WASHER WITH COOLING PASSAGE FOR A TURBINE ENGINE COMBUSTOR
A washer for a turbine engine combustor comprises a first surface, a second surface facing generally opposite from the first surface, a bore communicating through the first and second surfaces, and a cooling passage separate from the bore and communicating through the first and second surfaces.
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
20.01.2011
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Subjects | |
Online Access | Get full text |
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Summary: | A washer for a turbine engine combustor comprises a first surface, a second surface facing generally opposite from the first surface, a bore communicating through the first and second surfaces, and a cooling passage separate from the bore and communicating through the first and second surfaces. |
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Bibliography: | Application Number: US20090505025 |