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Volume 09 - Metallography and Microstructures Part 13 potx

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Fig. 13 Same material, thickness, cold reduction, and annealing as Fig. 12 , then temper rolled (10% additional reduction). Ferrite grains are slightly elongated; some compression is evident at the surface. 3% nital. 100× Fig. 14 Same material, thickness, cold reduction, annealing, and temper-rolling reduction as Fig. 11 , but heated to 940 °C (1725 °F) and held 2 min. The recrystallized ferrite grains are very large. 3% nital. 100× Fig. 15 Same material, thickness, cold reduction, annealing, and temper-rolling treatment as Fig. 13 , but reheated to 940 °C (1725 °F) and held 2 min. Structure: large recrystallized ferrite grains. 3% nital. 100× Fig. 16 3% Si flat-rolled electrical strip (M- 22), cold rolled 70% to 0.6 mm (0.025 in.) thick. Structure is ferrite grains elongated in the direction of rolling. See also Fig. 17. 10% nital. 100× Fig. 17 Same material, thickness, and cold reduction as Fig. 16 , decarburization annealed in moist hydrogen at 815 °C (1500 °F) and annealed for grain growth in dry hydrogen at 870 °C (1600 °F). Compare with Fig. 18 . 10% nital. 100× Fig. 18 3% Si flat-rolled electrical strip (M-22), cold rolled to ~0.6- mm (0.023 in.) (70% reduction), decarburization annealed in moist hydrogen at 815 °C (1500 °F), and annealed in dry hydrogen at 925 °C (1700 °F) for grain growth. Note large ferrite grain size. 10% nital. 100× Fig. 19 3.25% Si cold- rolled electrical strip, 0.3 mm (0.011 in.) thick, annealed at 1175 °C (2150 °F), showing domain structure of (110) [001] oriented materia l with no applied field. The specimen was demagnetized at 60 Hz. Domains reveal where the deviation of [001] direction is not more than 3 or 4° from parallel. As- polished. Magnification not reported Fig. 20 3% Si flat- rolled electrical strip, cold reduced 70% to approximately 0.6 mm (0.025 in.) thick, decarburization annealed in moist hydrogen at 815 °C (1500 °F) and at 1040 °C (1900 °F) in dry hydrogen for grain growth. The ferrite grain size is larger than in Fig. 17 and 18. 10% nital. 100× Fig. 21 3% Si flat- rolled, oriented electrical hot band, as hot rolled. Cross section from near the surface (right) to a depth of approximately 0.5 mm (0.02 in.). Hot finishing temperature was approximately 900 °C (1650 °F). The structure is ferrite grains; note difference in grain shape from near surface to near center. 10% nital. 100× Fig. 22 3% Si flat-rolled orie nted electrical strip, cold reduced 65% and annealed at 925 °C (1700 °F). Structure: recrystallized ferrite grains. The material is ready for final cold reduction and a grain- coarsening anneal. See also Fig. 23 and 24 for effects of further processing. 10% nital. 100× Fig. 23 Same material as Fig. 22 , but given a second cold reduction of 50% to final strip thickness. Ferrite grains are elongated, ready for the grain-coarsening anneal. See also Fig. 24. 10% nital. 100× Fig. 24 Same material and reduction as Fig. 23 after a grain- coarsening box anneal at 1095 to 1205 °C (2000 to 2200 °F) in hydrogen. The upper strip shows portions of two grains; the lower strip, one complete and two partial grains. 10% nital. 100× Fig. 25 3.25% Si flat- rolled, oriented electrical strip, continuously cold rolled to 0.3 mm (0.011 in.) thick, annealed at 1175 °C (2150 °F). Macrograph shows secondary recrystallized ferrite grains with cube-on- edge orientation. 