METHOD FOR CALIBRATING A GAS TURBINE BURNER DURING RECONDITION OR PRODUCTION BY USING A CALIBRATING PIN

A method for calibrating a gas turbine burner (12) during recondition or production; the method comprising the steps of:a) providing a gas turbine burner (12) provided with a plurality of holes (31) configured for injecting fuel gas in an airflow, each hole (31) comprising an outlet (39) having an i...

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Bibliographische Detailangaben
1. Verfasser:	MARLOW, Paul
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBINED OPERATIONS COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MACHINE TOOLS MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PERFORMING OPERATIONS TRANSPORTING UNIVERSAL MACHINE TOOLS WEAPONS
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Beschreibung
Zusammenfassung:	A method for calibrating a gas turbine burner (12) during recondition or production; the method comprising the steps of:a) providing a gas turbine burner (12) provided with a plurality of holes (31) configured for injecting fuel gas in an airflow, each hole (31) comprising an outlet (39) having an initial outlet diameter;b) deforming each hole outlet (39) using a calibrating device (34) configured so that the outlet is deformed reducing the initial outlet diameter to a smaller outlet diameter.