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C55

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Journal Articles
Alloy Digest (2022) 71 (3): CS-219.
Published: 01 March 2022
... 1055, C55, C55E, and C55R are wrought medium-carbon non-alloy steels that are used in the normalized, cold worked, quenched and tempered, or austempered condition. 1055, C55E, and C55R may also be flame or induction hardened. These steels are widely used for moderately and highly stressed parts...
Journal Articles
Alloy Digest (2023) 72 (9): CS-258.
Published: 01 September 2023
... 1055, C55, C55E, and C55R are wrought medium-carbon (carbon = 0.50–0.60%) non-alloy steels that are used in the normalized, cold worked, quenched and tempered, or austempered condition. 1055, C55E, and C55R may also be flame or induction hardened, nitrided, or nitrocarburized. These steels...
Journal Articles
Alloy Digest (2021) 70 (9): CS-212.
Published: 01 September 2021
... Lucefin C55, C55E, and C55R are medium-carbon, non-alloy steels that are used in the normalized, cold worked, or quenched and tempered condition. C55E and C55R may also be flame or induction hardened. C55, C55E, and C55R are used for applications where the higher carbon is needed to improve wear...
Journal Articles
Alloy Digest (1962) 11 (2): TS-115.
Published: 01 February 1962
... 185OoF and double tempered. Button head specimens ritk a 0.160 diameter and . 1 eaee lenarh.1 Test Tempcrsture Stress, psi to Ruptute io OF 10 Hours 100 Hours 1000 Hosts - - Tempered to Rockwell C55-56 800 258000 250000 232000 900 240000 21ww 14WOO 1600 172000 Tempered to Rockwell C51-52 $i 214000...
Journal Articles
Alloy Digest (1963) 12 (1): Ni-78.
Published: 01 January 1963
... heat, Btu/lb./oF (77-2120F) 0.109 Note: The term Colmonoy and Sprayweld are registered trade marks of Wall Colmonoy Corporation. Table 2 - ELEVATED TEMPERATURE ROCKWELL HARDNESS Test Temperature Oxy-Acetylene oF Welded Deposit 600 C55 800 C52 1000 C48 1200 c44 Spraywelded Deposit c55 C52 C48 C44...
Journal Articles
Alloy Digest (1963) 12 (2): Fe-22.
Published: 01 February 1963
... Incremental permeability (approx.) 10.5 Table 2 - TYPICAL MECHANICAL PROPERTIES Tensile strength, psi 125000 Rockwell hardness c55 Heat Treatment: Anneal: Heat to 12000C (Zl%!OF), quench in oil. Magnetic Heat Treatment (Anneal): Heat to 12000C (2192oF), quench in oil, temper for 2 hours at 6500C (1202oF...
Journal Articles
Alloy Digest (1959) 8 (9): SS-93.
Published: 01 September 1959
... TREATED PROPERTIES (Oil quenched from 1900°F.) Drawn at 600°F. Full Range Tensile strength, psi 285000 100000 - 285000 Yield strength, psi (0.2%) 275000 60000 - 275000 Elongation, % in 2 2.0 8-l Reduction of area, % 10.0 Brine11 hardness 580 200-600 Rockwell hardness C55 - 56 B95 - C58 Table 7 -EFFECT...
Journal Articles
Alloy Digest (1961) 10 (7): Co-28.
Published: 01 July 1961
... x 3/8 specimen, 1% span) 60,000-65,000 o-1 300,000-340,000 c55-63 7,000-8,000 * Investment cast ** Permanent mold cast The properties are regulated by pouring temperature and the chill or cooling rate of the casting. The size or volume of the casting obviously controls the rate of cooling. A fast...
Journal Articles
Alloy Digest (1965) 14 (1): TS-157.
Published: 01 January 1965
... and double tempered 2 t 2 hours at 6000F) Tensile strength, psi 293000 Yield strength, psi (0.2%) 265000 Elongation, % in 2 Reduction of area, % l Rockwell hardness c55 Static bend, psi 660000 Charpy impact (unnocched) ft. Ibs. 120 Farigue strength, psi (1 x 106 cycles) Fatigue strength, psi (100 x 10...
Journal Articles
Alloy Digest (1967) 16 (3): CS-27.
Published: 01 March 1967
... in oil and C55-60 in water. Temper after treatment.) As Rolled Hot Rolled 106000 62000 16 35 Cold Drawn 118000 !14000 :8 Table 3 - TYPICAL HEAT TREATED PROPERTIES (1, dia. bar, water hardened) Tempering Tensile Yield Reduction Temperature Strength Point Elongation of Area OF psi psi % in 2 % 300 265000...
Journal Articles
Alloy Digest (1964) 13 (11): TS-154.
