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US Patent 11674415 Front section stiffness ratio
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Is a
Patent
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Date Filed
October 28, 2021
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Date of Patent
June 13, 2023
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Patent Application Number
17512824
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Patent Citations
US Patent 9784129 Rear mount assembly for gas turbine engine
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US Patent 9032740 Engine assembly for an aircraft comprising attachments for engines offset below on the fan frame
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US Patent 10190501 Gas turbines engine support structures
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US Patent 7654075 Fan static structure
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US Patent 8979491 Turbofan mounting arrangement
0
Patent Jurisdiction
United States Patent and Trademark Office
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Patent Number
11674415
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Patent Primary Examiner
Eldon T Brockman
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CPC Code
F02C 7/36
0
F01D 5/02
0
F01D 25/24
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F01D 25/243
0
F01D 25/246
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F01D 25/26
0
F02K 3/06
0
F05D 2220/32
0
F02C 7/20
0
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