Composite structural component with tension/compression mechanical joint

Patent metadata

Field	Value
Publication number	US-2018282992-A1
Application number	US-201815909028-A
Country	US
Kind code	A1
Filing date	Mar 1, 2018
Priority date	Mar 31, 2017
Publication date	Oct 4, 2018
Grant date	—

Abstract

A composite structural component includes an elongate member made of a polymer matrix composite material. The elongate member generally extending along an axis of the composite structural component from an end portion thereof. The component also includes an end fitting forming a mechanical joint with the end portion. The elongate member includes a first member extending from the end portion along the axis of the composite structural component and a second member extending from the end portion along the axis of the composite structural component. The end fitting is constrained in the end portion by the first and second members such that the first member is preloaded with a compressive stress in the axial direction and the second member is preloaded with a tensile stress in the axial direction.

First claim

1 . A composite structural component comprising:
an elongate member made of a polymer matrix composite material, the elongate member generally extending along an axis of the composite structural component from an end portion thereof; and an end fitting forming a mechanical joint with the end portion; wherein the elongate member comprises: a first member extending from the end portion along the axis of the composite structural component; a second member extending from the end portion along the axis of the composite structural component; and wherein the end fitting is constrained in the end portion by the first and second members such that the first member is preloaded with a compressive stress in the axial direction and the second member is preloaded with a tensile stress in the axial direction.

2 . A composite structural component according to claim 1 , wherein the first member comprises an end face in contact with the end fitting.

3 . A composite structural component according to claim 2 , wherein the first member further comprises an outer annular component arranged in contact with an outer surface so as to circumscribe the first member at the end face.

4 . A composite structural component according to claim 2 , further comprising a rubber or elastomeric member arranged in contact with the end face of the first member.

5 . A composite structural component according to claim 1 , wherein the first member is axisymmetric.

6 . A composite structural component according to claim 1 , wherein the first member is a filament wound structure comprising multiple layers wound at different angles, for example one or more layers of low angle fibre wrapped at 8-20°) and one or more layers of high angle fibre wrapped at 70-89°.

7 . A composite structural component according to claim 1 , wherein the second member comprises an axisymmetric dome in the end portion.

8 . A composite structural component according to claim 1 , wherein the second member comprises a tension band that wraps around the end fitting in a direction that is perpendicular to the axis.

9 . A composite structural component according to claim 8 , wherein the tension band forms a continuous loop extending along the axis and around an end fitting at each end of the composite structural component.

10 . A composite structural component according to claim 8 , wherein the end fitting comprises a groove in an outer surface that extends in a direction perpendicular to the axial direction and receives the tension band.

11 . A composite structural component according to any of claim 8 , wherein the tension band is made of a polymer matrix composite material consisting of fibre reinforcement extending at an angle of 0-5° to the axis.

12 . A method of forming a mechanical joint for a composite structural component comprising an elongate member made of a polymer matrix composite material, the elongate member generally extending along an axis from an end portion thereof, the method comprising:
providing a first member of the elongate member; positioning an end fitting in contact with the first member in the end portion of the elongate member so as to preload the first member with a compressive stress in the axial direction; providing a second member of the elongate member in contact with the end fitting to form a mechanical joint with the end portion; positioning the end fitting so as to be constrained in the end portion by the first and second members and so as to preload the second member with a tensile stress in the axial direction.

13 . A method according to claim 12 , wherein providing the first member comprises winding fibres or filaments around a mandrel to form the first member.

14 . A method according to claim 12 , wherein providing the second member comprises winding fibres or filaments around the end fitting.

15 . A method according to claim 12 , wherein providing the second member comprises applying a tension band around the end fitting.

Assignees

• Crompton Technology Group Ltd

Inventors

• Beale Tom

Classifications

• F16C3/026 Primary

  Shafts made of fibre reinforced resin · CPC title

• F16C2240/30

  Angles, e.g. inclinations · CPC title

• B29D29/00 Primary

  Producing belts or bands · CPC title

• B64C2001/0072

  from composite materials · CPC title

• B64C1/06

  Frames; Stringers; Longerons {; Fuselage sections} · CPC title