Method of manufacturing a composite shaft

Patent metadata

Field	Value
Publication number	US-9358437-B2
Application number	US-201514682423-A
Country	US
Kind code	B2
Filing date	Apr 9, 2015
Priority date	Mar 14, 2013
Publication date	Jun 7, 2016
Grant date	Jun 7, 2016

Abstract

A composite shaft formed from a single flag of composite material having variable fiber orientation, and methods of forming said shaft, are disclosed herein.

First claim

I claim as my invention the following:

1. A composite shaft comprising a shaft axis,
wherein the composite shaft is composed of a single composite flag comprising a butt end and a tip end,
wherein the composite flag comprises a plurality of carbon fibers,
wherein the fiber orientation of the flag with respect to the shaft axis varies along at least a portion of the shaft axis, wherein the fiber orientation of the flag with respect to the shaft axis increases from the tip portion of the flag to an approximate midpoint of the flag, wherein the fiber orientation of the flag remains constant from the midpoint to the butt end of the flag, and
wherein the composite flag is cut from a sheet of pre-deformed prepreg material.

2. The composite shaft of claim 1 , wherein the fiber orientation of the flag at the tip end is no less than 0° and no more than 15°.

3. The composite shaft of claim 2 , wherein the fiber orientation of the flag at the tip end is approximately 0°.

4. The composite shaft of claim 1 , wherein the fiber orientation of the flag at the butt end is no less than 20° and no more than 45°.

5. The composite shaft of claim 4 , wherein the fiber orientation of the flag at the butt end is approximately 30°.

6. The composite shaft of claim 1 , wherein the flag is approximately trapezoidal in shape.

7. The composite shaft of claim 1 , further comprising a golf club head and a grip, wherein the golf club head is affixed to a tip end of the composite shaft, and wherein the grip is affixed to a butt end of the composite shaft.

8. The composite shaft of claim 1 , wherein the composite flag comprises a backing material.

9. The composite shaft of claim 8 , wherein the backing material is composed of an open weave material.

10. The composite shaft of claim 1 , wherein the shaft has a length of at least 35 inches and no more than 46 inches.

11. The composite shaft of claim 1 , wherein the shaft has a length of approximately 18 inches.

12. The composite shaft of claim 1 , wherein the shaft has a length of approximately 48 inches.

13. The composite shaft of claim 1 , wherein the fiber orientation of the flag at the tip portion is approximately 0°, and wherein the fiber orientation of the flag at the midpoint is approximately 22°.

14. A composite shaft comprising a shaft axis,
wherein the composite shaft is composed of a single composite flag comprising a butt end and a tip end,
wherein the composite flag comprises a plurality of continuous carbon fibers,
wherein the composite flag is trapezoidal in shape,
wherein the fiber orientation of the flag with respect to the shaft axis varies along at least a portion of the composite shaft,
wherein the fiber orientation increases from a tip portion to an approximate midpoint of the flag, and
wherein the fiber orientation remains constant from the midpoint to the butt end of the flag.

15. The composite shaft of claim 14 , wherein the fiber orientation of the tip end is approximately 0°, and wherein the fiber orientation of the midpoint is approximately 22°.

16. The composite shaft of claim 14 , wherein the fiber orientation of the tip end is no less than 0° and no more than 15°, and wherein the fiber orientation of the butt end is no less than 20° and no more than 45°.

17. The composite shaft of claim 14 , wherein each of the composite fibers has a smoothly curved shape.

18. The composite shaft of claim 14 , further comprising a backing material composed of an open weave material.

Assignees

• Callaway Golf Co

Inventors

• Ehlers Steven M

Classifications

• B29C35/02

  Heating or curing, e.g. crosslinking or vulcanizing {during moulding, e.g. in a mould}(cold vulcanisation B29C35/18 {; vulcanising tyres, presses therefor B29D30/0601}) · CPC title

• Y10T156/1002

  with permanent bending or reshaping or surface deformation of self sustaining lamina · CPC title

• B29C71/02

  Thermal after-treatment {(B29C71/0063 and B29C71/0072 take precedence)} · CPC title

• Y10T156/1062

  Prior to assembly · CPC title

• B29L2031/5227

  Clubs · CPC title