US Patent 11859515 Gas turbine engines with improved guide vane configurations
Patent 11859515 was granted and assigned to General Electric on January, 2024 by the United States Patent and Trademark Office.
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US Patent 11859515 Gas turbine engines with improved guide vane configurations
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Patent abstract
There is provided apparatuses and methods for a gas turbine engine. The embodiments include a core section with a flow path. The flow path includes a stator vane array having outlet vanes. Each outlet vane has a trailing edge. A strut has a leading edge that is upstream of the trailing edges. Alternatively, the flow path includes a stator vane array having inlet vanes. Each inlet vane has a leading edge. The strut has a trailing edge that is downstream of the leading edges. There also is increased spacing between adjacent vanes and rotor blades.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Andrew Breeze-Stringfellow0
Darek Zatorski0
Tsuguji Nakano0
Date of Patent
January 2, 2024
0Patent Application Number
176868430
Date Filed
March 4, 2022
0Patent Citations
Patent Primary Examiner
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