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US Patent 11971051 Compressor flowpath
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Patent
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Date Filed
June 9, 2023
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Date of Patent
April 30, 2024
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Patent Application Number
18207805
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Patent Citations
US Patent 7021042 Geartrain coupling for a turbofan engine
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US Patent 7219490 Nested core gas turbine engine
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US Patent 7328580 Chevron film cooled wall
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US Patent 7374403 Low solidity turbofan
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US Patent 7487630 Jet engine with compact arrangement of fan
0
US Patent 7591754 Epicyclic gear train integral sun gear coupling design
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US Patent 7632064 Variable geometry guide vane for a gas turbine engine
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US Patent 7662059 Lubrication of windmilling journal bearings
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US Patent 7694505 Gas turbine engine assembly and method of assembling same
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US Patent 7806651 Method for designing a low-pressure turbine of an aircraft engine, and low-pressure turbine
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•••
Patent Inventor Names
Lisa I. Brilliant
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Yuan Dong
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Becky E. Rose
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Stanley J. Balamucki
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11971051
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Patent Primary Examiner
Justin D Seabe
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CPC Code
F02K 3/06
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F02K 3/04
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F04D 29/522
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F04D 29/563
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F04D 29/547
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F04D 29/321
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F04D 25/045
0
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