GAS TURBINE

PROBLEM TO BE SOLVED: To provide a gas turbine which inhibits heat stress applied to an exhaust air duct.SOLUTION: A gas turbine includes: a cylindrical exhaust air duct 31 where an exhaust air passage 35 for circulating an exhaust gas G is formed; a first reinforcement rib 41 which is provided alon...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	TAKESHITA NAOYA, AOTA TOYOMASA, KATO EIGO, KADOWAKI TOMOHIKO, KUROSAKI HIKARU, KATAYAMA HIROYUKI
Format:	Patent
Sprache:	eng
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:	PROBLEM TO BE SOLVED: To provide a gas turbine which inhibits heat stress applied to an exhaust air duct.SOLUTION: A gas turbine includes: a cylindrical exhaust air duct 31 where an exhaust air passage 35 for circulating an exhaust gas G is formed; a first reinforcement rib 41 which is provided along an outer periphery of the exhaust air duct 31; a space D which is formed contacting with the first reinforcement rib 41; an inflow pipe 51 which allows the exhaust air passage 35 to communicate with the space D and flows the exhaust gas G circulating in the exhaust air passage 35 into the space D; and an outflow pipe 52 which allows the exhaust air passage 35 to communicate with the space D and flows out the exhaust gas G in the space D into the exhaust air passage 35.