Loaded bearing system

1. A bearing system for supporting an engine shaft, the bearing system comprising:

a bearing including:

an inner race extending circumferentially about an axis, the inner race having an interior sized to be coupled to the engine shaft;

a series of rolling elements disposed circumferentially about the axis and around the inner race; and

an outer race extending circumferentially about the axis and around the series of rolling elements;

a flange projecting radially outward of the outer race;

a housing having a housing cavity about the axis, the bearing received by the housing cavity, the housing cavity circumferentially circumscribed by a radially inner housing surface, the outer race of the bearing sealingly engaged with the radially inner housing surface, a piston chamber located radially outward of the radially inner housing surface, the piston chamber defined circumferentially by an outer piston chamber surface and axially by an axial piston chamber surface, the axial piston chamber surface defining an axial location relative to the axis, the flange extending radially outwardly beyond the radially inner housing surface to inside the piston chamber, the flange carrying a seal at a radially outer circumference thereof, the seal in sealing engagement with the outer piston chamber surface;

a first axial loading structure disposed in the housing cavity and operatively connected to the bearing, the first axial loading structure including a piston head formed by the flange of the outer race; and

a second axial loading structure disposed in the piston chamber, the second axial loading structure in axial abutment against the axial piston chamber surface and extending axially away from the axial location in a first axial direction, the second loading structure opposing axial movement of the bearing relative to the axial location in a second axial direction opposite the first axial direction when the bearing axially loads the second axial loading structure in the second axial direction, the first and the second axial loading structures being operationally independent from one another; and

a spacer in axial abutment between the second axial loading structure and the flange of the outer race, the spacer having an outer diameter surface in sliding contact with the outer piston chamber surface.

2. The bearing system of claim 1 , wherein the housing defines an oil orifice in fluid communication with inside the piston chamber, and the oil orifice and the second axial loading structure are located on a same side of the piston head.

3. The bearing system of claim 1 , wherein the housing defines an oil orifice in fluid communication with inside the piston chamber, and the bearing system includes at least one of a valve and a restrictor in fluid communication with the piston chamber via the oil orifice.

4. The bearing system of claim 1 , wherein the second axial loading structure is at least one of a wave spring, a disc spring, an elastomeric piece and a resilient structure defined by the housing.

5. The bearing system of claim 1 , wherein the piston chamber is defined by an annular groove of the housing extending circumferentially about the axis, the second axial loading structure including a spring received by the annular groove, the flange disposed axially outside of the annular groove, the spacer having a portion axially overlapping the annular groove and the spring.

6. A bearing system for supporting an engine shaft, the bearing system comprising:

a bearing including:

an inner race extending circumferentially about an axis, the inner race having an interior sized to be coupled to the engine shaft;

a series of rolling elements disposed circumferentially about the axis and around the inner race;

an outer race extending circumferentially about the axis and around the series of rolling elements; and

a flange projecting radially outward of the outer race;

a housing having a housing cavity about the axis, the bearing received in the housing cavity, the housing cavity circumferentially circumscribed by a radially inner housing surface, the outer race of the bearing engaged with the radially inner housing surface, a piston chamber located radially outward of the radially inner housing surface, the piston chamber defined circumferentially by an outer piston chamber surface and axially by an axial piston chamber surface, the axial piston chamber surface defining an axial location relative to the axis, the flange extending radially outwardly beyond the radially inner housing surface to inside the piston chamber, the flange carrying a seal at a radially outer circumference thereof, the seal in sealing engagement with the outer piston chamber surface;

a biasing member disposed in the piston chamber, the biasing member in axial abutment against the axial piston chamber surface and extending axially away from the axial location in a first axial direction toward the flange of the outer race, the biasing member arranged for opposing axial movement of the outer race relative to the axial location in a second axial direction opposite the first axial direction; and

a spacer axially trapped between the biasing member and the flange, the spacer having an outer diameter surface in sliding contact with the outer piston chamber surface.

7. The bearing system of claim 6 , wherein the housing defines an oil orifice in fluid communication with inside the piston chamber, and the oil orifice and the biasing member are located on a same side of the flange.

8. The bearing system of claim 6 , wherein the housing defines an oil orifice in fluid communication with inside the piston chamber, and the bearing system includes at least one of a valve and a restrictor in fluid communication with the piston chamber via the oil orifice.

9. The bearing system of claim 6 , wherein the biasing member is at least one of a wave spring, a disc spring, an elastomeric element and a resilient structure projecting from the housing.

10. The bearing system of claim 9 , wherein the biasing member and the housing form an integral piece.

11. The bearing system of claim 6 , wherein the piston chamber is defined by an annular groove of the housing extending circumferentially about the axis, the biasing member received by the annular groove, the flange disposed axially outside of the annular groove, the spacer having a portion axially overlapping the annular groove.

12. A turbine engine comprising:

a first and a second bearing about an axis, the first and the second bearings respectively including:

a first and a second inner race extending circumferentially about the axis;

a first and a second series of rolling elements disposed circumferentially about the axis and around the first and the second inner races respectively;

a first and a second outer race extending circumferentially about the axis and around the first and the second series of rolling elements respectively; and

a flange projecting radially outwardly from the second outer race;

a shaft about the axis, the shaft having a pair of abutments axially spaced from one another, the first and the second inner races mounted to the shaft adjacent to one another between the abutments such that each of the first and the second inner race is axially bound;

a housing having a housing cavity about the axis, the first and second bearings received in the housing cavity, the housing cavity circumferentially circumscribed by a radially inner housing surface, the second outer race of the second bearing engaged with the radially inner housing surface, a piston chamber located radially outward of the radially inner housing surface, the piston chamber defined circumferentially by an outer piston chamber surface and axially by an axial piston chamber surface, the axial piston chamber surface defining an axial location relative to the axis, the flange extending radially outwardly beyond the radially inner housing surface to inside the piston chamber, the flange carrying a seal at a radially outer circumference thereof, the seal in sealing engagement with the outer piston chamber surface;

a biasing member disposed in the piston chamber, the biasing member in axial abutment against the axial piston chamber surface and extending axially away from the axial location in a first axial direction toward the flange of the second outer race, the biasing member arranged for opposing axial movement of the second outer race relative to the axial location in a second axial direction opposite the first axial direction; and

a spacer filling an axial gap (D 3 ) between the biasing member and the flange, the spacer having an outer diameter surface in sliding contact with the outer piston chamber surface.

13. The turbine engine of claim 12 , wherein the turbine engine includes an oil system and at least one of a valve and a restrictor in fluid communication between the oil system and the piston chamber.

14. The turbine engine of claim 12 , wherein the housing defines an oil orifice in fluid communication with inside the piston chamber, and the oil orifice and the biasing member are located on a same side of the flange.

15. The turbine engine of claim 12 , further comprising the spacer disposed in the piston chamber between the biasing member and the flange.