Method of fabricating liquid cooled gas turbine components

Details Method of fabricating liquid cooled gas turbine components Method of fabricating liquid cooled gas turbine components

B - Operations, Transporting

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26/150

B23P 15/02 (2006.01) B21K 3/00 (2006.01) B23P 15/04 (2006.01) F01D 5/18 (2006.01) F01D 5/28 (2006.01)

Patent

CA 1101644

ABSTRACT OF THE DISCLOSURE A method of fabricating complex, composite components for water-cooled, high temperature gas turbines is provided. The method utilizes hot isostatic pressure with molten glass as a pressure transmitting medium. Metal tubing and cladding are bonding to a turbine bucket core under conditions such that the ends of the tubing extend above the molten glass whereby the pressure inside and outside of the tubing is maintained at equilibrium to prevent collapsing thereof during the application of hot isostatic pressure.

299919

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