A fixed vane of a turbo molecular pump suitable for reducing damage to the fixed vane.
The variable vane assembly includes a vane operable to pivot about a pivot axis.
The two scrolls (22) forming air inlet slot (20) are each formed of a fixed vane (36) and a floating vane (38).
Thus, the side clearance of the stator vane in the stator vane-type turbocharger can be removed.
Provided is a stator vane-type turbocharger wherein a stator vane (15) is provided in a passage (9) between a bearing housing (1) as a first member and a turbine housing (4) as a second member.
In order to reduce a secondary flow loss thereby to improve a turbine efficiency, a portion, as positioned on the outer side of a boundary portion (28), of a stator blade (21) are bent in the revolving direction of a rotor.
A stationary blade and a steam turbine which can control self-excited vibration through a simple configuration.
The disclosed gas turbine has a turbine stationary blade (1) provided with a cooling mechanism which can effectively cool at a low required air flow rate.
Stationary blade of a gas turbine capable of effective cooling in a state, in which a low-pressure cooling air eases a pressure withstanding strength and with a simple construction.
The invention relates to a turbine (1) and a method for dismantling a blade (12) of a turbine.
The system includes an internally cooled stationary vane (12) located in a path of a working gas of the turbine.
The variable vane assembly also includes a labyrinth seal positioned between the bushing and the button portion.
The variable vane assembly also includes a bushing encircling the stem portion and abutting the button portion.
The main rotor can include an interior cavity and a fixed vane (or blade) that is attached to the peripheral and side walls of that cavity.
The invention also relates to an arrangement.
A gas turbine stationary vane having an airfoil portion and inner (36) and outer (38) shrouds.
A stationary vane assembly (5) for a turbo-machine in which the vane (5) is restrained against motion in the circumferential direction by first (26) and second (19) locking pins.
A stationary guide vane includes a top platform, a bottom platform, and a vane body located between the top platform and the bottom platform.
This cooling system branches into a first branch (18) via which the combustion chamber (2) and the first stages, particularly the first guide vane of the turbine (3) are cooled.
Requêtes fréquentes français :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Requêtes fréquentes anglais :1-200, -1k, -2k, -3k, -4k, -5k, -7k, -10k, -20k, -40k, -100k, -200k, -500k, -1000k,
Traduction Translation Traducción Übersetzung Tradução Traduzione Traducere Vertaling Tłumaczenie Mετάφραση Oversættelse Översättning Käännös Aistriúchán Traduzzjoni Prevajanje Vertimas Tõlge Preklad Fordítás Tulkojumi Превод Překlad Prijevod 翻訳 번역 翻译 Перевод