Shroud leading edge cooling

Details Shroud leading edge cooling Shroud leading edge cooling

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01) F01D 5/18 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2528076

A cooling device includes a plurality of passages extending through outer platforms of turbine vane segments for directing cooling air in a choked flow condition towards a downstream turbine shroud.

Un dispositif de refroidissement comprend plusieurs passages se prolongeant dans des plates-formes extérieures de segments d'ailettes de turbine pour diriger l'air de refroidissement dans un état d'écoulement réduit vers une enveloppe de turbine en aval.

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