Gas turbine sealing air supply system

Details Gas turbine sealing air supply system Gas turbine sealing air supply system

F - Mech Eng,Light,Heat,Weapons

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D

F01D 11/02 (2006.01) F01D 5/08 (2006.01) F01D 11/10 (2006.01) F02C 7/18 (2006.01) F02C 9/18 (2006.01)

Patent

CA 2498057

A sealing air bypass flow path is provided in a gas turbine for supplying sealing air to a sealing air supply flow path by bypassing the flow path between the tangential on board injection (TOBI) nozzles and seal disk holes.

Selon l'invention, un passage de dérivation d'air d'étanchéité est formé dans une turbine à gaz pour acheminer de l'air d'étanchéité dans un passage d'acheminement d'air d'étanchéité par dérivation du passage entre les tuyères à injection tangentielle de bord (TOBI) et des trous ménagés dans un disque d'étanchéité.

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