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Summary of first round of testing of shim concept for modular coil assembly

Summary of first round of testing of shim concept for modular coil assembly. 8-28-06. Problem. Shear loading in the inboard regions has no manner in which to be resolved. From Art and H.M. modeling.

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Summary of first round of testing of shim concept for modular coil assembly

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  1. Summary of first round of testing of shim concept for modular coil assembly 8-28-06

  2. Problem Shear loading in the inboard regions has no manner in which to be resolved

  3. From Art and H.M. modeling Bottom Line: friction alone will not prevent sliding. (how much sliding that would ultimately result is unanswered)

  4. 20° Linear H.M E = 8.5 Mpsi Freudenberg

  5. Further Checking The stress plots between the two models agree well with each other. However, It appears that turning one coil non-linear at a time produces different compressive forces at coil joints (unbalanced) then cases where all coils exhibit like properties.

  6. Concept to resolve shear forces Add shear pins to prevent this motion from occurring

  7. Calculation for size and number based on largest shear force from shim abinb

  8. What an individual shim would look like 53 pins on approx 2.5” centers 70 pins on approx 2” centers Design will be similar to the left figure (with 50 pins per section)

  9. Pins and shims (up-close) Large clearance holes are needed to allow for alignment

  10. SST Shims, G-10 Shims, bushings and pins

  11. Test Fixture A prototype fixture containing 4 pins was designed and loaded

  12. Stycast not shown .625 Pins are 2” apart Fixture

  13. Fixture Outer pull plate is invisible Welded stud bushing epoxy G-10 shim Steel shim

  14. Stud Welding • The four half inch studs were welded on at the MDL laboratory onto the two pull plates. The pins had very little tilt to them and were fairly normal to the plates. • The weld bead was then ground off and the studs were cut back to 3/8” long. • This procedure can be performed at PPPL in the same manner as was done at MDL. • All other parts of the fixture (excluding the studs), were machined at a local machine shop.

  15. Sample Preparation (Awaiting Insertion of the Stycast) 1/32” Groove for Stycast run off (two places) Imagine from cell phone (poor quality)

  16. Sample Preparation (Insertion of the Stycast) Mixed Stycast 2850 with catalyst 23LV Extracted using Walgreens syringe Stycast was inserted from the top filling all four holes in this orientation

  17. Stycast Support Weight First two holes (with pins up) were filled with 3cc’s of Stycast to the top 3cc’s were then placed in the other two holes and the top plate was placed down.

  18. More Preparation pictures pool Another View of Stycast Pool Final Step (assembling top pull plate onto fixture)

  19. Independent measuring extensometer installed on outer lower block via magnetic mount Max Load tested so far = 15,000 lbs (3750 lbs/pin) Stroke and load are measured by the 5-0 kip load cell on top of the machine (just outside the picture) Shim Test Fixture loaded into pull fixture

  20. The “one armed bandit” Close up of the bandit Hard to see, but the probe touches the bottom of the shim piece here.

  21. Prototype testing Max loading of 15,000 lbs

  22. First test

  23. 2 mil offset

  24. Test Setup #2: left and right side measuring All tests showed approximately 6-7 mils of deflection at 15,000 lbs

  25. Finite Element Analysis Experimental demonstrated .006-.007 in deflection for 15,000 lbs (3750 lbs/pin)

  26. FEA Loading and setup Mesh Elastic Modulus SST = 28 Mpsi G-10 = 7 Mpsi Stycast 2850 = 1.05 Mpsi from Fermilab paper (TM-2339-E) 200 lb preload applied to bolts 15,000 lb tension load (top hole) Model is fixed at bottom hole Frictionless contact between g-10 shims and outer pulling plates

  27. Deformation Stycast has frictionless contact with bushing, thus only compressive loading is seen by the Stycast. Upward movement of 1.75 mils. Deflection (x 1e-2 in )

  28. Stress Intensity on pins Very Localized peak stress near the root of the pin, σnom approx 14 ksi

  29. Post testing Observations The analysis underestimated the experimentally observed deflection by a factor of 3.5. Why did this happen?

  30. Post test Pictures Top Pull Plate removed

  31. Pictures of Stycast and bushings Top View: Bushing are not concentric No cracking is seen. ISO view: Large gaps 1/8” are seen in the level of the stycast compared to the sst shim,

  32. Pictures of Stycast and bushings More gap pictures and a view of the relief groove milled into the shim.

  33. Air Bubbles Bubble Bubbles Bubble After removing bottom pull plate and breaking the stycast, Multiple air bubbles were observed throughout the material (largest bubble approx dia = 3/16”)

  34. Gaps Introduced around pins on one side (see pictures above). Modulus reduced by 50% (estimate) to account for bubbles. Resulting Deflection is 7.35 mils Updated Analysis [Model changes to reflect post test observations] No gaps on reverse side gaps

  35. Solutions and Path Forward. • Inject Stycast from the side of each hole (instead of top) using Zerc fittings and hypodermic needle. • Two holes will be drilled to allow for insertion and vacuum pulling of stycast around each bushing. • Deair stycast until bubbling has ceased using vacuum (Use prototype to test Stycast mixture for presence of bubbles) • Limit stirring of Stycast • Test Stycast samples in LN2 environment to test compressive strength.

  36. To ensure a void-free embedment, vacuum deairing should be used to remove any entrapped air introduced during the mixing operation. Vacuum deair mixture at 1-5 mm mercury. The foam will rise several times the liquid height and then subside. Continue vacuum deairing until most of the bubbling has ceased. This usually requires 3-10 minutes. To facilitate deairing in difficult to deair materials, add 1-3 drops of an air release agent, such as ANTIFOAM 88, into 100 grams of mixture. Gentle warming will also help, but working life will be shortened. Appendix: Bubble Solution

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