plurality of control profiles having different control characteristics; applying the selected control profile to a controller of the engine system; and controlling the engine system with the controller in accordance with the selected control profile. Also disclosed are an engine control system, a gas turbine engine, and an aircraft.
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公开(公告)号:US20240191633A1
公开(公告)日:2024-06-13
申请号:US18513073
申请日:2023-11-17
Applicant: ROLLS-ROYCE PLC
Inventor: David M. Donnelly , Derek S. Wall , Jonathan Wieland
CPC classification number: F01D21/12 , F02C7/268 , F05D2270/3032
Abstract: A method of operating a gas turbine engine having a spool includes executing, by a controller, a shutdown procedure. The shutdown procedure includes: performing an idle rotation operation; determining a parameter associated with a thermal condition of the gas turbine engine while the idle rotation operation is performed; determining, based on the determined parameter, whether the gas turbine engine has met a pre-determined criterion corresponding to a thermally stabilised condition; and terminating the idle rotation operation in response to a determination that the gas turbine engine has met the pre-determined criterion.
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