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A support assembly for coupling a first gearbox to an airframe of an aircraft. The first gearbox has an output gear operable to transfer torque to an input gear of a second gearbox via a common shaft rotatable about a longitudinal axis. The support assembly includes a fixed joint proximate the longi

A support assembly for coupling a first gearbox to an airframe of an aircraft. The first gearbox has an output gear operable to transfer torque to an input gear of a second gearbox via a common shaft rotatable about a longitudinal axis. The support assembly includes a fixed joint proximate the longitudinal axis. A first directional reacting joint remote from the longitudinal axis provides a first radial growth degree of freedom to the first gearbox relative to the longitudinal axis. A second directional reacting joint remote from the longitudinal axis provides a second radial growth degree of freedom to the first gearbox relative to the longitudinal axis. The first radial growth degree of freedom is not parallel with the second radial growth degree of freedom such that the support assembly maintains the output gear of the first gearbox in substantial collinear alignment with the input gear of the second gearbox.

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1. A drive system for an aircraft having an airframe, the drive system comprising: a first gearbox coupled to the airframe and having an input gear;a second gearbox having an output gear;a common shaft configured to transfer torque from the output gear of the second gearbox to the input gear of the

1. A drive system for an aircraft having an airframe, the drive system comprising: a first gearbox coupled to the airframe and having an input gear;a second gearbox having an output gear;a common shaft configured to transfer torque from the output gear of the second gearbox to the input gear of the first gearbox, the common shaft rotatable about a longitudinal axis; anda support assembly coupling the second gearbox to the airframe, the support assembly including a fixed joint proximate the longitudinal axis, a first directional reacting joint remote from the longitudinal axis providing a first radial growth degree of freedom to the second gearbox relative to the longitudinal axis and a second directional reacting joint remote from the longitudinal axis providing a second radial growth degree of freedom to the second gearbox relative to the longitudinal axis;wherein, the first radial growth degree of freedom is not parallel with the second radial growth degree of freedom; andwherein, the support assembly maintains the output gear of the second gearbox in substantial collinear alignment with the input gear of the first gearbox. 2. The drive system as recited in claim 1 wherein the fixed joint further comprises a bolted connection. 3. The drive system as recited in claim 1 wherein the first directional reacting joint further comprises an A-frame connector having spherical elements generally normal to the first radial growth degree of freedom of the second gearbox. 4. The drive system as recited in claim 1 wherein the second directional reacting joint further comprises an A-frame connector having spherical elements generally normal to the second radial growth degree of freedom of the second gearbox. 5. The drive system as recited in claim 1 wherein the fixed joint, the first directional reacting joint and the second directional reacting joint provide lateral support to the second gearbox. 6. The drive system as recited in claim 1 wherein the fixed joint and the first directional reacting joint provide support to the second gearbox in a direction generally parallel to the second radial growth degree of freedom. 7. The drive system as recited in claim 1 wherein the fixed joint and the second directional reacting joint provide support to the second gearbox in a direction generally parallel to the first radial growth degree of freedom. 8. The drive system as recited in claim 1 wherein the first radial growth degree of freedom further comprises a first thermal growth degree of freedom and wherein the second radial growth degree of freedom further comprises a second thermal growth degree of freedom. 9. The drive system as recited in claim 1 wherein the first radial growth degree of freedom is generally normal to the second radial growth degree of freedom. 10. The drive system as recited in claim 1 wherein the first radial growth degree of freedom is generally in a fore/aft direction and wherein the second radial growth degree of freedom is generally in a vertical direction. 11. The drive system as recited in claim 1 wherein the support assembly maintains the output gear of the second gearbox in substantial collinear alignment with the input gear of the first gearbox throughout thermal expansion cycles of the second gearbox. 12. An aircraft comprising: an airframe;a first gearbox coupled to the airframe and having an input gear;a second gearbox having an output gear;a common shaft configured to transfer torque from the output gear of the second gearbox to the input gear of the first gearbox, the common shaft rotatable about a longitudinal axis; anda support assembly coupling the second gearbox to the airframe, the support assembly including a fixed joint proximate the longitudinal axis, a first directional reacting joint remote from the longitudinal axis providing a first radial growth degree of freedom to the second gearbox relative to the longitudinal axis and a second directional reacting joint remote from the longitudinal axis providing a second radial growth degree of freedom to the second gearbox relative to the longitudinal axis;wherein, the first radial growth degree of freedom is not parallel with the second radial growth degree of freedom; andwherein, the support assembly maintains the output gear of the second gearbox in substantial collinear alignment with the input gear of the first gearbox. 13. The aircraft as recited in claim 12 wherein the fixed joint further comprises a bolted connection, wherein the first directional reacting joint further comprises an A-frame connector having spherical elements generally normal to the first radial growth degree of freedom of the second gearbox and wherein the second directional reacting joint further comprises an A-frame connector having spherical elements generally normal to the second radial growth degree of freedom of the second gearbox. 14. The aircraft as recited in claim 12 wherein the fixed joint, the first directional reacting joint and the second directional reacting joint provide lateral support to the second gearbox, wherein the fixed joint and the first directional reacting joint provide support to the second gearbox in a direction generally parallel to the second radial growth degree of freedom and wherein the fixed joint and the second directional reacting joint provide support to the second gearbox in a direction generally parallel to the first radial growth degree of freedom. 15. The aircraft as recited in claim 12 wherein the first radial growth degree of freedom further comprises a first thermal growth degree of freedom, wherein the second radial growth degree of freedom further comprises a second thermal growth degree of freedom and wherein the support assembly maintains the output gear of the second gearbox in substantial collinear alignment with the input gear of the first gearbox throughout thermal expansion cycles of the second gearbox. 16. The aircraft as recited in claim 12 wherein the first radial growth degree of freedom is generally in a fore/aft direction and wherein the second radial growth degree of freedom is generally in a vertical direction. 17. A support assembly for coupling a first gearbox to an airframe of an aircraft, the first gearbox having an output gear operable to transfer torque to an input gear of a second gearbox via a common shaft rotatable about a longitudinal axis, the support assembly comprising: a fixed joint proximate the longitudinal axis;a first directional reacting joint remote from the longitudinal axis providing a first radial growth degree of freedom to the first gearbox relative to the longitudinal axis; anda second directional reacting joint remote from the longitudinal axis providing a second radial growth degree of freedom to the first gearbox relative to the longitudinal axis;wherein, the first radial growth degree of freedom is not parallel with the second radial growth degree of freedom; andwherein, the support assembly maintains the output gear of the first gearbox in substantial collinear alignment with the input gear of the second gearbox. 18. The support assembly as recited in claim 17 wherein the fixed joint, the first directional reacting joint and the second directional reacting joint provide lateral support to the first gearbox, wherein the fixed joint and the first directional reacting joint provide support to the first gearbox in a direction generally parallel to the second radial growth degree of freedom and wherein the fixed joint and the second directional reacting joint provide support to the first gearbox in a direction generally parallel to the first radial growth degree of freedom. 19. The support assembly as recited in claim 17 wherein the first radial growth degree of freedom further comprises a first thermal growth degree of freedom, wherein the second radial growth degree of freedom further comprises a second thermal growth degree of freedom and wherein the support assembly maintains the output gear of the first gearbox in substantial collinear alignment with the input gear of the second gearbox throughout thermal expansion cycles of the first gearbox. 20. The support assembly as recited in claim 17 wherein the first radial growth degree of freedom is generally in a fore/aft direction and wherein the second radial growth degree of freedom is generally in a vertical direction.