PRESSURE SENSOR ASSEMBLY FOR A TURBINE ENGINE
A gas turbine engine includes a liner positioned within a compressor section or a turbine section of the gas turbine engine and at least partially defining a core air flowpath through the gas turbine engine. The gas turbine engine also includes a casing at least partially enclosing the liner. Additi...
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Main Authors | , , , , , , |
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Format | Patent |
Language | English French |
Published |
16.08.2018
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Subjects | |
Online Access | Get full text |
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