F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
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 2555395
A method for assembling a gas turbine engine (10) includes coupling a rotor assembly (33) including a plurality of rotor blades (34) about a rotatable main shaft (24) of the gas turbine engine. The main shaft is aligned in an axial direction (25) of the gas turbine engine. A shroud assembly (50) is coupled to the gas turbine engine. The shroud assembly includes a plurality of shroud segments (60) circumferentially coupled about the rotor assembly such that a shroud spacing gap (62) is formed in the axial direction (83) between adjacent shroud segments. A cooling fluid source is coupled to each shroud segment such that cooling fluid is channeled through each shroud segment into a corresponding shroud spacing gap to facilitate positive purge flow through the shroud spacing gap.
Demers Daniel
Hooper Tyler F.
Nicoll Robert Alexander
Probasco Douglas Patrick
Shapiro Jason David
Company General Electric
Craig Wilson And Company
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