High-Performance Composites

MAY 2014

High-Performance Composites is read by qualified composites industry professionals in the fields of continuous carbon fiber and other high-performance composites as well as the associated end-markets of aerospace, military, and automotive.

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1 6 | H I G H - P E R F O R M A N C E C O M P O S I T E S TESTING TECH men mid-thickness (the neutral axis of bending stress). These screws prevent axial and lateral movement. Finally, because the specimen is con- tinually defecting (bending) during each cycle, each of the loading/support clamps must be free to rotate so that they do not constrain the bending of the specimen. An example of a test fxture that meets all of the above requirements is shown in Fig. 1. The base and loading beams are directly attached to the base and crosshead of a testing machine capable of applying an axial load in both ten- sion and compression. The specimen loading and support span lengths can be varied by loosening the two bolts at the outer end of each loading/support assembly and sliding the assemblies along the beam to the desired position. These bolts can be seen at the top of the image in Fig. 1. As shown, the fxture is set up to perform four-point loading. For three-point loading, one of the loading head assemblies is removed and the remaining head assembly is moved to the center of the beam. (The comparative merits of three- and four-point loading were discussed in my previous columns.) A pivoting cradle is mounted in each loading/support assembly (the bushings in which the cradle axes pivot appear as white circles in Fig. 1). These particu- lar bushings were fabricated of a Tefon polymer. Oil-impregnated bronze bush- ings are stronger, are fabricated to closer tolerances and, thus, are more suitable for high fxture loadings, but the Tefon bushings generate little friction and, therefore, wear very well. The fxture shown has fat loading and support pads since it is designed to be used in sandwich panel testing. Alterna- tively, cylindrically shaped pads can be used — these are sometimes specifed for solid composite laminates. The pads are clamped against the specimen by tight- ening the bolt in each clamp half. Using two bolts permits the user to accommo- date specimens of different thicknesses while keeping the specimen centered in the cradle. Although there has been some inter- est in reversed fexural fatigue testing of composites for many years, there is at the present time no ASTM standard for such testing. However, there is a rela- tively new standard for plastics, ASTM D 7772-12, "Standard Test Method for Flex- ural Fatigue Properties of Plastics," which does include reversed loading. Further, reversed fexural fatigue testing of composites appears to be increasing signifcantly. This is, perhaps, an indica- tion of this industry's progress toward maturity — and the need for more realis- tic service data as applications become more demanding. L E A R N M O R E @ w w w. c o m p o s i t e s w o r l d . c o m Read this article online at short. compositesworld.com/RLFlex. Dr. Adams' commentary on "Flexural testing of composite materials" can be read in HPC March 2013 (p. 11) or by visiting short.compositesworld.com/H85ksD8P. Dr. Adams' discussion of "Flexural test method standards for composite materials" can be read in HPC May 2013 (p. 11) or by visiting short.compositesworld.com/7hguppDi. 0514HPC_TestingTech-OK.indd 16 4/22/2014 2:53:57 PM

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