Tiltrotor aircraft having pillow block mounted pylon assemblies
A propulsion system for a tiltrotor aircraft includes an engine supported by the airframe and a fixed gearbox operably coupled to the engine. Inboard and outboard pedestals are supported by the airframe and positioned above the wing. A pylon assembly is rotatably coupled between the inboard and outboard pedestals. The pylon assembly includes a spindle gearbox having an input gear, a mast operably coupled to the input gear and a proprotor assembly operable to rotate with the mast. The spindle gearbox is rotatable about a conversion axis to selectively operate the tiltrotor aircraft between helicopter and airplane modes. A common shaft, rotatable about the conversion axis, is configured to transfer torque from an output gear of the fixed gearbox to the input gear of the spindle gearbox. Each of the inboard and outboard pedestals includes a pillow block housing such as a full or a split pillow block housing.
1. A propulsion system for a tiltrotor aircraft having a helicopter mode and an airplane mode, the tiltrotor aircraft having an airframe including a fuselage and a wing, the propulsion system comprising:
an engine supported by the airframe proximate an outboard end of the wing;
a fixed gearbox operably coupled to the engine and having an output gear;
inboard and outboard pedestals supported by the airframe and positioned above the wing;
a pylon assembly rotatably coupled between the inboard and outboard pedestals, the pylon assembly including a spindle gearbox having an input gear, a mast operably coupled to the input gear and a proprotor assembly operable to rotate with the mast, the spindle gearbox rotatable about a conversion axis to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode; and
a common shaft configured to transfer torque from the output gear of the fixed gearbox to the input gear of the spindle gearbox, the common shaft rotatable about the conversion axis;
wherein, each of the inboard and outboard pedestals further comprises a pillow block housing.
2. The propulsion system as recited in claim 1 wherein each of the inboard and outboard pedestals further comprises a full pillow block housing.
3. The propulsion system as recited in claim 1 wherein each of the inboard and outboard pedestals further comprises a split pillow block housing.
4. The propulsion system as recited in claim 1 wherein the inboard pedestal further comprises a full pillow block housing and wherein the outboard pedestal further comprises a split pillow block housing.
5. The propulsion system as recited in claim 1 wherein one of the inboard and outboard pedestals further comprises a full pillow block housing and the other of the inboard and outboard pedestals further comprises a split pillow block housing.
6. The propulsion system as recited in claim 1 wherein the inboard and outboard pedestals are coupled to the airframe.
7. The propulsion system as recited in claim 6 wherein each of the inboard and outboard pedestals further comprises an intermediate support.
8. The propulsion system as recited in claim 6 wherein each of the inboard and outboard pedestals is coupled directly to the airframe.
9. The propulsion system as recited in claim 6 wherein the coupling between each of the inboard and outboard pedestals and the airframe further comprises a sheer boss.
10. The propulsion system as recited in claim 1 wherein at least a portion of the inboard and outboard pedestals is integral with the airframe.
11. The propulsion system as recited in claim 1 wherein the inboard and outboard pedestals support fore/aft loads generated by the proprotor assembly when the tiltrotor aircraft is in the airplane mode.
12. The propulsion system as recited in claim 1 wherein the inboard and outboard pedestals support vertical loads generated by the proprotor assembly when the tiltrotor aircraft is in the helicopter mode.
13. A tiltrotor aircraft having a helicopter mode and an airplane mode, the tiltrotor aircraft comprising:
an airframe including a fuselage and a wing;
an engine supported by the airframe proximate an outboard end of the wing;
a fixed gearbox operably coupled to the engine and having an output gear;
inboard and outboard pedestals supported by the airframe and positioned above the wing;
a pylon assembly rotatably coupled between the inboard and outboard pedestals, the pylon assembly including a spindle gearbox having an input gear, a mast operably coupled to the input gear and a proprotor assembly operable to rotate with the mast, the spindle gearbox rotatable about a conversion axis to selectively operate the tiltrotor aircraft between the helicopter mode and the airplane mode; and
a common shaft configured to transfer torque from the output gear of the fixed gearbox to the input gear of the spindle gearbox, the common shaft rotatable about the conversion axis;
wherein, each of the inboard and outboard pedestals further comprises a pillow block housing.
14. The tiltrotor aircraft as recited in claim 13 wherein each of the inboard and outboard pedestals further comprises a full pillow block housing.
15. The tiltrotor aircraft as recited in claim 13 wherein each of the inboard and outboard pedestals further comprises a split pillow block housing.
16. The tiltrotor aircraft as recited in claim 13 wherein the inboard pedestal further comprises a full pillow block housing and wherein the outboard pedestal further comprises a split pillow block housing.
17. The tiltrotor aircraft as recited in claim 13 wherein one of the inboard and outboard pedestals further comprises a full pillow block housing and the other of the inboard and outboard pedestals further comprises a split pillow block housing.
18. The tiltrotor aircraft as recited in claim 13 wherein the inboard and outboard pedestals are coupled to the airframe.
19. The tiltrotor aircraft as recited in claim 13 wherein at least a portion of the inboard and outboard pedestals is integral with the airframe.
20. The tiltrotor aircraft as recited in claim 13 wherein the inboard and outboard pedestals support fore/aft loads generated by the proprotor assembly when the tiltrotor aircraft is in the airplane mode and wherein the inboard and outboard pedestals support vertical loads generated by the proprotor assembly when the tiltrotor aircraft is in the helicopter mode.