Methods and apparatus for assembling turbine engines
A method facilitates the assembly of a gas turbine engine. The method comprises providing a turbine nozzle including an inner band, an outer band, and at least one vane extending between the inner and outer bands, wherein the vane includes a first sidewall and a second sidewall connected together at...
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Main Authors | , , , , |
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Format | Patent |
Language | English |
Published |
22.04.2008
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Subjects | |
Online Access | Get full text |
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