METHOD for ASSEMBLING A GAS TURBINE ENCLOSURE

The invention relates to a method for assembling a gas turbine enclosure. Provided is a method for assembling the enclosure of a gas turbine (10). The method comprises arranging gas turbine equipment (23, 33, 43, 53) in an internal (22, 32, 42, 52) of a frame (21, 31, 41, 51) at a first location (1)...

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Bibliographische Detailangaben
Hauptverfasser:	RONALD LAWRENCE YENSER, DANIEL NEAL ALVAREZ, MATTHEW JOHN CANHAM, KYLE JOSEPH CONGER
Format:	Patent
Sprache:	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 invention relates to a method for assembling a gas turbine enclosure. Provided is a method for assembling the enclosure of a gas turbine (10). The method comprises arranging gas turbine equipment (23, 33, 43, 53) in an internal (22, 32, 42, 52) of a frame (21, 31, 41, 51) at a first location (1) (Operation (200)), connecting wall panels (24, 34, 44, 54) to the frame to form a pre-assembled module (20, 30, 40, 50) at the first location (1) (operation (201)), transporting the preassembled module from the first location (1) to a second location (2) (operation (202)) and placing the pre-assembled module close to the gas turbine such that the gas turbine equipment is exposure to be connected to the gas turbine, and forming a part of the outer enclosure (60) of the gas turbine and the gas turbine equipment by part of the wall panels (operation (203)).