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HAYNES ALLOY 75

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Journal Articles
Alloy Digest (1999) 48 (7): Ni-557.
Published: 01 July 1999
... Haynes alloy 75 is an 80 nickel-20 chromium alloy with both good oxidation resistance and good mechanical properties at high temperatures. It is amenable to all forms of fabrication and welding. A typical application for sheet metal is fabrications in gas turbine engines. This datasheet provides...
Journal Articles
Alloy Digest (2020) 69 (7): Ni-761.
Published: 01 July 2020
... ATI 75 (UNS N06075) is a nickel-chromium alloy with controlled additions of titanium and carbon; it derives its high temperature strength essentially from solid solution strengthening. This datasheet provides information on composition, physical properties, and tensile properties. It also includes...
Journal Articles
Alloy Digest (1988) 37 (8): Ni-359.
Published: 01 August 1988
... max. 1.00 max. 50.00-55.00 4.75-5.50 0.20-0.80 0.35 max. 0.15 max. 0.15 max. 0.006 max. 0.10 max. 0.35 max. 0.65-1.15 Remainder Physical Constants: Density, lb / cu in. / (At 72°F. aged amdition) g / cu cm (At 72O. aged condition) Thermal coef. expansion /OF (75-200°F) (75~6oOT) (75-1OOOT) (75-14W F...
Journal Articles
Alloy Digest (1963) 12 (11): Cb-6.
Published: 01 November 1963
... - BEARING STRENGTH - Sheet* (0.030 thick) (Effective bearing area taken as product of hole diameter and thickness of test specimen) Test Ultimate Yield Temperature Strength Strength oF psi psi (0.2%) 75 101800 85200 1000 83500 73200 2200 59000 45900 2400 41400 22300 Table 5 - SHEAR STRENGTH - Sheet* (0 030...
Journal Articles
Alloy Digest (1971) 20 (1): Co-62.
Published: 01 January 1971
... Ittdica~ Pa Cent of Cold Reduction 10% 20% 3w 40% 50% 69 71 73 75 76 60 58 54 54 :9 62 59 i: 55 63 58 62 55 ii 58 56 64 65 54 51 62 65 %: 65 65 67 68 67 68 67 69 f: 71 2 69 71 68 70 69 69 74 75 75 72 lti 5 - STRESS-RUPTURE DATA* - Sheet 0.03W.069 in. Thick (Heat treated at 215oOF. wata quenched) Average...
Journal Articles
Alloy Digest (1969) 18 (11): Co-59.
Published: 01 November 1969
... near UTS nil nil 4570 lzod impact. ft. Ibs. funnotched) 5 Rockwell hardness c44 Table 2 - HOT HARDNESS - Sand Cast Test Temperature Brinell* Hardness oF at Temperature 68 445 752 300 932 300 1112 265 1292 ?75 1472 230 1652 180 1832 90 Recovery hardness at room temperature - 445 *Special Brinell...
Journal Articles
Alloy Digest (1961) 10 (3): Ni-64.
Published: 01 March 1961
...-melted, air-cast alloy designated as lnconel 713C alloy by Into. Melting and casting the alloy under vacuum has materially improved its prop- erties. Vacuum-cast parts are capable of meeting a 75 hour minimum life and a 5% minimum elongation when tested at 17OoOF and 30,000 psi. When tested at 1800°F and...
Journal Articles
Alloy Digest (1961) 10 (8): Co-29.
Published: 01 August 1961
... Manganese SiIiCoO olromium Es- Nickel Ocher8 CobsIt NOElid 2.45 1.00 max. 1.00 mas. specific gravity Density, Ib/cu.is. Melting rage, oF Theassl coef. apsssios (me&/OF x IO-6 32- 212oF 32-12920F 32-1832oF 8.38 0.303 22552408 Elecaicsl condaucivig, 75 IACS Elecaicsl resisdvicy, miaohms-cm Moddus of dssticicg...
Journal Articles
Alloy Digest (2020) 69 (10): Ni-763.
Published: 01 October 2020
... International®. All rights reserved. Chemical Composition Element Composition, wt%(a) Haynes HR-224 Haynes 214 Nickel 47(b) 75(b) Cobalt 2 max 2 max Iron 27.5 3 Chromium 20 16 Molybdenum 0.5 max 0.5 max Tungsten 0.5 max 0.5 max Manganese 0.5 max 0.5 max Silicon 0.3 0.2 max Niobium (Columbium) 0.15 max 0.15 max...
Journal Articles
Alloy Digest (2006) 55 (5): Ni-637.
Published: 01 May 2006
... Hydroformed gas turbine component Table 4 Typical Creep Strength, Sheet Approximate initial stress to produce 1% creep in time shown Test temperature 100 h 1000 h °C °F MPa ksi MPa ksi 649 1200 552 80 704 1300 517 75 365 53 760 1400 324 47 241 35 816 1500 221 32 145 21 871 1600 126 18 68 10 927 1700 65 9...
Journal Articles
Alloy Digest (2000) 49 (3): Ni-560.
Published: 01 March 2000
... rupture in time Temperature 10 h 100 h 1000 h °C °F MPa ksi MPa ksi MPa ksi 600 1100 660 96 650 1200 635 92 550 80 705 1300 615 89 515 75 395 57 760 1400 495 72 365 53 240 35 815 1500 345 50 220 32 130 19 870 1600 215 31 125 18 68 9.9 925 1700 120 17.5 66 9.6 Aging treatment is same as that...
