An aerofoil assembly in a gas turbine
Stator aerofoil for a gas turbine engine, comprising: a body portion (412); at least one panel (424) which forms at least part of one of either the pressure or suction surface of the aerofoil; at least one internal chamber (434) which is bounded by the body portion and panel; and, at least one elast...
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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
17.01.2018
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Subjects | |
Online Access | Get full text |
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Summary: | Stator aerofoil for a gas turbine engine, comprising:
a body portion (412); at least one panel (424) which forms at least part of one of either the pressure or suction surface of the aerofoil; at least one internal chamber (434) which is bounded by the body portion and panel; and, at least one elastomeric component (446) within the at least one internal chamber, wherein the elastomeric component at least partially defines a cell (450) within the internal chamber, wherein the cell is in fluid communication with the exterior of the aerofoil. |
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Bibliography: | Application Number: EP20120181298 |