CASING ARRANGEMENT
A fan casing arrangement for a gas turbine engine, the arrangement comprising an annular casing member and a fan track liner provided radially inward of the casing member and connected thereto. A forward portion of a gas washed surface of the fan track liner is curved so as to define a concave porti...
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Main Authors | , , , |
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Format | Patent |
Language | English |
Published |
13.07.2017
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Subjects | |
Online Access | Get full text |
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Summary: | A fan casing arrangement for a gas turbine engine, the arrangement comprising an annular casing member and a fan track liner provided radially inward of the casing member and connected thereto. A forward portion of a gas washed surface of the fan track liner is curved so as to define a concave portion of the gas washed surface (e.g. curved such that the radial position of said forward portion of the gas washed surface varies in an axial direction). |
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Bibliography: | Application Number: US201615383185 |