Joint structure of coolant passage, tube seal and gas turbine

Details Joint structure of coolant passage, tube seal and gas turbine Joint structure of coolant passage, tube seal and gas turbine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/12 (2006.01) F01D 5/08 (2006.01) F01D 5/18 (2006.01)

Patent

CA 2401945

A tube seal is fitted with a spherical spring, being an elastic member, at one end of a tubular barrel . The end where the spring is fitted to the tubular barrel is inserted into a steam supply pipe outlet, which is a coolant passage provided in a rotor disk. The other end of the barrel is formed into a spherical shape, and this end is inserted into a steam supply port in a dynamic blade, being another coolant passage port, and abuts against the internal surface of the steam supply port.

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