5 mL HCl, 1 mL HF, and 8 mL H 2 O. Actual size Fig. 26 3% Si steel, 0.35 mm (0.014 in.) thick, gradient annealed by heating to 760 °C (1400 °F) in 1 h, then at 65 °C (100 °F) per hour to 1065 °C (1950 °F) at hot end (right) in dry hydrogen and held 3 h. Secondary grain coarsening started at approximately 815 °C (1500 °F). Grain size is typical. 20% HNO 3 , then 20% HCl (alternated). Actual size Fig. 27 3% Si Steel, hot rolled to 0.35 mm (0.014 in.) thick, annealed 24 h at 1150 °C (2100 °F) in dry hydrogen. Note fine, poorly oriented grains, which are parallel to the rolling direction, in a matrix of normal, well-oriented grains. This can result from stringers of inclusions or from rolled-in scale. 5% HF, then 10% HNO 3 . Actual size Fig. 28 3% Si steel, 0.3 mm (0.012 in.) thick, annealed 7.5 h in dry hydrogen at 1175 °C (2100 °F). Specimen shows abnormally small grain size, which indicates poo r orientation. This may be caused by the wrong percentage of cold reduction or by heating too rapidly above 1010 °C (1850 °F). 20% HNO 3 , then 20% HCI (alternated). Actual size Fig. 29 Cubic etch pits in cube-on-face grain- oriented 3% Si steel. The area seen is a single ferrite grain, obtained by annealing at 1175 °C (2150 °F) or higher. Fe 2 (SO 4 ) 3 . 1000× Fig. 30 Scanning electron micrograph of cubic etch pits in cube-on-face grain- oriented 3% Si steel. The area shown is a single grain of ferrite. See also Fig. 29 and 31. Fe 2 (SO 4 ) 3 . 1000× Fig. 31 Etch Pits in a 3% Si steel, showing two orientations. The hexagonal pits have cube-on- corner orientation; the others have cube-on-edge orientations. Fe 2 (SO 4 ) 3 . 1000× Fig. 32 Thermal faceting and pitting of (100) planes of ferrite in 3% Si grain- oriented steel, cold rolled from 0.3 to 0.1 mm thick and annealed 3 h in dry hydrogen at 1205 °C (2200 °F). Thermal etch in hydrogen at 1205 °C (2200 °F).100× Fig. 33 Solenoid- quality type 430FR ferritic stainless steel. Note that some of the ferrite grain boundaries were not revealed. Ralph's reagent. 100× Fig. 34 Fe-30Ni cold- rolled strip, batch annealed 6 h at 950 °C (1740 °F) and furnace cooled in dry hydrogen. Grains are coarse because carbon content was low. HCl, CuCl 2 , FeCl 3 , HNO 3 , methanol, and H 2 O. 100× Fig. 35 Fig. 36 Austenitic Fe-50.5Ni soft magnetic alloy, showing the effects of different etchants. Fig. 35: etched using a flat etchant, glyceregia. Fig. 36: etched using a grain contrast etchant, Marble's reagent. Both 100×. See Fig. 37, 38, 39 for the effects of deformation (cold rolling) and heat treatment on the structure of a similar Fe-50Ni alloy. Fig. 37 Fe-50Ni cold-rolled 0.15-mm strip, annealed 2 h in H 2 at 900 °C and furnace cooled. Structure: primary recrystallized grains of austenite. 60 mL ethanol, 15 mL HCl, and 5 g anhydrous FeCl 3 . 100× Fig. 38 Fe-50Ni cold-rolled 0.03-mm strip, annealed 4 h at 1175 °C (2150 °F) in dry H 2 and furnace cooled. Structure is nonoriented primary recrystallized grains. See also Fig. 39. Saturated (NH 4 ) 2 S 2 O 8 . 100× Fig. 39 Fe-50Ni cold-rolled strip, 0.03 mm (0.014 in.) thick, annealed same as Fig. 38. The structure is comprised of nonoriented secondary recrystallized grains. Thermal etch in hydrogen at 1175 °C (2150 °F). 