Bearing assembly and method of assembling the same

Details Bearing assembly and method of assembling the same Bearing assembly and method of assembling the same

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/06 (2006.01) F16C 41/00 (2006.01) F16C 43/02 (2006.01)

Patent

CA 2613770

A gas turbine engine assembly is provided. The gas turbine assembly includes a compressor rotor (314), a compressor stator (312) coupled upstream from the compressor rotor, a bearing assembly (300) coupled between the compressor rotor and the compressor stator for supporting the compressor rotor. The bearing assembly includes a pair of foil thrust bearings (334,336) coupled to a portion of the compressor stator, and a pair of spring packs (338,340) coupled substantially co-axially to the pair of foil thrust bearings, and a second bearing assembly (400) coupled downstream from the bearing assembly, the second bearing assembly includes a radial foil bearing (356).

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