초록 ▼

A number of machines such as gas turbine engines have asymmetric axial loading along a shaft (2, 3, 4). In order to accommodate for this asymmetric loading, known as an end bearing load, a load share bearing (103) is typically provided. However, specifying the fixed bearing (11, 12) becomes increasi

A number of machines such as gas turbine engines have asymmetric axial loading along a shaft (2, 3, 4). In order to accommodate for this asymmetric loading, known as an end bearing load, a load share bearing (103) is typically provided. However, specifying the fixed bearing (11, 12) becomes increasingly difficult as space and weight considerations are taken into account. In such circumstances providing a combination of a fixed bearing (11, 12) and a load share bearing (103) to achieve an acceptable bearing end load capacity is more acceptable. The proportion of the combination provided respectively by the fixed bearing and the load share bearing can be varied dependent upon operational stage in order to achieve more efficient operation.

대표청구항 ▼

1. A method of operating a bearing arrangement for a shaft subject to axial loading over an operating cycle, the bearing arrangement including at least a fixed bearing and a load share bearing to act in combination to accommodate the axial load, method comprising: determining a stage of the operatin

1. A method of operating a bearing arrangement for a shaft subject to axial loading over an operating cycle, the bearing arrangement including at least a fixed bearing and a load share bearing to act in combination to accommodate the axial load, method comprising: determining a stage of the operating cycle;determining the axial load and varying the axial load applied to the load share bearing; andvarying the axial load applied between the load share bearing and the fixed bearing by operating a hydraulic piston operatively connected at least one dedicated pump. 2. The method of claim 1, wherein the load applied to the load share bearing is one of a plurality of fixed load values. 3. The method of claim 1, wherein the bearing arrangement incorporates a sensor to determine the stage of the operating cycle. 4. The method of claim 1, wherein there is a fixed relationship between the stage of the operating cycle and the axial load applied by the hydraulic piston. 5. The method of claim 1, wherein there is a variable relationship between the stage of the operating cycle and the axial load applied by the hydraulic piston dependent upon a sensor determining actual axial load upon the shaft. 6. The method of claim 1, wherein the method comprises the step of applying at least half of a total axial load to the load share bearing. 7. The method of claim 1, wherein two load share bearings are present on the shaft and the method comprises the step of applying at least one third of a total axial load on each of the two load share bearings. 8. The method of claim 1, wherein the varying step is performed while the bearing arrangement is installed in an aircraft engine, and the aircraft engine undergoes any one or more of the following stages ground/idle and taxi and/or take off and/or climb and/or cruise and/or descent and/or reverse thrust. 9. The method of claim 1, further comprising: preferentially loading the load share bearing using a feedback loop, such that a differential load between the load share bearing and the fixed bearing is set for particular stages of the operating cycle. 10. The method of claim 1, further comprising: actively controlling the hydraulic piston using a control unit that varies an amount of hydraulic pressure necessary to displace the hydraulic piston to meet axial load for a particular stage of the operating cycle. 11. A bearing arrangement for a shaft subject to axial loading over an operating cycle, the bearing arrangement comprising: a fixed bearing;a load share bearing that acts in combination with the fixed bearing to accommodate the axial loading; anda hydraulic piston;a dedicated pump operatively connected to the hydraulic piston, such that operation of the hydraulic piston varies the axial load applied between the load share bearing and the fixed bearing. 12. The bearing arrangement of claim 11, wherein the axial load applied to the load share bearing is one of a plurality of fixed load values. 13. The bearing arrangement of claim 11, wherein the bearing arrangement incorporates a sensor to determine the stage of the operating cycle. 14. The bearing arrangement of claim 11, wherein there is a fixed relationship between a particular stage of the operating cycle and the axial load applied by the hydraulic piston. 15. The bearing arrangement of claim 11, wherein there is a variable relationship between a particular stage of the operating cycle and the axial load applied by the hydraulic piston dependent upon a sensor determining actual axial load upon the shaft. 16. The bearing arrangement of claim 11, further comprising: a feedback loop that preferentially loads the load share bearing, such that a differential load between the load share bearing and the fixed bearing is set for particular stages of the operating cycle. 17. The bearing arrangement of claim 11, further comprising: an active control unit that is configured to vary an amount of hydraulic pressure necessary to displace the hydraulic piston to meet axial load for a particular stage of the operating cycle.