US Patent 9970323 Geared turbofan engine with optimized diffuser case flange location
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Patent abstract
A gas turbine engine has a compressor section, a compressor case substantially surrounding the compressor section, and a diffuser case attached at an attachment interface to the compressor case. The attachment interface is between a forward and an aft end of the compressor. A geared turbofan is also disclosed.
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Patent Inventor Names
Frederick M. Schwarz0
Gabriel L. Suciu0
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US Patent 09970323 Geared turbofan engine with optimized diffuser case flange location US Patent 9970323 Geared turbofan engine with optimized diffuser case flange location
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Patent Number
099703230
Patent Number
99703230
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Patent Applicant
Patent Jurisdiction
Patent Number
099703230
Date of Patent
May 15, 2018
0Patent Application Number
144276640
Date Filed
March 14, 2013
0Patent Primary Examiner
Edits on 20 Jan, 2022
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US Patent 09970323 Geared turbofan engine with optimized diffuser case flange location
Infobox
Is a
Patent applicant
Patent jurisdiction
Patent number
09970323
Date of patent
May 15, 2018
Patent application number
14427664
Date Filed
March 14, 2013
Patent primary examiner
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