3× Fig. 40 4-79 Moly Permalloy (4Mo-79Ni-17Fe), cold- rolled strip 0.03 mm (0.014 in.) thick, annealed 4 h in dry hydrogen at 1175 °C (2150 °F) and cooled at 320 °C (575 °F) per hour to room temperature. The structure is coarse-grained austenite. HCl, CuCl 2 , FeCl 3 , HNO 3 , methanol, and H 2 O. 100× Fig. 41 4-79 Moly Permalloy magnetic test-ring specimen taken from 0.3-mm (0.014-in.) thick cold- rolled strip, annealed 4.5 h at 1120 °C (2050 °F) in dry hydrogen. The structure is austenite grains. Marble's reagent. 0.875× Fig. 42 Fe-27Co cold-rolled strip, annealed 2 h in dry H 2 at 925 °C (1700 °F) and furnace cooled. The microstructure is ferrite solid solution. HCl, CuCl 2 , FeCl 3 , methanol, and H 2 O. 100× Fig. 43 Fe-Co-1.9V alloy, annealed 2 h in wet hydrogen at 885 °C (1625 °F). A duplex ferritic grain structure. 2% nital. 50× Fig. 44 Fig. 45 Remendur 27 (Fe-Co-2.8V) wire, 0.5 mm (0.021 in.) in diameter. Structure: α 1 and α 2 phases. Fig. 44: bright-field illumination. Fig. 45: differential interference contrast illumination. 2% nital etches α 1 leaving α 2 in relief. Both 1000× [...]... 3. 5-4 .5 3. 5-4 .5 1. 5-4 .0 0.10 0.20 19, 20, 30, and 31 SAE 792 77.0 min 9. 0-1 1.0 9. 0-1 1.0 0.7 0.50 0.50 0.7 0.40 17, and 18 SAE 793 83.0 min 7. 0-9 .0 3. 5-4 .5 0.5(h) 0.50 0.50 0.7 0.30 23 72. 0-7 6.0 14. 0-1 8.0 9. 0-1 1.0 0.5 0.50 0.50 0.7 0.30 24, 25, 26, 27, 28, and 32 SAE 794 68. 5-7 5.5 21. 0-2 5.0 3. 0-4 .0 0.5(h) 0.50 0.50 0.7 0.40 22 SAE 795 88. 0-9 2.0(i) 0.2 5-0 .7 rem 0.10 0.20 41 88. 0-9 2.0(i) 9. 5-1 0.5... rem 8. 0-1 2.0 0.5 42, 43, 44, 45, 46, 51, 52, 53, 54, 55, 56, and 57 SAE 192 rem 8. 0-1 2.0 1. 0-3 .0 0.5 38, and 39 SAE 193 rem 16. 0-2 0.0 2. 0-3 .0 0.5 83, and 84 SAE 194 rem 5. 0-1 0.0 0.5 Fig Alloy designation Composition, %(a) Cu Pb Sn Ag Zn P Fe Others (total) Others (each) Copper-lead(c) 15, and 16 SAE 48 67. 0-7 4.0 26. 0-3 3.0 0.5 1.5 0.10 0.02 0.7 0.15 12, 13, 14, and 33 SAE 49 73. 0-7 9.0 21. 0-2 7.0... 7, and 8 SAE 13 rem 5. 0-7 .0 9. 0-1 1.0 0.7 0.25 0.10 0.005 0.005 0.05 0.02 3, 4, and 5 SAE 14 rem 9. 0-1 1.0 14. 0-1 6.0 0.7 0.6 0.10 0.005 0.005 0.05 0.02 9, 10, and 11 SAE 15 rem 0. 9-1 .7 13. 5-1 5.5 0.7 0. 8-1 .2 0.10 0.005 0.005 0.02 0.02 40 SAE 16(b) rem 3. 5-4 .7 3. 0-4 .0 0.10 0.05 0.10 0.005 0.005 0.005 0.40 Fig Alloy designation Composition, %(a) designation Pb Sn Cu In Others (total) Plated overlay 36, and. .. 80, and 81 SAE 782 rem 2.73.5 0.30 0. 7-1 .3 0.30 0.71.3 0.15 0.10 64, 65, 66, and 67 SAE 783 rem 17.522.5 0.50 0. 7-1 .3 0.50 0.10 0.15 0.10 68, and 69 SAE 784 rem 0.2 10.012.0 0. 7-1 .3 0.30 0.10 0.03 0.10 70, and 71 SAE 785 rem 0.2 0. 7-1 .3 0. 7-1 .3 0.30 4.55.5 0.30 0.10 72, and 73 SAE 786 rem 37.542.5 0.30 0.30 0.10 74, and 75 SAE 787 rem 0. 5-2 .0 3. 5-4 .5 0.51.0(f) 0.30 4 .09. 0... Trimetal bearing: lead-tin-copper electroplated overlay, copper electroplated barrier, aluminum-silicon-cadmium alloy 5% nital High-tin aluminum alloy clad to nickel-plated steel Lead-base babbitt liner Tin-base babbitt liner Steel backing of any bearing alloy Keller's reagent (a) Lead-tin-copper overlay on aluminum-cadmium alloy Equal parts of concentrated NH4OH and water with 2-4 drops of H2O2 (30%)... material NH4OH and H2O2(a) Commercial bronze liner H2O2(a) Copper-lead alloy liner Copper-lead-tin alloy liner High-leaded tin bronze liner Leaded tin bronze liner Lead-tin-copper overlay on copper-lead alloy liner Nickel bronze infiltrated with lead-base babbitt Nickel-tin bronze infiltrated with lead-base babbitt Silver electroplate on steel Silver-lead alloy electroplate on steel Tin-base babbitt... visible in the microstructures of mixtures containing either element Binary age-hardenable alloys of copper-chromium and copper-beryllium are more resistant to thermal softening than unalloyed copper (see the article "Beryllium-Copper and Beryllium-Nickel Alloys" in this Volume) Several ternary and quaternary alloys, including those that contain cobalt and beryllium, or cobalt, cadmium, and silicon,... 