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US Patent 11549373 Reduced deflection turbine rotor
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Is a
Patent
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Date Filed
December 16, 2020
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Date of Patent
January 10, 2023
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Patent Application Number
17123344
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Patent Citations
US Patent 10724380 CMC blade with internal support
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US Patent 10794188 Rotor blade assembly comprising a ring-shaped or disc-shaped blade carrier and a radially inner reinforcement structure
US Patent 10161773 Methods and apparatus to determine airflow conditions at an inlet of an engine
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US Patent 10358924 Turbofan arrangement with blade channel variations
US Patent 10371047 Geared turbofan engine with targeted modular efficiency
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US Patent 10371061 Turbine section of high bypass turbofan
Patent Inventor Names
Michael G. McCaffrey
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Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11549373
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Patent Primary Examiner
Loren C Edwards
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CPC Code
F01D 11/22
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F01D 25/16
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F01D 25/28
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F05D 2240/24
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F05D 2240/307
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F01D 5/025
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F05D 2260/30
0
F02C 7/06
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F02C 7/36
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F02C 3/107
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