INSERT REMOVAL DEVICE FOR GAS TURBINE STATIONARY BLADE AND INSERT REMOVAL METHOD FOR GAS TURBINE STATIONARY BLADE

An insert removal device (20) for a gas tourbine stationary blade, which removes weld metal which surrounds an insert collar so as to connect the insert collar protruding outwardly from the outer peripheral surfaces of inserts to a stationary blade outside shroud non-gas path surface by arc-discharg...

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Bibliographische Detailangaben
Hauptverfasser:	TSUKIMOTO KOJI, TAKEUCHI YASUSHI, OSAME YUKI
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	An insert removal device (20) for a gas tourbine stationary blade, which removes weld metal which surrounds an insert collar so as to connect the insert collar protruding outwardly from the outer peripheral surfaces of inserts to a stationary blade outside shroud non-gas path surface by arc-discharge which is repeated in a short period between an electrode (21) and the gas turbine stationary blade, wherein the bottom surface (24) of the electrode (21) has the same planar view shape as the planar view shape of the weld metal.