US Patent 11415064 Geared architecture for gas turbine engine
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Jason Husband0
William G. Sheridan0
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Patent Number
114150640
Date of Patent
August 16, 2022
0Patent Application Number
166896900
Date Filed
November 20, 2019
0Patent Citations
Patent Primary Examiner
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US Patent 11415064 Geared architecture for gas turbine engine
Article
A turbofan engine includes a fan section. A turbine section is in driving engagement with the fan section through a geared architecture. A flexible support supports the geared architecture relative to an engine static structure. A deflection limiter includes at least one of an axially extending branch or a radially extending branch. A flexible output shaft is in driving engagement with the fan section and driven by the geared architecture. A speed change mechanism for a gas turbine engine is also disclosed.
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Is a
Patent Jurisdiction
Patent Number
11415064
Date of Patent
August 16, 2022
Patent Application Number
16689690
Date Filed
November 20, 2019
Patent Citations
Patent Primary Examiner
CPC Code
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