US Patent 11280267 Geared turbofan engine gearbox arrangement
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Patent Number
112802670
Date of Patent
March 22, 2022
0Patent Application Number
170071660
Date Filed
August 31, 2020
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112802670
Date of Patent
March 22, 2022
0Patent Application Number
170071660
Date Filed
August 31, 2020
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US Patent 11280267 Geared turbofan engine gearbox arrangement
Article
A gas turbine engine according to the present disclosure includes, among other things, a fan section having a plurality of fan blades, the plurality of fan blades having a peak tip radius Rt and an inboard leading edge radius Rh at a first inboard boundary of a first flowpath, and a core engine including a first turbine configured to drive a first compressor, and a fan drive turbine configured to drive the fan section.
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Patent jurisdiction
Patent number
11280267
Date of patent
March 22, 2022
Patent application number
17007166
Date Filed
August 31, 2020
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