US Patent 11111816 Rotor blade arrangement
Patent 11111816 was granted and assigned to Rolls-Royce PLC on September, 2021 by the United States Patent and Trademark Office.
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Patent abstract
The blades for a rotor of a gas turbine engine are all manufactured to the same design. However, manufacturing tolerances mean that in practice each individual blade is different to the others. It is proposed to arrange the blades around the circumference of the rotor in a manner that limits excessive stress being induced in the blades due to differences in the vibration response between a given blade and its two neighbouring blades.
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Patent Inventor Names
Bharat M. Lad0
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Official Website
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Patent Number
111118160
Date of Patent
September 7, 2021
0Patent Application Number
201905100
Date Filed
May 10, 2019
0Official Website
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US Patent 11111816 Rotor blade arrangement
Infobox
Is a
Patent applicant
Current assignee
Patent jurisdiction
Patent number
11111816
Date of patent
September 7, 2021
Patent application number
20190510
Date Filed
May 10, 2019
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