US Patent 11549464 Hybrid gas turbine engine starting control
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Patent Inventor Names
Gary Collopy0
Neil Terwilliger0
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US Patent 11549464 Hybrid gas turbine engine starting control
Article
A system includes a gas turbine engine having a low speed spool, a high speed spool, and a combustor. The system also includes a low spool motor configured to augment rotational power of the low speed spool. The system further includes a controller configured to cause fuel flow. The controller is operable to control the low spool motor to drive rotation of the low speed spool responsive to a thrust command while the controller does not command fuel flow to the combustor.
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Patent Jurisdiction
Patent Number
115494640
Date of Patent
January 10, 2023
0Patent Application Number
169366020
Date Filed
July 23, 2020
0Patent Citations
Patent Primary Examiner
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