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          Elimination of the Dependence of Forming Limits for AHSS on Testing Process Conditions

          2018-10-29 11:16:00
          LUQIMENG
          Original
          1997
          Junying Min, Tongji University
          John E. Carsley, General Motors Company
          Mark Tharrett, General Motors Company
          Jeong-Whan Yoon, Deakin University and KAIST


          ? Introduced by Keeler in 1960’s and
          adopted by industry in late ‘60s
          ? Used in tryout and stamping plants
          ? Applied to assess formability in
          “virtual” tryout since mid ‘80s
          ? Most reliably determined empirically
          ? Theoretical models require calibration

          1) Understand the cause of this ambiguity
          2) Find a solution to it
          What does a solution look
          like?
          1) A unique forming limit,
          regardless of test
          2) An understanding how to
          use this forming limit

          We can measure the strain path for each test done to determine the FLC


          Each test results in different (unique) degrees of nonlinear strain paths


          The strain FLC is NOT a static
          forming limit.
          The strain FLC is a DYNAMIC limit.
          Question: Could this fact impact
          our measurement of the FLC?


          1) 3% difference in strain between
          the top and bottom surface
          4) Is this intuition correct?
          2) What strain defines the limit?
          3) Intuition suggests to use the average


          Stretch-Bending Study Reported By: Tharrett & Stoughton SAE Report 2003-01-1157


          Conclusion of the Study:
          In every test specimen in which a neck was detected, the MEASURED strain on the CONCAVE 

          side was found to be above the forming limit for in-plane stretching


          hese experimental results make perfect sense from a theoretical perspective
          Necking is an instability that affects the plastic flow of ALL layers through the sheet thickness
          So the instability cannot proceed until all layers satisfy the instability condition

          While it is tempting to think
          these two FLC’s are close
          enough
          The Nakazima Test results are
          systematically higher
          … which suggests we have
          missed something in the
          compensation
          This becomes more obvious
          when we add the 50 mm test



          … when the degree of nonlinearity,
          curvature of the sheet, and contact pressures
          that are involved in stamping automotive
          components


          are more than 10 TIMES LARGER?
          We should instead ALWAYS convert the strain limit to
          a stress limit, and account for the curvature and contact
          pressure in our assessments of the severity of the
          process with respect to necking.



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