Extended housing sleeve with stiffening ring feature
A sleeve for a bearing damper comprising a cylinder shaped body having a forward end opposite an aft end, the body including an interior surface opposite an exterior surface, the body configured insertable between a bearing proximate the interior surface and a housing proximate the exterior surface; a ring portion proximate the forward end, the ring portion having an outer diameter larger than a diameter of the body; and an extension portion configured to provide an active damper surface extending beyond the housing.
1. A gas turbine bearing assembly comprising:
a housing bore proximate a bearing having an oil damper including a damper stop surface that extends beyond the support of said housing bore, said bearing supporting a shaft;
a sleeve having a cylinder shaped body having a forward end opposite an aft end, said body including an interior surface opposite an exterior surface, said body configured insertable between said bearing proximate said interior surface and said housing bore proximate said exterior surface; said sleeve including a ring portion proximate said forward end, said ring portion having an outer diameter larger than a diameter of said body, wherein said ring portion comprises a thickened cross-section that has a greater thickness than the remainder of the cylinder shaped body of the ring portion configured to stiffen said sleeve proximate said extension portion; and
an extension portion configured to support a damper stop surface extending beyond and being unsupported by said housing bore proximate to the sleeve; said extension portion configured to support the damper stop surface that extends beyond said housing bore, and an active damper surface configured to support a damper film length from 5 percent to 15 percent of an outer diameter of the bearing damper.
2. The gas turbine bearing assembly according to claim 1 , wherein said extension portion provides a sleeve length longer than the housing bore length.
3. The gas turbine bearing assembly according to claim 1 , further comprising:
a seal receiver formed in said interior surface proximate said ring portion at said forward end.
4. The gas turbine bearing assembly according to claim 3 , wherein said seal receiver is configured as a chamfer.
5. The gas turbine bearing assembly according to claim 1 , wherein said ring portion includes a geometry that provides added stiffness to the body, said added stiffness including mechanical properties, configured to prevent thermal or mechanical distortion of the sleeve.
6. A process for creating an active damper surface extending beyond a housing bore comprising:
inserting a sleeve between the housing and a bearing mounted within said housing bore, said bearing including a damper stop surface that extends beyond the support of said housing bore and is unsupported by the housing bore;
said sleeve having a cylinder shaped body having a forward end opposite an aft end, said body including an interior surface opposite an exterior surface, said body configured insertable between said bearing proximate said interior surface and said housing bore proximate said exterior surface; said sleeve including a ring portion proximate said forward end, said ring portion having an outer diameter larger than a diameter of said body; and
an extension portion configured to support a damper stop surface extending beyond said housing bore proximate to the sleeve; said extension portion configured to support the damper stop surface that extends beyond said housing bore, and an active damper surface configured to support a damper film length from 5 percent to 15 percent of an outer diameter of the bearing damper.
7. The process of claim 6 , wherein said extension portion provides a sleeve length longer than the housing bore length.
8. The process of claim 6 , wherein said sleeve comprises said active damper surface between O-rings, said active damper surface enables an extended interface length of a damper coupled to said bearing proximate said housing bore.
9. The process of claim 6 , wherein said ring portion includes cross section that has a greater thickness than the remainder of the body.
10. The process of claim 6 , further comprising:
a seal receiver formed in said interior surface proximate said ring portion at said forward end.
11. The process of claim 6 , wherein said ring portion includes a geometry that provides added stiffness to the body, said added stiffness including mechanical properties, configured to prevent thermal or mechanical distortion of the sleeve.
12. The process of claim 11 , further comprising:
a feature formed in said body between the forward end and the aft end, said feature comprising at least one of an anti-rotation feature, and a clocking feature.