초록 ▼

A damper bearing assembly for a gas turbine engine is disclosed. The damper bearing assembly is designed to define forward and aft axial gaps which allow for normal deflection under standard operating thrust loads, but then close during a fan blade out event to allow the increased load to transfer t

A damper bearing assembly for a gas turbine engine is disclosed. The damper bearing assembly is designed to define forward and aft axial gaps which allow for normal deflection under standard operating thrust loads, but then close during a fan blade out event to allow the increased load to transfer to the damper housing. Frictional forces between contacting parts limit torsional windup and increase torsional resistance with increasing load. The damper bearing assembly includes a damper housing configured substantially within a U-shaped spring finger housing and a spanner nut with a radial hook portion coupled to the spring finger housing. The damper housing is coupled to the spring finger housing such that it is substantially confined within the U-shaped void. The spanner nut is coupled to the spring finger housing such that the radial hook portion is configured to limit the deflection of the spring finger housing and damper housing during a fan blade out event.

대표청구항 ▼

1. A bearing assembly for a gas turbine engine, said assembly comprising: a spring finger housing comprising a first portion and a second portion, wherein said first portion is substantially perpendicular to said second portion;a damper housing including a radially inner platform comprising an aft f

1. A bearing assembly for a gas turbine engine, said assembly comprising: a spring finger housing comprising a first portion and a second portion, wherein said first portion is substantially perpendicular to said second portion;a damper housing including a radially inner platform comprising an aft face, a forward face, and a radially inner surface positioned therebetween, said damper housing coupled within said spring finger housing such that a first axial gap is defined between said forward face and said first portion; anda spanner nut coupled to a radially inner surface of the second portion, wherein said spanner nut includes a hook portion that defines a second axial gap between said aft face and said hook portion, and wherein said hook portion and said spring finger housing second portion define a radial gap therebetween. 2. The bearing assembly in accordance with claim 1, wherein said spring finger housing has a substantially U-shaped cross section. 3. The bearing assembly in accordance with claim 1, wherein said radial gap is contlgured to at least limit separation of said spanner nut and said spring finger housing. 4. The bearing assembly in accordance with claim 1 further comprising a bearing housing coupled to said spring finger housing adjacent said spanner nut. 5. The bearing assembly in accordance with claim 4 further comprising a bearing coupled to said bearing housing. 6. The bearing assembly in accordance with claim 1, wherein at least one of said spring finger housing, said damper housing, and said spanner nut is an annular ring. 7. The bearing assembly in accordance with claim 1, wherein said second portion of said spring finger housing and said radially inner surface of said damper platform define a radial clearance therebetween. 8. The bearing assembly in accordance with claim 1, wherein said first axial gap is configured to dose at a first point on said bearing assembly and said second gap is configured to dose at a second point on said bearing assembly, wherein said first and second axial gaps close simultaneously and said first point is opposite said second point on said annular bearing assembly. 9. A method of assembling a bearing assembly for a gas turbine engine, said method comprising: providing a spring finger housing that includes a first portion and a second portion, wherein the first portion is substantially perpendicular to the second portion;providing a damper housing including a radially inner platform that includes an aft face, a forward face, and a radially inner surface positioned therebetween;coupling the damper housing within the spring finger housing such that a first axial gap is defined between the forward face and the first portion;coupling a spanner nut to a radially inner surface of the second portion, wherein the spanner nut includes a hook portion that defines a second axial gap between the aft face and the hook portion; andsimultaneously closing the first axial gap at a first point on the bearing assembly and closing the second axial gap at a second point on the bearing assembly, wherein the first point is opposite the second point on the annular bearing assembly. 10. The method in accordance with claim 9, wherein the spring finger housing has a substantially U-shaped cross section. 11. The method in accordance with claim 9, wherein coupling a spanner nut to a radially inner surface of a second portion of the spring finger housing further comprises threadably coupling a spanner nut to a radially inner surface of a second portion of the spring finger housing. 12. The method in accordance with claim 9, wherein coupling a spanner nut to a radially inner surface of a second portion of the spring finger housing further comprises defining a radial gap between the spring finger housing second portion and the hook portion. 13. The method in accordance with claim 9 further comprising coupling a bearing housing to the spring finger housing adjacent the spanner nut. 14. A rotor assembly comprising: a rotor shaft; anda bearing assembly configured to support said rotor shaft, said bearing assembly comprising: a spring finger housing comprising a first portion and a second portion, wherein said first portion is substantially perpendicular to said second portion;a damper housing including a radially inner platform comprising an aft face, a forward face, and a radially inner surface positioned therebetween, wherein said damper housing coupled within said spring finger housing such that a first axial gap is defined between said forward face and the first portion;a spanner nut coupled to a radially inner surface of the second portion, wherein said spanner nut includes a hook portion that defines a second axial gap between said aft face and said hook portion; anda bearing housing coupled to said spring finger housing adjacent said spanner nut. 15. The rotor assembly in accordance with claim 14, wherein said spring finger housing has a substantially U-shaped cross section. 16. The rotor assembly in accordance with claim 14, wherein said hook portion and said spring finger housing second portion define a radial gap therebetween. 17. The rotor assembly in accordance with claim 14, wherein said first axial gap is configured to close at a first point on said bearing assembly and said second gap is configured to close at a second point on said bearing assembly, wherein said first and second axial gaps dose simultaneously and said first point is opposite said second point on annular bearing assembly.