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Gas turbine with a spacer member and a turbine rotor disk defining an air cooling passage
Gas turbine with a spacer member and a turbine rotor disk defining an air cooling passage
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机译:具有间隔件和限定空气冷却通道的涡轮转子盘的燃气轮机
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摘要
In a gas turbine, in which a compressor (15) and a turbine (16) are connected by means of a distant piece (7,107), the distant piece and a turbine first-stagedisk (1,101) are connected by means of a joint portion. On the distant piece is formed a projection portion, and a spacer (8,108) is held by means of a spigot portion (7d,8d). Thin portion (8b) is formed on an outer diameter side of the spacer, and is in contact with a fin (13) of a turbine disk through a seal member (14). The turbine disk, the distant piece and the spacer define a cavity (8a,108a).
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