Load balanced journal bearing pin for planetary gear

1. A fan drive gear system comprising:

a sun gear rotatable about an axis of rotation;

a plurality of intermediate gears rotatable about an intermediate gear rotation axis in meshing engagement with the sun gear;

a ring gear circumscribing the intermediate gears;

a bearing assembly supporting at least one of the plurality of intermediate gears, the bearing assembly including a first beam, a second beam and a bearing surface, the first beam extending axially in a first direction from a support structure to a first end spaced axially from the support structure, the second beam extending from the first end of the first beam in a second axial direction that is opposite the first direction to a midway portion of the bearing surface, and the bearing surface is supported on the second beam, wherein both the first beam and the second beam include an approximately common stiffness and bend in opposite directions to maintain the bearing surface substantially parallel to the intermediate gear rotation axis under a load applied to the bearing surface during operation.

2. The fan drive gear system as recited in claim 1 , wherein the first beam includes a first thickness in cross-section that combined with a first length provides a first stiffness.

3. The fan drive gear system as recited in claim 1 , wherein the first beam comprises a portion of a support structure.

4. The fan drive gear system as recited in claim 3 , wherein the support structure comprises a torque frame.

5. The fan drive gear system as recited in claim 1 , wherein the second beam extends from the end of the first beam to a midway point of the bearing surface.

6. The fan drive gear system as recited in claim 1 , including a passage for lubricant through the bearing surface and a lubricant conduit for communicating lubricant from the first beam to the passage in the bearing surface.

7. The fan drive gear system as recited in claim 6 , including a first opening within the first beam receiving a first end of the lubricant conduit and a second opening in the second beam proximate the lubricant passage for receiving a second end of the lubricant conduit.

8. The fan drive gear system as recited in claim 7 , wherein the lubricant conduit is flexible to enable relative bending of the first beam relative to the second beam.

9. A fan drive gear system comprising:

a sun gear rotatable about an axis of rotation;

a plurality of intermediate gears rotatable about an intermediate gear rotation axis in meshing engagement with the sun gear;

a ring gear circumscribing the intermediate gears;

a bearing assembly supporting at least one of the plurality of intermediate gears, the bearing assembly including a first beam extending in a first direction and a second beam extending from an end of the first beam in a second direction, and a bearing surface supported on the second beam, wherein the first and second beams are configured to maintain the bearing surface substantially parallel to the intermediate gear rotation axis during operation, wherein the first beam includes a first thickness in cross-section that combined with a first length provides a first stiffness and the second beam includes a second thickness in cross-section that combined with a second length provides a second stiffness approximately equal to the first stiffness, wherein both the first beam and the second beam include an approximately common stiffness and bend in opposite directions to maintain the bearing surface substantially parallel to the intermediate gear rotation axis under a load applied to the bearing surface.

10. A turbofan engine comprising:

a fan including a plurality of fan blades rotatable about an axis;

a compressor section;

a combustor in fluid communication with the compressor section;

a turbine section in fluid communication with the combustor; and

a fan drive gear system driven by the turbine section, the fan drive gear system including a sun gear rotatable about an axis of rotation; a plurality of intermediate gears each rotatable about an intermediate gear rotation axis and in meshing engagement with the sun gear; a ring gear circumscribing the intermediate gears, and a bearing assembly supporting at least one of the plurality of intermediate gears, wherein the bearing assembly includes a first beam, a second beam and a bearing surface, the first beam extending in a first axial direction from a support structure to a first end, the second beam extending from the first end of the first beam in a second axial direction to a midway portion of the bearing surface, and the bearing surface is supported on the second beam, wherein both the first beam and the second beam include an approximately common stiffness and bend in opposite directions to maintain the bearing surface substantially parallel to the intermediate gear rotation axis under a load applied to the bearing surface during operation.

11. The turbofan engine as recited in claim 10 , wherein the turbine section includes a fan drive turbine coupled to drive the fan through the fan drive gear system and a second turbine forward of the fan drive turbine and a ratio of a number of fan blades in the fan and a number of rotors in the fan drive turbine is between 3.3 and 8.6.

12. A turbofan engine comprising:

a fan including a plurality of fan blades rotatable about an axis;

a compressor section;

a combustor in fluid communication with the compressor section;

a turbine section in fluid communication with the combustor; and

a fan drive gear system driven by the turbine section, the fan drive gear system including a sun gear rotatable about an axis of rotation; a plurality of intermediate gears each rotatable about an intermediate gear rotation axis and in meshing engagement with the sun gear; a ring gear circumscribing the intermediate gears, and a bearing assembly supporting at least one of the plurality of intermediate gears, wherein the bearing assembly includes a first beam extending in a first direction and a second beam extending from an end of the first beam in a second direction, and a bearing surface supported on the second beam, wherein the first and second beams are configured to maintain the bearing surface substantially parallel to the intermediate gear rotation axis during operation, wherein the first beam includes a first thickness in cross-section that combined with a first length provides a first stiffness and the second beam includes a second thickness in cross-section that combined with a second length provides a second stiffness approximately equal to the first stiffness and wherein both the first beam and the second beam include an approximately common stiffness and bend in opposite directions to maintain the bearing surface substantially parallel to the intermediate gear rotation axis under a load applied to the bearing surface.

13. The turbofan engine as recited in claim 12 , wherein the second beam extends from the end of the first beam to a midway point of the bearing surface.

14. The turbofan engine as recited in claim 13 , wherein the first beam comprises a portion of a support structure.

15. The turbofan engine as recited in claim 14 , including a passage for lubricant through the bearing surface and a lubricant conduit for communicating lubricant from the first beam to the passage in the bearing surface.

16. A method of assembling a fan drive gear system comprising:

providing a sun gear for rotation about an axis of rotation;

providing a plurality of intermediate gears configured for rotation about an intermediate gear rotation axis to be in meshing engagement with the sun gear; and

providing a bearing assembly to support at least one of the plurality of intermediate gears, wherein the bearing assembly is further configured to include a first beam, a second beam and a bearing surface, the first beam configured to extend in a first axial direction from a support structure to a first end, the second beam configured to extend from the first end of the first beam in a second direction to a midway portion of the bearing surface, and the bearing surface configured to be supported on the second beam and configuring both the first beam and the second beam to include an approximately common stiffness and to bend in opposite directions for maintaining the bearing surface substantially parallel to the intermediate gear rotation axis under a load applied to the bearing surface.

17. The method as recited in claim 16 , wherein configuring the first beam includes defining a first thickness in cross-section that combined with a first length provides a first stiffness.

18. The method as recited in claim 17 , wherein configuring the second beam includes defining a second thickness in cross-section that combined with a second length provides a second stiffness approximately equal to the first stiffness.

19. The method as recited in claim 18 , including defining a passage for lubricant through the bearing surface and defining a lubricant conduit for communicating lubricant from the first beam to the passage in the bearing surface.