Steam cooling a turbine rotor

An axial bore tube assembly (48) for a turbine is provided to supply cooling steam to hot gas components of the turbine wheels and return the spent cooling steam. A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward en...

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Hauptverfasser: WILSON, IAN DAVID, DESTEFANO, THOMAS DANIEL
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Sprache:eng ; fre ; ger
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DESTEFANO, THOMAS DANIEL
description An axial bore tube assembly (48) for a turbine is provided to supply cooling steam to hot gas components of the turbine wheels and return the spent cooling steam. A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward ends of the tubes communicate with an end cap assembly (80) having sets of peripheral holes (88) communicating with first and second sets of radial tubes (92) whereby cooling steam from the concentric passage (54) is supplied through the end cap holes (88) to radial tubes (93) for cooling the buckets and return steam from the buckets is provided through the second set of radial tubes (95) through a second set of openings (90) of the end cap (80) into the coaxial return passage (56). A radial-to-axial flow transitioning device, including anti-swirling vanes (112), is provided in the end cap (81). A strut ring adjacent the aft end of the bore tube assembly permits axial and radial thermal expansion of the inner tube (52) relative to the outer tube (50).
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A pair of inner and outer tubes (52, 50) define a steam supply passage (54) concentric about an inner return passage (56). The forward ends of the tubes communicate with an end cap assembly (80) having sets of peripheral holes (88) communicating with first and second sets of radial tubes (92) whereby cooling steam from the concentric passage (54) is supplied through the end cap holes (88) to radial tubes (93) for cooling the buckets and return steam from the buckets is provided through the second set of radial tubes (95) through a second set of openings (90) of the end cap (80) into the coaxial return passage (56). A radial-to-axial flow transitioning device, including anti-swirling vanes (112), is provided in the end cap (81). 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language eng ; fre ; ger
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subjects 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
title Steam cooling a turbine rotor
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