21. 0-2 7.0 0. 6-2 .0 0.7 0.45 34, and 35 SAE 485 rem 44. 0-5 8.0 1. 0-5 .0 0.35 0.45 0.15 Fig Alloy designation Composition, %(a) Al Sn Cd Si Cu Fe Ni Pb Zn Others (total) Others (each) Aluminum base 59 SAE 770 rem 5. 5-7 .0 0.7 0. 7-1 .3 0.7 0.71.3 0.30 0.10 82, 85, 86, and 87 SAE 780 rem 5. 5-7 .0 1. 0-2 .0 0. 7-1 .3 0.7 0.20.7 0.15 0.10 60, 61, 78, and 79 SAE 781(d) rem 0.81.4 3. 5-4 .5 0.050.15... coarser than those in Fig 49 1:1:2 HF, HNO3, and H2O 1000× Fig 51 Macrostructure of Chromindur II (Fe-28Cr-10.5Co) cup-shaped telephone receiver magnets that were deep drawn from 1-mm (0.04-in.) thick strip and solution annealed at (left) 980 °C (1795 °F) and (right) 955 °C (1750 °F) Glyceregia See Fig 52 for a higher magnification view of a deep-drawn and solution-annealed Chromindur II structure A transmission... on copper-lead-tin alloy liner Tin bronze infiltrated with lead-base babbitt Tin bronze infiltrated with Teflon Trimetal bearing: lead-tin-copper electroplated overlay, brass electroplated barrier, copper-lead alloy 0.5% HF Aluminum alloy clad to steel Aluminum-silicon alloy clad to steel High-tin aluminum alloy clad with unalloyed aluminum Lead-tin-copper overlay on aluminum alloy liner Low-tin aluminum . the 600-grit paper in grinding and on the percentage of tungsten in the specimen, rapid rough polishing can begin with 1 5- or 9- m diamond paste and can proceed in steps through 6- and 3- m pastes examples are copper-tungsten and copper-graphite mixtures as well as silver- graphite, silver-cadmium oxide, and silver-nickel combinations. These materials often are examined in the as-polished (not. min. Microstructures of Electrical Contact Materials The electrical contact materials depicted in this article include copper-, silver-, tungsten-, tungsten-carbide-, and molybdenum-base materials,

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Tài liệu tham khảo Loại Chi tiết
1. T.J. Bertone, The Metallographic Sample Preparation of Fiber-Reinforced Composites, in Metallographic Specimen Preparation, Optical and Electron Microscopy, J.L. McCall and W.M. Mueller, Ed., Plenum Press, 1974, p 251-273 Sách, tạp chí
Tiêu đề: Metallographic Specimen Preparation, Optical and Electron Microscopy
2. Personnel of the Metallographic Laboratory, Materials and Process Engineering, General Dynamics Convair, San Diego, private communication, Feb 1985 Khác
3. J.E. Zimmer, Acurex Aerotherm, Mountain View, CA, private communication, Feb 1985 4. G. Shaw, Midwest Research Institute, Kansas City, private communication, Feb 1985 Khác
5. D.L. Dozer, Lockheed Missiles and Space Co., Sunnyvale, CA, private communication, Jan 1985 Khác
12. F.I. Hurwitz, NASA Lewis Research Center, Cleveland, private communication, April 1985 13. W. Stuckey, The Aerospace Corp., El Segundo, CA, private communication, Jan 1985 Macroexamination Khác

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