Method and fixture for manufacturing components

A fixture (200) for positioning a gas turbine engine (10) component is provided. A fixture (200) includes, a stationary portion (204) including at least one stationary datum locator (208, 210) extending outward from the stationary portion. A fixture (200) further includes a movable portion (206) inc...

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Bibliographische Detailangaben
Hauptverfasser: GRAHAM, MICHAEL EVANS, GABRIEL, THOMAS ANDREW, RAMAMURTHY, RAJESH, BEZDECNY, MICHELLE RENE, ASH, CLARENCE ALBERT
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Zusammenfassung:A fixture (200) for positioning a gas turbine engine (10) component is provided. A fixture (200) includes, a stationary portion (204) including at least one stationary datum locator (208, 210) extending outward from the stationary portion. A fixture (200) further includes a movable portion (206) including at least one movable datum locator extending from the movable portion, the at least one movable datum locator is substantially parallel to the at least one stationary datum locator, the movable portion is movable in a direction away from the stationary portion.