US Patent 10458247 Stator of an aircraft turbine engine
Patent 10458247 was granted and assigned to Safran on October, 2019 by the United States Patent and Trademark Office.
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Patent abstract
A stator of an aircraft turbine engine, comprising an annular row of fixed vanes and an annular row of arms, wherein the trailing edges of the fixed vanes are positioned substantially in a first transverse plane that is positioned downstream of a second transverse plane that passes substantially through the leading edges of the arms.
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Patent Inventor Names
Matthieu Yoann Perrier0
Simon Pierre Claude Charbonnier0
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
104582470
Date of Patent
October 29, 2019
0Patent Application Number
155170960
Date Filed
September 29, 2015
0Patent Primary Examiner
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US Patent 10458247 Stator of an aircraft turbine engine
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
10458247
Date of patent
October 29, 2019
Patent application number
15517096
Date Filed
September 29, 2015
Patent primary examiner
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