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AISI 1065

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Journal Articles
Alloy Digest (1976) 25 (10): CS-63.
Published: 01 October 1976
... AISI 1065 is a high-carbon oil-hardening machinery and tool steel of low hardenability. It is used for springs, hand tools, machinery parts, shafts and many machine tools requiring strength and wear resistance. This datasheet provides information on composition, physical properties, hardness...
Journal Articles
Alloy Digest (1988) 37 (1): CS-118.
Published: 01 January 1988
... ordinary temperatures. Specification Equivalents: AISI 1065. QQ-S-633. QQ-S-00640 (Army Ord). General Characteristics: Because of its low hardenability, SAE 1065 can be hardened fully by oil quenching only in very thin sections. Only partial hardening can be achieved in heavier sections but the increase in...
Journal Articles
Alloy Digest (2010) 59 (5): SS-1065.
Published: 01 May 2010
... properties, hardness, and tensile properties. It also includes information on corrosion resistance as well as casting and joining. Filing Code: SS-1065. Producer or source: Kubota Metal Corporation, Fahramet Division. Producer or Source: Kubota Metal Corporation, Fahramet Division Copyright © ASM...
Journal Articles
Alloy Digest (1993) 42 (11): TS-521.
Published: 01 November 1993
... THYRODUR 2510 (AISI D2) is an oil hardening, non-shrinking die steel which can be hardened at relatively low temperatures. The alloy exhibits excellent wear resistance. This datasheet provides information on composition, physical properties, and hardness. It also includes information on heat...
Journal Articles
Alloy Digest (2001) 50 (9): TS-590.
Published: 01 September 2001
... Lanark is a silicon-manganese shock resistant tool steel with highest impact strength of the AISI S type tool steels. It is used for pneumatic tools, shear blades, and mandrels. This datasheet provides information on composition, physical properties, hardness, and elasticity. It also includes...
Journal Articles
Alloy Digest (2011) 60 (10): SS-1103.
Published: 01 October 2011
... ATI 50 Alloy is an austenitic stainless steel strengthened with nitrogen. It is superior to AISI Type 316L in both strength and corrosion resistance. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on corrosion...
Journal Articles
Alloy Digest (1997) 46 (9): SS-418.
Published: 01 September 1997
... Project 70 and Project 7000 Type 304 stainless steel are versions of conventional AISI Type 304 (18Cr-8Ni) stainless steel having improved machinability and higher tensile and creep strengths. This datasheet provides information on composition, physical properties, hardness, elasticity, and...
Journal Articles
Alloy Digest (2003) 52 (1): SS-872.
Published: 01 January 2003
... AK Steel Type 316L is a Cr-Ni-Mo steel with a very low carbon content (0.03 max). Its general resistance to corrosion is similar to AISI Type 316 (see Alloy Digest SS-865, October 2002) but, because of its low carbon content, it has superior resistance to the formation of harmful carbides that...
Journal Articles
Alloy Digest (1984) 33 (7): TS-425.
Published: 01 July 1984
... VascoJet 2000 was developed to meet the needs of the aerospace industry. It also has been used for special tooling applications. It is a vacuum-melted modification of AISI H12 hot-work die steel. VascoJet 2000 has a tensile strength of 200,000 psi (1500 MPa) at room temperature and exceptional...
Journal Articles
Alloy Digest (1988) 37 (8): SS-497.
Published: 01 August 1988
... Treatment: Solution Treating: AL 174 precipitation Hardening Alloy is furnished in the annealed (solution treated) condition which consists of air cooling from 1900-1950°F (1040-1065°C) to room temperature. precipitation Hardening: A high degree of strengthening is ohtnincd bv aging for ahjut 1 hour at WWF...
Journal Articles
Alloy Digest (1989) 38 (7): SS-509.
Published: 01 July 1989
... from 19502000°F (1065-1090°C). Stress relieving may be accomplished at 400-800°F (205-425 C) and cooling at any desired rate. Hot workability of these steels is good. Forge in the range 2300- 17OO F (1260-930°C). Annealing is recommended following forging for best corrosion resistance. Cold workability...
Journal Articles
Alloy Digest (1990) 39 (8): SS-514.
