Flow outlet device at turbine end of gas turbine

The invention discloses a gas turbine end outflow device which comprises a first pipe section, a second pipe section and a third pipe section which are sequentially sleeved from inside to outside and arranged at intervals, a first cavity is formed between the first pipe section and the second pipe s...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	HUANG DAN, SHEN GUOHUA, HU LONGBING, SHI SHI
Format:	Patent
Sprache:	chi ; 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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The invention discloses a gas turbine end outflow device which comprises a first pipe section, a second pipe section and a third pipe section which are sequentially sleeved from inside to outside and arranged at intervals, a first cavity is formed between the first pipe section and the second pipe section, and a second cavity is formed between the second pipe section and the third pipe section. The first pipe section is provided with a first cavity and a second cavity, cooling gas is arranged in the first cavity and the second cavity, the first pipe section is provided with a channel, the channel is suitable for introducing high-temperature exhaust gas, the cooling gas is used for exchanging heat with the high-temperature exhaust gas, the cooling gas in the first cavity and the cooling gas in the second cavity can circulate, the third pipe section is provided with a third cavity, and cooling water is arranged in the third cavity. And the cooling water is used for exchanging heat with high-temperature exhaust.