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US Patent 12104530 Gas turbine engine

Patent 12104530 was granted and assigned to Rolls-Royce PLC on October, 2024 by the United States Patent and Trademark Office.

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
Rolls-Royce PLC
Rolls-Royce PLC
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Date Filed
September 8, 2022
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Date of Patent
October 1, 2024
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Patent Applicant
Rolls-Royce PLC
Rolls-Royce PLC
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Patent Application Number
17940035
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Patent Citations
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US Patent 10648475 Turbine engine
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US Patent 10690147 Compressor with segmented inner shroud for an axial turbine engine
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US Patent 10826343 High speed electric machine with radially supported rotor magnets
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US Patent 11597527 Aircraft hybrid propulsion fan drive gear system DC motors and generators
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US Patent 11077953 Electric ducted fan
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US Patent 7448199 Self powdered missile turbojet
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US Patent 7621117 Apparatus and method for controlling engine windmilling
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US Patent 10184401 Turbojet engine suspension using a double rear support
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US Patent 10308365 Fully integrated hybrid electric jet engine
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US Patent 10583932 Aero engine flow rate
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Patent Inventor Names
Benjamin J Sellers
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Jonathan A Cherry
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Craig Town
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
12104530
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Patent Primary Examiner
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Steven M Sutherland
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CPC Code
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F05D 2220/76
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F05D 2260/213
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F05D 2260/40
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F02C 3/06
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F02C 7/32
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F02C 7/12
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F02C 7/36
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F05D 2220/323
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