Pressure activated seals for a gas turbine engine
An assembly for use in a gas turbine engine is disclosed. The assembly includes a first component arranged adjacent to a second component to form a gap therebetween and a pressure activated seal that resists flow through the gap.
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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
06.08.2019
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Subjects | |
Online Access | Get full text |
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Summary: | An assembly for use in a gas turbine engine is disclosed. The assembly includes a first component arranged adjacent to a second component to form a gap therebetween and a pressure activated seal that resists flow through the gap. |
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Bibliography: | Application Number: US201615159163 |