Journal Articles
Alloy Digest (1993) 42 (8): Ni-440.
Published: 01 August 1993
... 0.35* Tungsten 3.04.5 3.04.5 others 0.50* 0.50* Physical Constants: Density, lb/cu in. Specific gravity Melting range, F Thermal coef. expansion/ F (75200°F) (751000°F) (75-17OOOF) Thermal conductivity, Btu/sq. ft./hrpF/in. (At -27OOF) (At 0°F) (At 100°F) (At 1000°F) (At 1400°F) (At 2000°F) Electrical...
Journal Articles
Alloy Digest (2004) 53 (6): Ni-621.
Published: 01 June 2004
... annealed hydrofluoric acid, % and heat treated C-22, mill annealed and heat treated 10 4 5 20 20 10 11 73 30 10 12 81 120 h at 38 °C (100 °F) Table 3 Resistance to Chloride-Induced Pitting and Crevice Corrosion. CPT CCT Alloy °C °F °C °F C-22HS, mill annealed and heat treated >100 >212 75 167 C-22 >120...
Journal Articles
Alloy Digest (2004) 53 (7): Ni-622.
Published: 01 July 2004
...% hydrochloric acid, 38 °C (100 °F) <0.1 13.0 29.9 10%hydrochloric acid, 24 °C (75 °F) <0.1 7.4 14.4 To convert mils per year to mm per year, divide by 40. Table 3 Stress-Corrosion Cracking Alloy Time to cracking, h Sanicro 25 36 Alloy G-30 168 Alloy G-35 No cracking after 1008 h ASTM G 36 method (45% magnesium...
Journal Articles
Alloy Digest (1999) 48 (5): Ni-552.
Published: 01 May 1999
... httpwww.haynesintl.com ISSN: 002-614X Ni-552B Table 3 Typical Shielded Metal Arc Welding Parameters (Flat Position) Electrode diameter Arc voltage, V Welding current, A mm in. 22 24 56 75 2.4 3 32 80 100 3.2 18 22 25 125 150 4.0 5 32 24 26 150 180 4.8 316 Polarity is electrode positive. Table 4 Typical Gas Tungsten Arc...
Journal Articles
Alloy Digest (1993) 42 (3): Co-89.
Published: 01 March 1993
...) 827 (119.9) 21.5 *Spray mode Table 5 - LOCALIZED CORROSION: PITTING Critical Pitting Temperature 11.5%HgS0,+1.2%HCl+1%FeC~+1%CuClg 24 Hours Temperature* Alloy C OF c-22m alloy 120 248 ULTIMET alloy 120 248 alloy C-276 110 230 alloy 625 75 167 alloy 6B 45 113 2OCB-3 = alloy 30 86 316L Stainless 25 77...
Journal Articles
Alloy Digest (2018) 67 (3): Ni-742.
Published: 01 March 2018
...) Specific heat capacity, 52 °C (126 °F), J/kg·K (Btu/lb·°F) 414 (0.099) Resistivity, 24 °C (75 °F), m ( circular-mil/ft) 1.14 (686) Coefficient of linear thermal expansion, 24 93 °C (75 199 °F), 10 6/K (10 6/°F) 12.4 (6.9) Thermal conductivity, W/m·K (Btu/ (h·ft·°F)) 48 °C (118 °F) 100 °C (212 °F) 300 °C...
Journal Articles
Alloy Digest (1996) 45 (9): Ni-516.
Published: 01 September 1996
... 2 Unifom Corrosion Resistance ASTM G28A. hoilinga) 26 0.65 250 625 ASTM G28B. boiling(b) 4 0.10 55 137 2o%HF.79T 19 0.47 32 0.80 5O%H$ Oboilin~ 1 0.02 7 0.17 75% H,Po* boiling 33 0.83 51 127 99%amic,hoihg Q.1 8.01 8.1 Co.01 8s%falkboiling 0.4 0.01 1.4 0.03 lO%dlIWiGbC&g 44 1.10 62 155 (a) G28A: I...
Journal Articles
Alloy Digest (1993) 42 (2): Ni-423.
Published: 01 February 1993
.... 75 mi ILS. and 700 mi CO. (pressure at temu Extension Rate: 4 x 10-6/set. 300 350 425 450 . 1 L. . 1 _ Time E / lime A Elongation; /Elongation A ROA EIROAA 1.06 1.06 0.98 1.25 1.16 0.90 1.06 1.05 1.00 1.44 1.00 0.87 Table 9 - C-RING DATA COLD WORKED G-5p ALLOY C-RING RESULTS Actual Stress 100% -No...
Journal Articles
Alloy Digest (2010) 59 (5): Ni-679.
Published: 01 May 2010
... tensile strength, MPa (ksi) Elongation, % RA, % Room temperature 376 (54.5) 851 (123.5) 79 65 93 (200) 334 (48.5) 796 (115.5) 78 71 149 (300) 307 (44.5) 765 (111.0) 76 70 204 (400) 282 (40.9) 745 (108.0) 73 69 260 (500) 263 (38.1) 724 (105.0) 75 69 Note: Data generated from only one plate at 0.5 in. thick...