AIR OUTLET FOR A NACELLE FOR AN AIRCRAFT TURBOFAN COMPRISING A GUIDING DEVICE FOR SUPPORTING A REVERSE THRUST PHASE
An air outlet for a nacelle for an aircraft turbofan having an inner wall and an outer wall connected to each other by a trailing edge, at least one radial through aperture extending over an angular portion of the air outlet and having inner and outer open faces and, for each aperture, a guiding dev...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
18.01.2023
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Subjects | |
Online Access | Get full text |
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Summary: | An air outlet for a nacelle for an aircraft turbofan having an inner wall and an outer wall connected to each other by a trailing edge, at least one radial through aperture extending over an angular portion of the air outlet and having inner and outer open faces and, for each aperture, a guiding device having inner and outer movable members movably mounted between a closed position wherein the inner and outer movable members respectively close off the inner and outer open faces, the aperture defining a closed cavity and an open position wherein the inner and outer movable members are configured to allow an external air flow to circulate in the aperture to support a reverse thrust phase. |
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Bibliography: | Application Number: EP20210707749 |