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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
Patent
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Patent attributes

Patent Applicant
Rolls-Royce PLC
Rolls-Royce PLC
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Current Assignee
Rolls-Royce PLC
Rolls-Royce PLC
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
111118160
Patent Inventor Names
Bharat M. Lad0
Date of Patent
September 7, 2021
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Patent Application Number
201905100
Date Filed
May 10, 2019
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Patent Citations Received
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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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