Published: 01 August 1990
... treatment. To anneal, rapid air cool or water quench from 1950- 205O F (1065-1121 C). Machinability: UNS S31600 steel has a machinability rating about 60% that of AISI carbon steel when machined at a speed of 100 sfrn using high-speed steel tooling. To avoid chatter, tooling and futures must be rigid...
Journal Articles
Alloy Digest (1995) 44 (12): SS-627.
Published: 01 December 1995
... joinability physical properties Sandvik 5R60 tensile properties workability thermal properties UNS S31600 S31609 - DIGEST k SANDVIK 5R60 Filing Code: SS-527 Stainless Steel (AM Type 316) DECEMBER 1995 DATA ON WORLD WIDE METALS AND ALLOYS Sandvik 5R60 (AISI Type 316) fUMedby: AUoyDige~t. lml2O1~77...
Journal Articles
Alloy Digest (1988) 37 (6): SS-496.
Published: 01 June 1988
... transformation. Within 1 hour cool to 55 F (lSsC)/hold M hour, minimum. Precipitation harden 1050° F (565 C)/ I % hours /cool to room temperature. Tensile strength typically 2lOOOO psi (1450 MPa). *Initially Condition A (mill annealed 195O F (1065 C)/cooled rapidly to room temperature. Structure essentially...
Journal Articles
Alloy Digest (2012) 61 (5): TS-702.
Published: 01 May 2012
... due to uneven heating. Austenitizing. Hardening range 1065 1150 ºC (1950 2100 ºF). Ramp rapidly to 1120 ºC (2050 ºF). Holding time after tool or part is heated fully through at austenitizing temperature: minimum of 30 minutes, maximum 1 hour. Alternatively, hold 20 minutes for the first inch (25.4 mm...
Journal Articles
Alloy Digest (1969) 18 (2): Al-184.
Published: 01 February 1969
...-6 Titanium 0.20 max. 68-392OF 12.9 x 1O-6 Others, each 0.05 max. 1065-I 170 , total Solidification range, OF 0.15 max. 10.3 x 106 Aluminum Remainder Modulus of elasticity, psi Electrical resistivity, microhm-cm 4.1 (When in the form of welding elec- trode the Be content will be 0.0008 mad PROPERTIES...
Journal Articles
Alloy Digest (1983) 32 (8): Ni-290.
Published: 01 August 1983
...%) Physical Constants: Chromium Boron Carbon Nickel 14.5-16 3.17-4.2 0.06 max. Remainder Density, lb/cu in. 0.295 Specific gravity 8. I6 Melting point, F ( C) (Liquidus) 1950( 1065) (Solidus) 1870( 1020) Structure as supplied Metallic glass (Amorphous) Cooling rate to produce, o F/set, minimum 1.8x IOr...
Journal Articles
Alloy Digest (1999) 48 (1): SS-736.
Published: 01 January 1999
...) Abrasive(b) CPM 420V 55 56 Hardened at 1065 °C (1950 °F) 30 22 30 35 55 65 57 Hardened at 1120 °C (2050 °F), double tem- pered 315 °C (600 °F) 16 12 35 40 50 60 CPM 440V 55 Hardened at 1065 °C (1950 °F) 24 18 15 25 70 85 58 Hardened at 1120 °C (2050 °F), double tem- pered 315 °C (600 °F) 17 13 20 30 60 70...
Journal Articles
Alloy Digest (2005) 54 (4): TS-562.
Published: 01 April 2005
... H13 1010 1850 45 237(c) 175(c) O1 800 1475 60 41 30 A2 955 1750 60 53 40 2 3 D2 1010 1850 60 28 21 3 4 CPM 3V 1065 1950 60 95 70 7 (a) Austenitized at temperature indicated and tempered to hardness. (b) Crossed cylinder adhesive wear test; higher number = better wear resistance. (c) H13 impact...
Journal Articles
Alloy Digest (2001) 50 (3): SS-820.
Published: 01 March 2001
... be a problem in corrosion environ- ments, use the lower carbon grade of the alloy, unless the welded assembly can be heated to 1040 °C (1900 °F) and water quenched. Although it is recommended that welding should be done with electrodes of the same composition, electrodes of AISI type 310 stainless...