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US Patent 11230926 High cycle fatigue design for gas turbine engines

Patent 11230926 was granted and assigned to Rolls-Royce on January, 2022 by the United States Patent and Trademark Office.

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Patent abstractTimelineTable: Further ResourcesReferences
Is a
Patent
Patent

Patent attributes

Patent Applicant
‌
Rolls-Royce
Current Assignee
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Rolls-Royce
Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
Patent Number
11230926
Date of Patent
January 25, 2022
Patent Application Number
16707081
Date Filed
December 9, 2019
Patent Citations
‌
US Patent 10233758 Detuning trailing edge compound lean contour
Patent Primary Examiner
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Lawrence Averick
Patent abstract

Devices, systems, and methods for making gas turbine engine component with high cycle fatigue performance include selecting target airfoils while detuning other airfoils. The selective detuning can reduce resource intensity for realistic testing during build. Conforming detuning masses can reduce the need for outside resources.

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