US Patent 11459893 Efficient gas turbine engine installation and operation
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Edits on 31 Jul, 2023
Golden AI
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Edits on 27 Apr, 2023
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Patent Applicant
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Patent Jurisdiction
Patent Number
114598930
Date of Patent
October 4, 2022
0Patent Application Number
172125540
Date Filed
March 25, 2021
0Patent Citations
Patent Primary Examiner
Edits on 1 Apr, 2023
Golden AI
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Edits on 8 Oct, 2022
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US Patent 11459893 Efficient gas turbine engine installation and operation
Article
A gas turbine engine that has improved fuel burn provides operability and/or maintenance requirements when installed on an aircraft. The gas turbine engine is provided with a core compressor that includes twelve, thirteen or fourteen rotor stages. The gas turbine engine has a ratio of a core compressor aspect ratio divided by a core compressor pressure ratio is in the range of from 0.03 to 0.09. This results in an optimum balance between installation benefits, operability, maintenance requirements and engine efficiency when the gas turbine engine is installed on an aircraft.
Infobox
Is a
Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
114598930
Date of Patent
October 4, 2022
0Patent Application Number
172125540
Date Filed
March 25, 2021
0Patent Citations
Patent Primary Examiner
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