A method of producing composite strips of metal powder and solid is
proposed by cold rolling and sinter bonding. Copper or stainless steel powder
is rolled together with a solid steel strip that has numerous punching holes.
The punched strip is sandwiched between layers of the compacted powder and then
is sintered. A composite strip with the compacted po%vder layer on one side of
the punched strip is also fabricated. Effects of the roll gap on (1) the
rolling load, (2) the relative density at powder layers and (3) the thickness of
composite strip after sintering are presented. The thickness of sintered
powder layer can be made very thick in comparison with the thickness of
sintered powder strip made from conventional powder rolling. The bond strength
between the powder layer and the punched strip is mainly dependent upon bridges
of the sintered powder through the punching holes. Re-rolling of the composite
strip gives higher strength, higher density and better surface roughness.
Keywords:powder forming, powder rolling, sintered powder materials, compos-
ite materials, plastic forming, powder compaction
Elastic-Plastic Behavior of Sheet Metal Subjected to In-plane Reverse Loading
(Received on December 5, 1994)
Toshihiko KUWABARA, Yoshiyuki MORITA
Yohsuke MIYASHITA and Susumu TAKAHASHI
A novel experimental method for measuring in-plane compressive stress-strain curves of sheet metal is
proposed with using comb-shaped dies. Furthermore, using this method, uniaxial tensile test of in-plane pre-
compressed specimens (CT-test), in-plane compression test of uniaxially pre-stretched specimens (TC-test), and
uniaxial re-tensile test of TC-tested specimens (TCT-test) are conducted for aluminum alloy A5182-0 and AK-
steel sheet (SPCE). Results obtained in this study are as follows. 1) For virgin material of A5182-0, in-plane
compressive true stress lcl is almost the same as the uniaxial tensile true stress cr, , while for AK-steel, lal
becomes larger than a, . 2) For TC-, CT-, TCT-tests, the plastic flow stress observed during reverse loading
exhibits a definite decrease compared with that of the virgin specimen. 3) It is found for A5182-0 that the c-and
ti-values of uniaxial stress-strain curves obtained from CT-and TCT-tests can be formulated as a single function
of the sum of the plastic strains imposed on the specimen prior to the tensile test. 4) AK-steel exhibits either non-
work hardening region or work softening region in the stress-strain curves during reverse loading. Further
investigation is necessary to formulate complicated work-hardening behavior of AK-steel.
Keywords: material testing, sheet metal, in-plane compression test, reverse loading, A5182-0, AK-steel