Low Leakage Multi-Directional Interface for a Gas Turbine Engine
An interface within a gas turbine engine includes a multiple of segmented components, each with a segment flange with a multiple of apertures, at least one of the multiple of apertures a first slot aperture. A full ring component with a ring flange that defines a multiple ring of apertures, at least...
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Main Authors | , , , , , , , |
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Format | Patent |
Language | English |
Published |
14.01.2016
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Subjects | |
Online Access | Get full text |
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Summary: | An interface within a gas turbine engine includes a multiple of segmented components, each with a segment flange with a multiple of apertures, at least one of the multiple of apertures a first slot aperture. A full ring component with a ring flange that defines a multiple ring of apertures, at least one of the multiple of ring apertures a second slot aperture, the second slot aperture transverse to the first slot aperture. |
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Bibliography: | Application Number: US201414766469 |