US Patent 11480112 Acceleration of a gas turbine
All edits
Edits on 27 Apr, 2023
Golden AI
Infobox
Patent Citations
Edits on 25 Apr, 2023
Golden AI
Infobox
Edits on 22 Apr, 2023
Golden AI
Infobox
Is a
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
114801120
Date of Patent
October 25, 2022
0Patent Application Number
168926900
Date Filed
June 4, 2020
0Patent Citations
Patent Primary Examiner
CPC Code
Edits on 28 Oct, 2022
Golden AI
Edits made to:
Infobox (+13 properties)
Article (+650 characters)
US Patent 11480112 Acceleration of a gas turbine
Article
A gas turbine engine for an aircraft comprises a high-pressure (HP) spool comprising an HP compressor and a first electric machine driven by an HP turbine; a low-pressure (LP) spool comprising an LP compressor and a second electric machine driven by an LP turbine; a combustion system comprising a fuel metering unit; and an engine controller configured to, in response to a change of a throttle lever angle setting indicative of an acceleration event, increase fuel flow to the combustion system by the fuel metering unit, and to operate the first electric machine in a motor mode to increase the HP spool rotational speed and engine core mass flow.
Infobox
Is a
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
114801120
Date of Patent
October 25, 2022
0Patent Application Number
168926900
Date Filed
June 4, 2020
0Patent Citations
Patent Primary Examiner
CPC Code
Find more entities like US Patent 11480112 Acceleration of a gas turbine
Use the Golden Query Tool to find similar entities by any field in the Knowledge Graph, including industry, location, and more.
By using this site, you agree to our Terms of Service.