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Dense Memory Module Advanced Interconnect Design Project By Mike Ryland

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  1. 1. Dense Memory Module Advanced Interconnect Design Project By Mike Ryland
  2. 2. Custom Edge Card Connector shown with 82 Beam style contacts
  3. 3. Connector - Card Interface
  4. 4. Contact to Pad Alignment Challenge
  5. 5. Edge Card Connector Concept Design
  6. 6. DMM Connector Configuration 32 Connector Array on top of Motherboard
  7. 7. DMM Connector Configuration Top View
  8. 8. DMM Connector Configuration Bottom of Mother board (Pin Array)
  9. 9. Pin Socket Interconnect Array Bottom of mother board
  10. 10. Pin-Socket-BGA/LGA Array Interconnects
  11. 11. DMM Board Thermal Management
  12. 12. 1U Chasis and DMM Module Detail
  13. 13. Contact Detail Design
  14. 14. Contact Detail Design cont.
  15. 15. Contact Detail Design cont.
  16. 16. Housing Detail Design
  17. 17. Housing Detail Design cont.
  18. 18. Housing Detail Design cont.
  19. 19. Contact to Housing Tolerance Analysis
  20. 20. Contact to Housing Tolerance Analysis cont.
  21. 21. Connector Prototype
  22. 22. Contact Prototypes
  23. 23. Contact Prototypes
  24. 24. PERMANENT SET AFTER .015 DEFLECTION
  25. 25. MAX RESIDUAL STRESS, K000029902 NORMAL FORCE, BENDING STRESS AND PERMANENT SET
  26. 26. MAX STRESS (Uniform Distribution) TAPERED BEAM UNIFORMELY DISTRIBUTES STRESS ALONG THE LENGTH OF THE CONTACT/BEAM. MINIMIZE LOCAL STRESS CONCENTRATIONS, UTILIZING FULL LENGTH OF BEAM TO DISTRIBUTE STRESS. NORMAL FORCE 5.3 GRAMS PER CONTACT MAX STRESS/DEFLECTION OCCURS AT STEP 10 OF 26, 1.528 SECONDS INTO THE 4.2 SECOND SIMULATION USING A PARABOLIC LOADING/UNLOADING CURVE. STEPS ARE .042 SECONE INCREMENTS.
  27. 27. STRESS DISTRIBUTION (cont). ANIMATION DEMONSTRATING ONE COMPLETE CYCLE OF LOADING-UNLOADING TAPERED BEAM UNIFORMELY DISTRIBUTES STRESS ALONG THE LENGTH OF THE CONTACT/BEAM. MINIMIZE LOCAL STRESS CONCENTRATIONS, UTILIZING FULL LENGTH OF BEAM TO DISTRIBUTE STRESS. NORMAL FORCE 5.3 GRAMS PER CONTACT MAX STRESS/DEFLECTION OCCURS AT STEP 10 OF 26, 1.528 SECONDS INTO THE 4.2 SECOND SIMULATION USING A PARABOLIC LOADING/UNLOADING CURVE. STEPS ARE .042 SECONE INCREMENTS. Animation Press Play button to see animation
  28. 28. MAX FIBRE/SURFACE STRESSES TENSION (+) AND COMPRRESSIVE (-) STRESSES
  29. 29. SETUP AND ASSUMPTIONS INPUT CURVE LOADING/UNLOADING CYCLE .015 PRESCRIBED DISPLACEMENT NO FIXED CONSTRAINTS WERE USED. ROLLER/SLIDER AND REFERENCE GEOMETRY/ SYMMETRY WAS USED TO MAKE SIMULATIONS AS REALISTIC AS POSSIBLE.
  30. 30. Solder Tab K000029903 STRESS ANALYSIS
  31. 31. DEFLECTION
  32. 32. Final DMM Module