SEGMENT CONTROL DEVICE TURBINE INCLUDING THE SAME

The present invention relates to a turbo machine and a gas turbine including the same. The turbo machine according to one aspect of the invention comprises: a stator having a plurality of fixed vanes; and a rotor disposed between the vanes and having a plurality of rotating blades. A first flange pr...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	CHO GEON HWAN, GOO BON HAN, JU SUNG JONG, SONG SUNG JIN
Format:	Patent
Sprache:	eng ; kor
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:	The present invention relates to a turbo machine and a gas turbine including the same. The turbo machine according to one aspect of the invention comprises: a stator having a plurality of fixed vanes; and a rotor disposed between the vanes and having a plurality of rotating blades. A first flange protruding toward the stator is formed on the rotor. The stator is formed with a second flange which protrudes toward the rotor and faces the first flange. On the surface of the first flange facing the second flange, a pressure adjusting protrusion may be formed to protrude to adjust a pressure of a cooling air between the first flange and the second flange. Provided are the turbo machine capable of stably sealing between the rotor and the stator, and the gas turbine including the same. 본 발명의 일 측면에 따른 터보 머신은 고정된 복수의 베인들을 갖는 스테이터와 상기 베인들 사이에 배치되며 회전하는 복수의 블레이드들을 갖는 로터를 포함하며, 상기 로터에는 상기 스테이터를 향하여 돌출된 제1 플랜지가 형성되고, 상기 스테이터에는 상기 로터를 향하여 돌출되되 상기 제1 플랜지와 마주하는 제2 플랜지가 형성되며, 상기 제1 플랜지에서 상기 제2 플랜지를 마주하는 면에는 제1 플랜지와 제2 플랜지 사이에서 냉각 공기의 압력을 조절하는 압력조절 돌기가 돌출 형성될 수 있다.