US Patent 11859538 Geared turbofan engine with targeted modular efficiency
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US Patent 11859538 Geared turbofan engine with targeted modular efficiency
Article
Patent abstract
A turbine engine includes a first compression section includes a last blade trailing edge radial tip length that is greater than about 67% of the radial tip length of a leading edge of a first stage of the first compression section. A second compression section includes a last blade trailing edge radial tip length that is greater than about 57% of a radial tip length of a leading edge of a first stage of the first compression section.
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Patent Inventor Names
Frederick M. Schwarz0
Date of Patent
January 2, 2024
0Patent Application Number
180968720
Date Filed
January 13, 2023
0Patent Citations
Patent Primary Examiner
CPC Code
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