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1、MATERIALS SELECTIONECONOMIC, ENVIRON., & DESIGN ISSUESISSUES TO ADDRESS. Price and availability of materials. How do we select materials based on optimal performance? Applications: -shafts under torsion -bars under tension -plates under bending -materials for a magnetic coil.MATERIALS SELECTIONECONO

2、MIC, Chapter 22-2 Current Prices on the web(a): -Short term trends: fluctuations due to supply/demand. -Long term trend: prices will increase as rich deposits are depleted. Materials require energy to process them:-Energy to produce materials (GJ/ton)Al PET Cu steel glass paper237 (17)(b) 103 (13)(c

3、) 97 (20)(b) 20(d) 13(e) 9(f) -Cost of energy used in processing materials ($/GJ)(g) elect resistance propane natural gas oil25 11 9 8 a http:/www.statcan.ca/english/pgdb/economy/primary/prim44.htm a b /recyclability.htm c /profchm/escalant.html d .facts/power/energy.htm e /EE/industry_glass.html f

4、http:/www.aifq.qc.ca/english/industry/energy.html#1 g /consumerinfo/rebriefs/cb5.htmlEnergy using recycled material indicated in green.PRICE AND AVAILABILITYChapter 22-2 Current Prices Chapter 22-3 Reference material: -Rolled A36 plain carbon steel. Relative cost, $, fluctuates less over time than a

5、ctual cost.Based on data in Appendix C, Callister, 6e. AFRE, GFRE, & CFRE = Aramid, Glass, & Carbon fiber reinforced epoxy composites.RELATIVE COST, $, OF MATERIALSChapter 22-3 Reference materi4 Bar must not lengthen by more than d under force F; must have initial length L. Maximize the Performance

6、Index:- Stiffness relation: - Mass of bar: (s = Ee) Eliminate the free design parameter, c:specified by applicationminimize for small M(stiff, light tension members)STIFF & LIGHT TENSION MEMBERS4 Bar must not lengthen by m5 Bar must carry a force F without failing; must have initial length L. Maximi

7、ze the Performance Index:- Strength relation: - Mass of bar: Eliminate the free design parameter, c:specified by applicationminimize for small M(strong, light tension members)STRONG & LIGHT TENSION MEMBERS5 Bar must carry a force F w6 Bar must carry a moment, Mt ; must have a length L. Maximize the

8、Performance Index:- Strength relation: - Mass of bar: Eliminate the free design parameter, R:specified by applicationminimize for small M(strong, light torsion members)STRONG & LIGHT TORSION MEMBERS6 Bar must carry a moment, MChapter 22-DATA: STRONG & LIGHT TENSION/TORSION MEMBERSIncreasing P for st

9、rong tension members Increasing P for strong torsion members 0.1 1 10 3 0 1 10 10 2 10 3 10 4 Density, r (Mg/m 3 ) Strength, s f (MPa) slope = 1 0.1 Metal alloys Steels Ceramics PMCs Polymers | grain grain wood Cermets slope = 3/2 7Adapted from Fig. 6.22, Callister 6e. (Fig. 6.22 adapted from M.F. A

10、shby, Materials Selection in Mechanical Design, Butterworth-Heinemann Ltd., 1992.) Chapter 22-DATA: STRONG & LIGChapter 22-0.1 1 10 3 0 0.1 1 10 10 2 10 3 10 4 Cermets Steels Density, r (Mg/m 3 ) Strength, sf (MPa) slope = 2 Increasing P for strong bending members Metal alloys Ceramics PMCs Polymers

11、 | grain grain wood 8 Maximize the Performance Index:Adapted from Fig. 6.22, Callister 6e. (Fig. 6.22 adapted from M.F. Ashby, Materials Selection in Mechanical Design, Butterworth-Heinemann Ltd., 1992.) DATA: STRONG & LIGHTBENDING MEMBERSChapter 22-0.1 1 10 3 0 Chapter 22-9 Other factors: -require

12、sf 300MPa. -Rule out ceramics and glasses: KIc too small. Maximize the Performance Index: Numerical Data: Lightest: Carbon fiber reinf. epoxy (CFRE) member. material CFRE (vf=0.65) GFRE (vf=0.65) Al alloy (2024-T6) Ti alloy (Ti-6Al-4V) 4340 steel (oil quench & temper)r (Mg/m3) 1.5 2.0 2.8 4.4 7.8 P

