Method and apparatus of connecting a fixed drive system to a rotating drive system for a tiltrotor aircraft

Patent metadata

Field	Value
Publication number	US-9834303-B2
Application number	US-201313966726-A
Country	US
Kind code	B2
Filing date	Aug 14, 2013
Priority date	Aug 14, 2013
Publication date	Dec 5, 2017
Grant date	Dec 5, 2017

Abstract

A quill shaft is configured for transferring torque and accepting misalignments between a fixed gearbox and a rotatable spindle gearbox in a propulsion system of a tiltrotor aircraft, the quill shaft includes a first splined portion configured for coupling to an output gear of the fixed gearbox, and a second splined portion configured for coupling to an input gear of the spindle gearbox. The spindle gearbox includes a rotor mast associated therewith, the spindle gearbox being rotatable so that the tiltrotor aircraft can selectively operate in a helicopter mode and airplane mode.

First claim

The invention claimed is:

1. A quill shaft configured for transferring torque and accepting misalignments between a fixed gearbox and a rotatable spindle gearbox in a propulsion system of a tiltrotor aircraft, the quill shaft comprising:
a first splined portion configured for coupling to an output gear of the fixed gearbox;
a second splined portion configured for coupling to an input gear of the spindle gearbox;
wherein the spindle gearbox includes a rotor mast associated therewith, the spindle gearbox being rotatable so that the tiltrotor aircraft can selectively operate in a helicopter mode and airplane mode; and
wherein the quill shaft is configured to selectively transfer torque to the rotatable spindle gearbox from a spiral bevel gearbox associated with a first engine, wherein the quill shaft is configured to selectively transfer torque to the rotatable spindle gearbox from an interconnect drive shaft associated with a second engine, and wherein an output of the spiral bevel gearbox is not substantially coaxial with the quill shaft.

2. The quill shaft according to claim 1 , wherein the quill shaft is oriented such that a centerline axis of the quill shaft intersects an axis of rotation of the rotor mast.

3. The quill shaft according to claim 1 , wherein the first splined portion has a larger diameter than the second splined portion.

4. The quill shaft according to claim 1 , further comprising:
an interior portion on the interior of the first splined portion that includes a feature that a removal tool is attachable thereto.

5. The quill shaft according to claim 4 , wherein the feature is a threaded portion.

6. The quill shaft according to claim 5 , wherein the fixed gearbox includes an access cover which can be removed for access to the feature in the interior portion.

7. The quill shaft according to claim 6 , wherein the quill shaft is removable by attaching the removal tool to the feature in the interior portion.

8. The quill shaft according to claim 1 , further comprising:
a first set of o-ring glands approximate the first splined portion with a first plurality of lubrication ports located between the first splined portion and the first set of o-ring glands;
wherein the first set of o-ring glands are configured to promote a flow of a lubrication fluid from the first plurality of lubrication ports to the first splined portion.

9. The quill shaft according to claim 1 , further comprising:
a second set of o-ring glands approximate the second splined portion with a second plurality of lubrication ports located between the second splined portion and the second set of o-ring glands;
wherein the second set of o-ring glands are configured to promote a flow of a lubrication fluid from the second plurality of lubrication ports to the second splined portion.

10. A tiltrotor aircraft, comprising:
a fuselage;
a wing member;
a first engine disposed at a fixed location relative to the wing member; and
a proprotor having a spindle gearbox, rotor mast, and a plurality of rotor blades drivable in rotation about the rotor mast, the spindle gearbox being rotatable about a conversion axis;
a fixed gearbox coupled to the engine;
a quill shaft configured to transfer torque from the fixed gearbox to the spindle gearbox, the quill shaft comprising:
a first splined portion configured for coupling to an output gear of the fixed gearbox;
a second splined portion configured for coupling to an input gear of the spindle gearbox;

wherein the quill shaft is configured to selectively transfer torque to the rotatable spindle gearbox from a spiral bevel gearbox associated with the first engine, wherein the quill shaft is configured to selectively transfer torque to the rotatable spindle gearbox from an interconnect drive shaft associated with a second engine, and wherein an output of the spiral bevel gearbox is not substantially coaxial with the quill shaft;
wherein the spindle gearbox includes a rotor mast associated therewith, the spindle gearbox being rotatable so that the tiltrotor aircraft can selectively operate in a helicopter mode and airplane mode; and
wherein the quill shaft is oriented such that a centerline axis of the quill shaft intersects an axis of rotation of the rotor mast.

11. The tiltrotor aircraft according to claim 10 , wherein the spindle gearbox is located above an upper wing skin of the wing member.

12. The tiltrotor aircraft according to claim 10 , wherein the first splined portion of the quill shaft has a larger diameter than the second splined portion of the quill shaft.

13. The tiltrotor aircraft according to claim 10 , the quill shaft further comprising:
an interior portion on the interior of the first splined portion that includes a feature that a removal tool is attachable thereto.

14. The tiltrotor aircraft according to claim 13 , wherein the feature of the quill shaft is a threaded portion.

15. The tiltrotor aircraft according to claim 14 , wherein the fixed gearbox includes an access cover which can be removed for access to the feature in the interior portion of the quill shaft.

16. The tiltrotor aircraft according to claim 15 , wherein the quill shaft is removable by attaching the removal tool to the feature in the interior portion of the quill shaft.

Assignees

• Bell Helicopter Textron Inc

Inventors

• Bockmiller David R
• Kooiman James E

Classifications

• B64F5/40

  Maintaining or repairing aircraft · CPC title

• B64C27/22 Primary

  Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft · CPC title

• Y10T74/1966

  Intersecting axes · CPC title

• Y10T29/49318

  Repairing or disassembling · CPC title

• B64C29/0033 Primary

  the propellers being tiltable relative to the fuselage · CPC title