GAS TURBINE

A gas turbine includes a compressor, a combustor, an air lead-out member, an outer peripheral cover portion, and an auxiliary device member. The outer peripheral cover portion includes outer peripheral concave portions and outer peripheral convex portions, and is formed in a manner so that the outer...

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Bibliographische Detailangaben
Hauptverfasser:	Kudo, Takuma, Kamoi, Yasuharu
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:	A gas turbine includes a compressor, a combustor, an air lead-out member, an outer peripheral cover portion, and an auxiliary device member. The outer peripheral cover portion includes outer peripheral concave portions and outer peripheral convex portions, and is formed in a manner so that the outer peripheral concave portions recessed radially inward of the combustor so as to enter between mutually-adjacent combustion cylinders among the plurality of combustion cylinders and the outer peripheral convex portions protruding radially outward of the combustor so as to extend along outer peripheral surfaces of the plurality of combustion cylinders are alternately and continuously arranged in a circumferential direction of the combustor. The auxiliary device member is attached to one of the outer peripheral concave portions.