US Patent 11994039 Shroud for a gas turbine engine
Patent 11994039 was granted and assigned to General Electric on May, 2024 by the United States Patent and Trademark Office.
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US Patent 11994039 Shroud for a gas turbine engine
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Patent abstract
A gas turbine engine having a rotor blade stage with a plurality of circumferentially spaced rotors, a nozzle stage adjacent the rotor blade stage and including an outer nozzle end, at least one stop, and a shroud. The shroud having a forward end positioned radially outward from the circumferentially spaced rotor blades, and an aft end axially aft of the forward end. The at least one stop confronting at least a portion of the outer nozzle end.
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Patent Applicant
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
Charles William Craig, III0
Kirk Douglas Gallier0
Date of Patent
May 28, 2024
0Patent Application Number
177114050
Date Filed
April 1, 2022
0Patent Citations
Patent Primary Examiner
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