US Patent 10450879 Gas turbine engine
Patent 10450879 was granted and assigned to Rolls-Royce on October, 2019 by the United States Patent and Trademark Office.
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Patent abstract
A gas turbine engine includes a circumferential row of vanes directly upstream of an asymmetric gas flow path. At a given spanwise position, a tangential and axial position of the outer guide vanes varies along the circumferential row of vanes. One or more of the vanes are leant such that the tangential and axial position of one or more vanes of the circumferential row of vanes varies in a spanwise direction.
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Patent Inventor Names
Fernando Barbarossa0
Luca Di Mare0
Max E. Rife0
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Official Website
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
104508790
Date of Patent
October 22, 2019
0Patent Application Number
153419410
Date Filed
November 2, 2016
0Official Website
Patent Citations
Patent Primary Examiner
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US Patent 10450879 Gas turbine engine
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
10450879
Date of patent
October 22, 2019
Patent application number
15341941
Date Filed
November 2, 2016
Patent citations
Patent primary examiner
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