Corrugated cowl for combustor of a gas turbine engine and method for configuring same
A cowl for use with a combustor of a gas turbine engine, the cowl includes a main body with an annular corrugation. A combustor of a gas turbine engine, the combustor includes: a hollow body defining a combustion chamber, the hollow body having a liner; an outer cowl having an annular corrugation, t...
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Main Authors | , , , , , |
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Format | Patent |
Language | English |
Published |
06.01.2004
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Edition | 7 |
Subjects | |
Online Access | Get full text |
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Summary: | A cowl for use with a combustor of a gas turbine engine, the cowl includes a main body with an annular corrugation. A combustor of a gas turbine engine, the combustor includes: a hollow body defining a combustion chamber, the hollow body having a liner; an outer cowl having an annular corrugation, the cowl connecting to the liner; and an inner cowl connecting to the liner. A method of configuring a cowl for a gas turbine engine combustor, the method includes forming an annular corrugation in a main body of the cowl. |
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Bibliography: | Application Number: US20020085767 |