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US Patent 11668246 Gas turbine engine

Patent 11668246 was granted and assigned to Rolls-Royce on June, 2023 by the United States Patent and Trademark Office.

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Patent Applicant

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Current Assignee

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Patent Jurisdiction

United States Patent and Trademark Office

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Patent Number

Date of Patent

June 6, 2023

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Patent Application Number

172099890

Date Filed

March 23, 2021

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Patent Citations

US Patent 10794289 Modulated turbine component cooling

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US Patent 8262345 Ceramic matrix composite turbine engine

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US Patent 10794286 Method and system for modulated turbine cooling as a function of engine health

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US Patent 10989112 Gas turbine engine

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Patent Citations Received

US Patent 12110830 Gas turbine engine

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Patent Primary Examiner

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A highly efficient gas turbine engine is provided. The fan of the gas turbine engine is driven from a turbine via a gearbox, such that the fan has a lower rotational speed than the driving turbine, thereby providing efficiency gains. The efficient fan system is mated to a core that has low cooling flow requirements and/or high temperature capability, and which may have particularly low mass for a given power.

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