Abstract A method for joining a composite material shaft, such as a graphite epoxy or fiber glass driveshaft, to a metal end member is disclosed, wherein said joint is capable of withstanding large ranges of temperature and humidity, can handle high torque and has high resistance to fatigue. The design of parallel grooves on the end of a metallic sleeve concentrically aligned within the shaft is amenable to mass production. The first layer of fibers of the composite material shaft is preferably wound perpendicular to the orientation of the grooves. On the other end of the metallic sleeve is carved a scalloped pattern which facilitates concentric alignment of the sleeve on the tooling mandrel and helps to reduce shear stress between the sleeve and shaft. A method for mass production of shafts with metallic end joints attached employs an elongated spinning mandrel and pre-preg tape wound at high speed.
Method for fabricating composite fiber-adhesive shafts with metallic and joints comprising: positioning at least two metallic sleeves at appropriate locations along an elongated tooling mandrel; forming parallel grooves in the outside surface of each of said sleeves; winding a first layer of fibers around said mandrel-cum-sleeves; winding at least a second layer of fibers on top of said first layer; curing said composite; and removing the mandrel from within the cured composite shaft structure; wherein said sleeves form at least part of said end joints; wherein one end of each sleeve is tapered and cut to form a plurality of crimping members having substantially identical shapes.
Claim 2
Dependent Claim
106 words
Method for fabricating composite fiber-adhesive shafts with metallic and joints comprising: positioning at least two metallic sleeves at appropriate locations along an elongated tooling mandrel; forming parallel grooves in the outside surface of each of said sleeves; winding a first layer of fibers around said mandrel-cum-sleeves; winding at least a second layer of fibers on top of said first layer; curing said composite; and removing the mandrel from within the cured composite shaft structure; wherein said sleeves form at least part of said end joints; wherein one end of each sleeve is tapered and cut to form a plurality of crimping members having substantially identical shapes.
Claim 3
Dependent Claim
34 words
Method of claim 1 wherein said winding steps are preceded by an additional step of crimping said crimping member onto said mandrel so as to facilitate concentric alignment between said sleeves and said mandrel.
Claim 4
Dependent Claim
29 words
Method of claim 2 wherein said crimping step is followed by the additional step of winding a high peel strength adhesive tape around the crimped portion of each sleeve.
Claim 5
Dependent Claim
32 words
Method of claim 1 wherein sinusoidal cuts are axisymmetrically cut into two sleeves simultaneously so as to form said crimping members in each of said two sleeves without producing any scrap metal.
Claim 6
Dependent Claim
30 words
Method of claim 1 wherein said winding steps use pre-impregnated composite tape; and each groove has a radius of between approximately one and four times the radius of said fibers.
Claim 7
Dependent Claim
17 words
Method of claim 1 wherein said curing step comprises spinning said wound mandrel at an elevated temperature.