GAS TURBINE PROVIDED WITH VALVE COOLING SYSTEM

PROBLEM TO BE SOLVED: To provide a method of cooling one or a plurality of valves in a gas turbine engine, and the gas turbine engine using the method.SOLUTION: A gas turbine engine 100 may include: an air extraction system 110 of a compressor 15 provided with a number of valves; an exhaust frame co...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	AMPILI KISHORE KUMAR, SRINIVAS AVISHETTI, ANIL KUMAR DASOJI, MERCHANT LAXMIKANT
Format:	Patent
Sprache:	eng ; jpn
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
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a method of cooling one or a plurality of valves in a gas turbine engine, and the gas turbine engine using the method.SOLUTION: A gas turbine engine 100 may include: an air extraction system 110 of a compressor 15 provided with a number of valves; an exhaust frame cooling system 310 provided with an exhaust frame blower 330; and a turbine valve cooling system 350 provided with one or a plurality of valve protection boxes 360 surrounding one or a plurality of the valves. One or the plurality of valve protection boxes 360 communicate with flow of air from the exhaust frame blower 330.SELECTED DRAWING: Figure 2 【課題】ガスタービンエンジン内の１つまたは複数のバルブを冷却する方法およびその方法を用いたガスタービンエンジンを提供する。【解決手段】ガスタービンエンジン１００は、いくつかのバルブを備えたコンプレッサー１５の空気抽出システム１１０と、エキゾーストフレームブロワー３３０を備えたエキゾーストフレーム冷却システム３１０と、１つまたは複数のバルブを囲む１つまたは複数のバルブ保護箱３６０を備えたタービンのバルブ冷却システム３５０とを含んでよく、バルブ保護箱３６０は、エキゾーストフレームブロワー３３０からの空気の流れを連通している。【選択図】図２