Turbine engine fan case with tip injection air recirculation passage
A fan case assembly adapted for use with a gas turbine engine includes a fan track liner and an annular case. The fan track liner extends circumferentially at least partway about a central axis of the gas turbine engine. The annular case is configured to support the fan track liner at a radial posit...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
18.07.2023
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Subjects | |
Online Access | Get full text |
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Summary: | A fan case assembly adapted for use with a gas turbine engine includes a fan track liner and an annular case. The fan track liner extends circumferentially at least partway about a central axis of the gas turbine engine. The annular case is configured to support the fan track liner at a radial position relative to the central axis. The fan case assembly further includes an air recirculation duct configured to redirect air around the fan track liner. |
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Bibliography: | Application Number: US202117560227 |