Method for manufacturing composite clubs
A method for manufacturing composite clubs includes the steps: forming a base material by forming a brushed surface on the peripheral surface of a metal tube; coating a bonding resin on the brushed surface of the metal tube; covering the entire outer surface of the metal tube that is coated with the base material with an impregnated glass fiber fabric or a carbon fiber fabric; wrapping the metal tube with a forming adhesive fabric to fix the glass fiber fabric; processing a two-stage heating for the metal tube; and removing the forming adhesive fabric from the metal tube and fabricating the surface of the metal tube to form a finished composite club that has reduced torsional deformation.
The present invention relates to a method for manufacturing composite clubs to reduce torsional deformation.
BACKGROUND OF THE INVENTIONInnovated materials have been constantly introduced for club fabrication in order to enable hitting ball to fly a greater distance. One of the approaches is to generate maximum torsion to reduce deformation of the club. However, altering the material often results in excessive torsion during club swinging, and produces too much deformation. Compared with the conventional rigid clubs, although change of club manufacturing method can enhance club swinging effect, it does not provide required torsion. And it does not help much in reducing the torsional deformation. Users have to improve swinging technique to achieve the desired result. It is not effective. On the other hand, conventional clubs made from carbon fibers and glass fibers usually are fabricated by wrapping a solid steel core, then the steel core is removed to form a hollow club tube. The material forming the club tube has to withstand the swinging torsion. Deformation increases and the strength cannot be enhanced.
SUMMARY OF THE INVENTIONIn view of the aforesaid disadvantages occurred to the conventional clubs that have a greater torsional deformation and smaller strength, the present invention aims to provide a method for manufacturing composite clubs that can reduce the deformation and increase the strength. The method according to the invention includes forming a base material on a metal tube that has a brushed surface by coating a bonding resin; then covering the entire metal tube surface with a layer of glass fiber fabric or carbon fiber fabric or both; wrapping the fabric on the metal tube with a forming adhesive fabric; heating the wrapped metal tube in a two-stage process; peeling off the forming adhesive fabric; finally fabricating the surface to complete the finished product of the composite club.
The foregoing, as well as additional objects, features and advantages of the invention will be more readily apparent from the following detailed description, which proceeds with reference to the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
Please referring to
-
- (a) Form base material 40:
- Prior to manufacturing the golf club, forming a brushed surface 10 on the peripheral surface of a metal tube 1 (referring to
FIG. 2 );
- Prior to manufacturing the golf club, forming a brushed surface 10 on the peripheral surface of a metal tube 1 (referring to
- (b) Bonding resin 41:
- Coating a bonding resin 11 on the brushed surface 10 of the metal tube 1 (referring to
FIG. 3 );
- Coating a bonding resin 11 on the brushed surface 10 of the metal tube 1 (referring to
- (c) Impregnating fabric 42:
- Impregnating a layer of resin (not shown in the drawings) on a glass fiber fabric 2 (or carbon fiber fabric 20);
- (d)—Cover the metal tube 43:
- Covering the entire surface of the metal tube 1 coated with the base material with the impregnated glass fiber fabric 2 (or carbon fiber fabric 20) (referring to
FIG. 4 );
- Covering the entire surface of the metal tube 1 coated with the base material with the impregnated glass fiber fabric 2 (or carbon fiber fabric 20) (referring to
- (e) Wrap the forming adhesive fabric 44:
- Wrapping the metal tube 1 covered by the glass fiber fabric 2 (or carbon fiber fabric 20) with a forming adhesive fabric 3 to fix the glass fiber fabric 2 (or carbon fiber fabric 20) (referring to FIGS. 5A and 5B);
- (f) Two-stage heating 45:
- Heating the metal tube 1 wrapped with the forming adhesive fabric 3 to bond and cure the glass fiber fabric 2 (or carbon fiber fabric 20) on the surface of the metal tube 1; and
- (g) Fabricate the surface process 46:
- Removing the forming adhesive fabric 3 from the metal tube 1, and fabricating the surface of the metal tube 1 (such as coating paint) to become a finished club that has a reduced torsional deformation and an enhanced strength.
- (a) Form base material 40:
Refer to
By means of the aforesaid method, the resulting gold club has less deformation and a greater strength. It offers significant improvements over the conventional golf clubs.
Claims
1. A method for manufacturing composite clubs, comprising steps of:
- (a) forming a base material by forming a brushed surface on the peripheral surface of a metal tube;
- (b) coating a bonding resin on the brushed surface of the metal tube;
- (c) impregnating a layer of resin on a glass fiber fabric;
- (d) covering the entire outer surface of the metal tube coated with the base material with the impregnated glass fiber fabric;
- (e) wrapping the metal tube that is covered by the glass fiber fabric with a forming adhesive fabric to fix the glass fiber fabric;
- (f) processing a two-stage heating for the metal tube that is wrapped with the forming adhesive fabric to bond and cure the glass fiber fabric on the surface of the metal tube; and
- (g) removing the forming adhesive fabric from the metal tube and fabricating the surface of the metal tube.
2. The method of claim 1, wherein the metal tube at step (d) is selectively covered by the glass fiber fabric or a carbon fiber fabric.
3. The method of claim 1, wherein the metal tube at step (d) is covered by the glass fiber fabric and a carbon fiber fabric.
Type: Application
Filed: Apr 7, 2004
Publication Date: Jul 21, 2005
Inventor: Ping-Wen Lin (Kaohsiung Hsien)
Application Number: 10/819,139