ELEMENT OR BLADE OF FLUID OPERATION FOR TURBO MACHINE
PURPOSE: An element or blade of fluid operation for a turbo machine is provided to enable to practice inspection and repair after production with precision and reliability obtained at first production process. CONSTITUTION: A turbine blade (18) for a gas turbine engine includes a machining datum and...
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Main Authors | , |
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Format | Patent |
Language | English Korean |
Published |
15.03.2001
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Edition | 7 |
Subjects | |
Online Access | Get full text |
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Summary: | PURPOSE: An element or blade of fluid operation for a turbo machine is provided to enable to practice inspection and repair after production with precision and reliability obtained at first production process. CONSTITUTION: A turbine blade (18) for a gas turbine engine includes a machining datum and support tool interface (52). The datum and interface feature is a frustoconical depression residing in a blade outer shroud (36) and ideally aligned with an airfoil stacking line (40). The blade has a prefinished state in which the depression has a prefinished depth (d1) and a finished state in which the depression has a finished depth (d2). The finished depth (d2) is smaller than the prefinished depth (d1), but is nevertheless sufficient to act as a support feature during manufacturing operations. The utility of the depression, as both a datum and as a support feature, survives the original manufacturing operations so that the depression is useful for post-manufacturing inspection and repair. |
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Bibliography: | Application Number: KR20000046870 |