Multiform film cooling holes

Details Multiform film cooling holes Multiform film cooling holes

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/12 (2006.01) F01D 5/18 (2006.01) F01D 25/14 (2006.01) F02C 7/12 (2006.01)

Patent

CA 2526717

A turbine wall (18) includes a plurality of first and second film cooling holes (34,36) arranged in a common row. The holes (34,36) have multiple forms and alternate in the row for collectively providing film cooling performance therefrom.

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