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US Patent 11668235 Turbofan gas turbine engine

OverviewStructured DataIssuesContributorsActivity
Is a
Patent
Patent
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Current Assignee
Rolls-Royce
Rolls-Royce
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Date Filed
September 24, 2021
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Date of Patent
June 6, 2023
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Patent Applicant
Rolls-Royce
Rolls-Royce
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Patent Application Number
17484096
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Patent Citations
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US Patent 10378554 Gas turbine engine with partial inlet vane
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US Patent 10378556 Outlet guide vane for aircraft turbine engine, presenting an improved lubricant cooling function
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US Patent 11118601 Gas turbine engine with partial inlet vane
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US Patent 11015468 Outlet guide vane for turbomachine, comprising a lubricant cooling passage equipped with a thermal conducting matrix compressed between the intrados and extrados walls
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US Patent 7811050 Operating line control of a compression system with flow recirculation
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US Patent 8579584 Turbofan jet engine
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US Patent 9765694 Gas turbine engine heat exchangers and methods of assembling the same
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US Patent 9777963 Method and system for radial tubular heat exchangers
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US Patent 10215096 Engine with nose cone heat exchanger and radially outer discharge
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
11668235
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Patent Primary Examiner
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Alain Chau
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CPC Code
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F02C 7/14
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F02C 7/141
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F02K 3/04
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F02K 3/06
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F02K 3/072
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F02C 7/08
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F02K 3/105
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F02K 3/115
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B64D 2033/0233
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B64D 2033/0286
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