Gas turbine and turbine rotor for a gas turbine

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 7114915
APP PUB NO 20030133786A1
SERIAL NO

10339293

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A refrigerant supplied from a refrigerant supply pipe flows into a first space, being a passage of the refrigerant, from a space between first stage and second stage rotor disks. The refrigerant supplied to the first space is guided to second, third and forth spaces through a gap between a spindle bolt and a bolt hole, during which the rotor disks are warmed up or cooled. In the second stage rotor disk, a refrigerant through hole axially penetrating this rotor disk is provided near the center thereof. The refrigerant flowing into the first space passes through the refrigerant through hole to flow into the second space, to thereby promote the convection in the first, second, third and fourth spaces and equalization of temperatures in the rotor disks.

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Patent Owner(s)

Patent OwnerAddress
MITSUBISHI HEAVY INDUSTRIES LTDTOKYO 100-8332

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Hirokawa, Kazuharu Hyogo-ken, JP 29 242
Uematsu, Kazuo Hyogo-ken, JP 50 602

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