13、(MPa)2/3m3/Mg) 73 52 16 15 11Data from Table 6.6, Callister 6e. tf (MPa) 1140 1060 300 525 780 DETAILED STUDY I: STRONG, LIGHT TORSION MEMBERSChapter 22-9 Other factors: Chapter 22-10 Minimize Cost: Cost Index M$ $/P (since M 1/P) Numerical Data: Lowest cost: 4340 steel (oil quench & temper) materia

14、l CFRE (vf=0.65) GFRE (vf=0.65) Al alloy (2024-T6) Ti alloy (Ti-6Al-4V) 4340 steel (oil quench & temper)$ 80 40 15 110 5P (MPa)2/3m3/Mg) 73 52 16 15 11($/P)x100 112 76 93 748 46 Need to consider machining, joining costs also. Data from Table 6.7, Callister 6e. DETAILED STUDY I: STRONG, LOW COST TORS

15、ION MEMBERSChapter 22-10 Minimize Cost:Chapter 22-11 Background(2): High magnetic fields permit study of: -electron energy levels, -conditions for superconductivity -conversion of insulators into conductors. Largest Example: -short pulse of 800,000 gauss (Earths magnetic field: 0.5 Gauss) Technical

16、Challenges: -Intense resistive heating can melt the coil. -Lorentz stress can exceed the material strength. Goal: Select an optimal coil material.(1) Based on discussions with Greg Boebinger, Dwight Rickel, and James Sims, National High Magnetic Field Lab (NHMFL), Los Alamos National Labs, NM (April

17、, 2002). (2) See G. Boebinger, Al Passner, and Joze Bevk, Building World Record Magnets, Scientific American, pp. 58-66, June 1995, for more information.Pulsed magnetic capable of 600,000 gauss field during 20ms period.Fractured magnet coil. (Photos taken at NHMFL, Los Alamos National Labs, NM (Apr.

18、 2002) by P.M. Anderson) DETAILED STUDY II: OPTIMAL MAGNET COIL MATERIALChapter 22-11 Background(2):Chapter 22-12 Applied magnetic field, H:H = N I/L Lorentz hoop stress: Resistive heating: (adiabatic)temp increase during current pulse of DtMagnetic field points out of plane.elect. resistivityspecif

19、ic heatLORENTZ STRESS & HEATINGChapter 22-12 Applied magnetChapter 22-13 Mass of coil:M = rdAL Eliminate free design parameters A, I from the stress & heating equations (previous slide): Applied magnetic field:H = N I/L-Stress requirement specified by applicationPerformance Index P1: maximize for la

20、rge H2/Mspecified by applicationPerformance Index P2: maximize for large Ht1/2/M-Heating requirement MAGNET COIL: PERFORMANCE INDEX Chapter 22-13 Mass of coil:MChapter 22-14 Relative cost of coil:$ = $ M Eliminate M from the stress & heating equations: Applied magnetic field:H = N I/L-Stress require

21、ment specified by applicationCost Index C1: maximize for large H2/$specified by applicationCost Index C2: maximize for large Ht1/2/$-Heating requirement MAGNET COIL: COST INDEX Chapter 22-14 Relative cost Chapter 22-15 Data from Appendices B and C, Callister 6e:Material 1020 steel (an) 1100 Al (an)

22、7075 Al (T6) 11000 Cu (an) 17200 Be-Cu (st) 71500 Cu-Ni (hr) Pt Ag (an) Ni 200 units sf 395 90 572 220 475 380 145 170 462 MPa rd 7.85 2.71 2.80 8.89 8.25 8.94 21.5 10.5 8.89 g/cm3 $ 0.8 12.3 13.4 7.9 51.4 12.9 1.8e4 271 31.4 - cv 486 904 960 385 420 380 132 235 456 J/kg-K re 1.60 0.29 0.52 0.17 0.57 3.75 1.06 0.15 0.95 W-m3 P1 50 33 204 25 58 43 7 16 52 sf/rd P2 2 21 15 5 3 1 19 1 2 (cv/re)0.5 rd C1 63 3 15 3 1 3 1 1 2 P1/$ C2 2.5 1.7 1.1 0.6 0.1 0.1 0.1 0.1 0.1 P2/$ Avg. values used. an = annealed; T6 = heat treated & aged; st = solution heat treated; hr = hot rolled Lightest for

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