Published: 01 November 1964
...) Tensile strength, psi 292500 Yield strength, psi (0.2%) 264300 Elongation, % in 2 1 Reduction of area, % 2.2 Rockwell hardness C55 Static bend, psi 660000 Charpy impact (unnotched) ft. lbs. 120 Fatigue strength, psi (I x 106 cycles) 145000 Fatigue strength, psi (100 x 106 cycles) 120000 Table 2 - EFFECT...
Journal Articles
Alloy Digest (1968) 17 (5): TS-205.
Published: 01 May 1968
... cooled from 1000°C and tempered at 540°C) Tensile strength, psi 280000 Yield strength, psi (0.2%) 216000 Elongation, % in 2 1 Reduction of area, % 0.2 Rockwell hardness c55 Table 3 - TYPICAL COMPRESSION PROPERTIES (Air cooled from 1020°C and tempered to Rockwell C60) Yield strength, psi at 0.01% offset...
Journal Articles
Alloy Digest (1966) 15 (7): Ni-114.
Published: 01 July 1966
... Tensile strength, psi 170000-190000 (Fully heat rreated coaditioo) Yield strength, psi (0.2%) 160000-180000 Test Temperature Rockwell Elongation, % io 2 1-2 OF Hardness Rockwell hardness C48-52 R.T. C55 100 c54 200 c53 400 C52 600 c50 800 C48 1000 c45 1200 A56 1300 A45 1400 A36 Table 2 - TYPICAL SHORT...
Journal Articles
Alloy Digest (1968) 17 (9): Ni-138.
Published: 01 September 1968
... Rockwell hardness B97 c55 Izod impact, ft. lbs. 3.75 Notch tensile strength, psi 190000 Table 2 - TYPICAL ELEVATED TEMPERATLJRE PROPERTIES (Precision cast, solution annealed and age hardened) Test Tensile Yield Temperature Strength Strength OF osi psi (0.2%) Elongation % in 2 200 220000 210000 2 400...
Journal Articles
Alloy Digest (1955) 4 (11): SS-36.
Published: 01 November 1955
... deg. F. per hour, then cool in air, oil or water to 190-2 15 BrinelL HARDEN: Firsr preheat slowly to 1450 deg. F. and soak, then raise temperature to 1850-1950 deg. F., quench in warm oil or air to C55-58 Rockwell, temper immediately to desired hardness. (Do not overheat, because full hardness cannot...
Journal Articles
Alloy Digest (1976) 25 (6): TS-302.
Published: 01 June 1976
... by merely heating with an oxyacetylene torch for a few seconds (long enough to heat the surface to a cherry red color, about 15000F). No quenching is required. The portion of the steel heated will harden to Rockwell C55-60 because of the rapid cooling produced by the conduction of heat from the small heated...
Journal Articles
Alloy Digest (1955) 4 (12): SS-38.
Published: 01 December 1955
... at 1550.1650 F., soak and cool slowly in furnace to 1000-1200°F. at rate of 20.50°F. per hour, then cool in air, oil or water to 190-215 Brinell. Harden: First preheat slowly to 1450 F. and soak, then raise temperawe to 1850-1950 F., quench in warm oil or air. The resulting hztdness is up to C55-58 Rockwell...
Journal Articles
Alloy Digest (1968) 17 (10): SS-215.
Published: 01 October 1968
... Brinell. Harden: First preheat slowly to 1400-145OOF and soak, then raise temperature to 1850-1950 F, quench in warm oil or air to C55-58 Rockwell, temper immedi- ate11 at 300-800°F to desired hardness. (Do not overheat, because full hardness cannot be obtained and rhe steel becomes non-magnetic when over...
Journal Articles
Alloy Digest (1969) 18 (4): SS-223.
Published: 01 April 1969
... 587-600 Brinell hardness 555 400 56-57 560-573 Izod impact, ft. Ibs. (V-notch) 2-5 500 53-54 522-534 Rockwell hardness c55 600 53 522 700 54 534 800 54 534 Table 3 - TYPICAL MECHANICAL PROPERTIES - Wire (0.250 inch diameter) Annealed Bright Soft Tensile strength, psi 107000 115000 Yield strength, psi...
Journal Articles
Alloy Digest (1968) 17 (1): TS-201.
Published: 01 January 1968
... 7.793 6.68 7.11 1505 30 23.0 0.11 OF 200 Table 6 - TYPICAL STRESS-RUPTURE PROPERTIES (Air cooled from 1850oF mad double tempered. Button bead s~ecimms with a 0.160 diameter m-d. 1 pge length.) Tesl Tempermurc Stress, psi to Rupture io OF 10 Hoors 100 Hours loo0 Hoors -- Tempered to Rockwell C55-56 800...