Vibration resistant torsionally compliant transmission shaft

Patent metadata

Field	Value
Publication number	US-11566657-B2
Application number	US-201916697485-A
Country	US
Kind code	B2
Filing date	Nov 27, 2019
Priority date	May 2, 2019
Publication date	Jan 31, 2023
Grant date	Jan 31, 2023

Abstract

A transmission shaft is provided comprising an input side for inputting torque, an output side for outputting torque, and a rod extending in a longitudinal direction between the input side and the output side to transfer torque along the transmission shaft. The rod comprises a first end provided at the input side, a second end provided at the output side and a torsional compliant section extending therebetween providing the transmission shaft with a torsional stiffness. The torsional compliant section comprises a cross-section which extends in the longitudinal direction to define a central core for transmitting torque directly from the first end to the second end and a radially outer section. This section also comprises a plurality ribs which extend radially and longitudinally from an outer periphery of the central core for increasing transverse stiffness of the rod.

First claim

The invention claimed is:

1. A transmission shaft for an aircraft comprising:
a first side for inputting torque;
a second side for outputting torque; and
a composite rod comprising fibres extending longitudinally the entire length of the rod, the rod extending in a longitudinal direction between the first side and the second side to transfer torque along the transmission shaft, the rod comprising:
a first end provided at the first side;
a second end provided at the second side; and
a torsional compliant section extending therebetween providing the transmission shaft with a torsional stiffness,
wherein the transmission shaft is configured for driving an actuator in a wing of the aircraft,
wherein the torsional compliant section comprises a cross-section which extends in the longitudinal direction to define a central core for transmitting torque directly from the first end to the second end and a radially outer section comprising a plurality ribs which extend radially and longitudinally from an outer periphery of the central core for increasing transverse stiffness of the rod,
wherein the first end of the rod and the first side of the transmission shaft are coupled through a first circumferentially extending interface to deliver torque into the torsional compliant section, and the second end of the rod and the second side of the transmission shaft are coupled through a second circumferentially extending interface to deliver torque out of the torsional compliant section,
wherein end surfaces of the ribs of the torsional compliant section are spaced from the first and second circumferentially extending interfaces, and
wherein the ribs or a plurality of the ribs comprise a laterally extending flange arranged at a radially outer end of the rib, the flange extending in a generally circumferential or tangential direction to the rib, and wherein each flange is arranged symmetrically at the radially outer end of the rib with the rib extending along a midline of the flange.

2. A transmission shaft as claimed in claim 1 , wherein:
the first side is arranged to transmit torque into the first end of the rod through a first portion of a circumferential outer surface of the central core only, the ribs comprising first end surfaces which extend from the circumferential outer surface spaced from the first side and the first circumferentially extending interface so as to be functionally isolated from the inputted torque as the torque enters the first end of the rod, and
the second side is arranged to transmit torque out of the second end of the rod through a second portion of the circumferential outer surface of the central core only, the ribs comprising second end surfaces which extend from the circumferential outer surface spaced from the second side and the second circumferentially extending interface so as to be functionally isolated from the outputted torque as the torque exits the second end of the rod.

3. A transmission shaft as claimed in claim 1 , wherein the first circumferentially extending interface between the first end of the rod and the first side of the transmission shaft is arranged to deliver torque into the torsional compliant section through radially extending fasteners.

4. A transmission shaft as claimed in claim 3 , wherein the radially extending fasteners are rivets.

5. A transmission shaft as claimed in claim 1 , wherein the first circumferentially extending interface between the first end of the rod and the first side of the transmission shaft is arranged to deliver torque into the torsional compliant section through a splined connection, an adhesive connection and/or a fused connection.

6. A transmission shaft as claimed in claim 1 , wherein:
the rod comprises a continuous cross-section.

7. A transmission shaft as claimed in claim 1 , wherein the central core has an outer diameter dimension which is more than twice the lateral thickness of any rib.

8. A transmission shaft as claimed in claim 7 , wherein the central core has an outer diameter dimension which is three times or more the lateral thickness of any rib.

9. A transmission shaft as claimed in claim 1 , comprising a first flexible coupling provided at the first side with a universal joint or a self-aligning bearing for inputting torque and a second flexible coupling provided at the second side with a universal joint or a self-aligning bearing for outputting torque.

10. A transmission shaft as claimed in claim 1 , wherein the rod has four or more ribs arranged around the central core.

11. A transmission shaft as claimed in claim 10 , wherein the rod has six ribs.

12. A transmission shaft as claimed in claim 10 , wherein the rod has eight ribs.

13. A method of making a transmission shaft for an aircraft, the transmission shaft comprising a first side for inputting torque, a second side for outputting torque, a composite rod comprising fibres extending longitudinally the entire length of the rod, the rod extending in a longitudinal direction between the first side and the second side to transfer torque along the transmission shaft, the rod comprising a first end provided at the first side, a second end provided at the second side and a torsional compliant section extending therebetween providing the transmission shaft with a torsional stiffness, wherein the transmission shaft is configured for driving an actuator in a wing of the aircraft, wherein the rod comprises a cross-section which extends in the longitudinal direction to define a central core for transmitting torque directly from the first end to the second end and a radially outer section comprising a plurality ribs which extend longitudinally and radially from an outer periphery of the central core for increasing transverse stiffness of the rod, wherein the method comprises:
coupling the first side to the first end through a first circumferentially extending interface which is able to deliver torque into the torsional compliant section; and
coupling the second end of the rod to the second side of the transmission shaft through a second circumferentially extending interface which is able to deliver torque out of the torsional compliant section;
wherein end surfaces of the ribs are spaced from the first and second circumferentially extending interfaces; and
wherein the method further comprises forming at least a plurality of the ribs with a circumferentially or tangentially extending flange and wherein each flange is formed symmetrically at a radially outer end of the respective rib.

14. A transmission shaft for an aircraft comprising:
a first side for inputting torque;
a second side for outputting torque; and
a composite rod comprising fibres extending longitudinally the entire length of the rod, the rod extending in a longitudinal direction between the first side and the second side to transfer torque along the transmission shaft, the rod comprising:
a first end provided at the first side;
a second end provided at the second side; and
a torsional compliant section extending therebetween providing the transmission shaft with a torsional stiffness,
wherein the transmission shaft is configured for driving an actuator in a wing of the aircraft,
wherein the torsional compliant section comprises a cross-section which extends in the longitudinal direction to define a central core for transmitting torque directly from the first end to the second end and a radially outer section comprising a plurality ribs which extend radially and longitudinally from an outer periphery of the central core for increasing transverse stiffness of the rod,
wherein the first end of the rod and the first side of the transmis

Assignees

• Goodrich Corp

Inventors

• Kiełbowicz Dariusz
• Krulak Maciej

Classifications

• F16C2202/02

  Mechanical properties · CPC title

• F16C2220/48

  by extrusion, e.g. of metallic profiles · CPC title

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• F16C1/02

  for conveying rotary movements · CPC title

• F16C1/08

  End connections · CPC title