SYSTEM AND METHOD FOR RESIZING HOLES

The present application thus provides a method of filling an existing hole in a surface of a turbine component. The method may include the steps of enlarging the existing hole, placing a rivet into the enlarged hole, welding the rivet into place, and grinding the rivet to be flush with the surface o...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	ADEL LOAIE ATTIA, CONRAD CHRISTOPHER CARL, BAILEY DONALD MARK, SHUBERT GARY CHARLES
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The present application thus provides a method of filling an existing hole in a surface of a turbine component. The method may include the steps of enlarging the existing hole, placing a rivet into the enlarged hole, welding the rivet into place, and grinding the rivet to be flush with the surface of the turbine component. 本申请因此提供一种填充涡轮构件的表面中的现有孔的方法。该方法可包括以下步骤：扩大现有孔，将铆钉放置到扩大的孔中，将铆钉焊接就位，以及将铆钉磨削成与涡轮构件的表面齐平。