IP Library › Granted Patent US 12,338,855
Granted Patent B2
US 12,338,855 · App. 18/406,914 · Granted Jun 24, 2025

Composite end connections

Inventors: James William Bernard (Brackley, GB); Jon Pethick (Leicestershire, GB); Robert Edwin Finney (Charlbury, GB)
Assignee: CROMPTON TECHNOLOGY GROUP, LTD.
F16C3/026
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Quick Facts
Patent No.
US 12,338,855
App. No.
18/406,914
Granted
Jun 24, 2025
Kind
B2
Abstract

A fiber-reinforced polymer composite shaft for transmitting loads along a central axis. The composite shaft comprises a first interface surface extending along the central axis and comprising at least one helical groove and/or a plurality of circumferential grooves for engaging with at least one corresponding helical ridge and/or a plurality of corresponding circumferential ridges of a second interface surface of an end fitting. The at least one helical groove and/or the plurality of circumferential grooves comprises at least one flank with a flank angle of between 32° and 51°. In such an assembly, a preload structure is arranged to provide a radial biasing force to bias the first interference surface against the second interference surface.

Claims (28)

1. A fibre-reinforced polymer composite shaft for transmitting loads along a central axis, the composite shaft comprising:

a first interface surface extending along the central axis and comprising at least one helical groove and/or a plurality of circumferential grooves for engaging with at least one corresponding helical ridge and/or a plurality of corresponding circumferential ridges of a second interface surface of an end fitting;

wherein the at least one helical groove and/or the plurality of circumferential grooves comprises at least one flank with a flank angle of between 32° and 41°, the flank angle being measured between the flank and a perpendicular to the central axis in a plane that contains the central axis.

2. The fibre-reinforced polymer composite shaft as claimed in claim 1 , wherein the flank angle is between 32° and 36°.

3. The fibre-reinforced polymer composite shaft as claimed in claim 1 , wherein the first interface surface comprises an average radius from the central axis of between 10 and 150 mm.

4. The fibre-reinforced polymer composite shaft as claimed in claim 3 , wherein the average radius is between 20 and 30 mm.

5. The fibre-reinforced polymer composite shaft as claimed in claim 1 , wherein the first interface surface is approximately 30 mm long.

6. The fibre-reinforced polymer composite shaft as claimed in claim 1 , wherein the first interface surface is an inner surface of the composite shaft or an outer surface of the composite shaft.

7. The fibre-reinforced polymer composite shaft as claimed in claim 1 , wherein the first interface surface is tapered relative to the central axis or the first interface surface extends parallel to the central axis.

8. An assembly for transmitting loads along a central axis, the assembly comprising:

a fibre reinforced polymer composite shaft as claimed in claim 1 ;

an end fitting comprising a second interface surface extending along the central axis and comprising at least one corresponding helical ridge and/or a plurality of corresponding circumferential ridges that is engaged with the at least one helical groove and/or the plurality of circumferential grooves so as to mount the end fitting to the fibre reinforced polymer composite shaft; and

a preload structure arranged to provide a radial biasing force to bias the first interference surface against the second interference surface.

9. The assembly as claimed in claim 8 , wherein the end fitting is metallic.

10. The assembly as claimed in claim 8 , wherein the coefficient of friction between the first and second surfaces is between 0.01 and 0.3.

11. The assembly as claimed in claim 8 , wherein the coefficient of friction between the first and second surfaces is 0.15.

12. The assembly as claimed in claim 8 , wherein the second interface surface is located radially inward of the first interface surface.

13. The assembly as claimed in claim 12 , wherein the preload structure comprises an annular member arranged to apply the radial biasing force to an outer surface of the composite shaft.

14. The assembly as claimed in claim 8 , wherein the second interface surface is located radially outward of the first interface surface.

15. The assembly as claimed in claim 14 , wherein the preload structure comprises a plug arranged to apply the radial biasing force to an inner surface of the composite shaft.

16. The assembly as claimed in claim 8 , wherein the preload structure is arranged in an interference fit with the composite shaft.

17. The assembly as claimed in claim 8 , wherein the end fitting is arranged to interface with another component.

18. A method of forming an assembly for transmitting loads along a central axis, the method comprising:

forming at least one helical groove and/or a plurality of circumferential grooves comprising at least one flank with a flank angle of between 32° and 41° in a first interface surface of a fibre-reinforced polymer composite shaft, the flank angle being measured between the flank and a perpendicular to the central axis in a plane that contains the central axis;

forming at least one corresponding helical ridge and/or a plurality of corresponding circumferential ridges in a second interface surface of an end fitting;

engaging the at least one helical groove and/or the plurality of circumferential grooves of the first interface surface with the at least one corresponding helical ridge and/or the plurality of corresponding circumferential ridges of the second interface surface so as to mount the end fitting to the composite shaft; and

subsequently engaging the composite shaft with a preload structure so as to bias the first interface surface against the second interface surface with a radial biasing force.

19. The method of claim 18 , wherein forming the at least one helical groove and/or a plurality of circumferential grooves comprises selecting a flank angle to minimise a performance measure that takes into account a total weight of the assembly and a sensitivity of the assembly to changes in friction between the first and second interface surfaces.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 10, 2024
From: BERNARD, JAMES WILLIAM; PETHICK, JON; FINNEY, ROBERT EDWIN
To: CROMPTON TECHNOLOGY GROUP, LTD.
Reel/Frame 066074/0504 →
Priority Claims (1)
EP 20275019 · Jan 29, 2020 · regional
Continuity (2)
Continuation 17161943 · Jan 29, 2021
Related Publication 20240151262A1 · May 9, 2024
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