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公开(公告)号：US10859003B2
公开(公告)日：2020-12-08
申请号：US16666928
申请日：2019-10-29
Applicant: ROLLS-ROYCE PLC
Inventor： Luis F Llano , Arthur L Rowe
Abstract: A control system for a gas turbine engine includes an engine core, the engine core including combustion equipment, a turbine, a compressor, and a core shaft connecting the turbine to the compressor. The control system includes at least one variable stator vane for controlling the angle at which gas enters the engine core, and there is a bypass passage within the engine core for directing gas flow to bypass the combustion equipment.
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