F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
F01D 25/14 (2006.01)
Patent
CA 2504165
A wall (32) in a gas turbine engine includes inner and outer surfaces (34,36) having a row of compound chevron film cooling holes (38) extending therethrough. The chevron holes (38) diverge both longitudinally and laterally between an inlet (40) at the wall inner surface (34) and a chevron outlet (42) at the wall outer surface (36).
Brassfield Steven Robert
Bunker Ronald Scott
Lee Ching-Pang
Company General Electric
Craig Wilson And Company
LandOfFree
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