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CYCLOPS N-9

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Journal Articles
Alloy Digest (1958) 7 (6): TS-71.
Published: 01 June 1958
... CYCLOPS N-9 is a chromium-nickel oil hardening steel with high toughness and fatigue resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on forming, heat...
Journal Articles
Alloy Digest (1981) 30 (1): TS-375.
Published: 01 January 1981
... Type L6. UNS No. T61206. General Characteristics: Cyclops L-6 is a low-ahoy, special-purpose nickel- chromium-molybdenum tool steel of medium harden- ability and great toughness. It was formerly Cyclops N-9 (Alloy Digest, TS-71, June 1958). It is a shock- resisting, oil-hardening grade but parts up...
Journal Articles
Alloy Digest (1971) 20 (12): Fe-48.
Published: 01 December 1971
... UNITEMP N-155 is an iron-base austenitic alloy used over a wide temperature range from subzero to about 1800 or 1900 F. It has relatively good oxidation and corrosion resistance. It is used in such applications as turbine rotors, shafts and blades, afterburner parts, nozzles and combustion...
Journal Articles
Alloy Digest (1971) 20 (9): SS-260.
Published: 01 September 1971
... 66 9 - .4luminum sulfate, 10%. bcJingl days Nil 51 - 468 altog , ;d&iga 9 0.6 a3 0.5 2-m 30%. 7w. 7 days 7.1 1.4 4o%, 7ov. 7 days 6.3 4.7 :: i2 I 4O%. 122°F. 7 days 590 386 so+ Fe2 (SO4) 3 + 50% H2SO4. boil, 120 hoam 15 23 18 157 Phosphmic acid 50%. 75oF. 7 dsyr Nil 0.8 - 10 5o%.boib& dws 0.8 9% 4.5...
Journal Articles
Alloy Digest (1954) 3 (3): TS-18.
Published: 01 March 1954
... AND ALLOYS Publisbcd by Eogineaing Alloys Digesf Inc upper W New J-w CARPENTER No. S-876 (A TOUGH, OIL-HARDENING. TRWLE ALLOY RYRELI CARPENTER No. 5-876 is a oidd~tium-1001~coum triple alloy steel for hard-tanpcrcd and for tough-tapered ap piications. It is a cold melt, +n cootrolled, ckctric furnace steel...
Journal Articles
Alloy Digest (1963) 12 (10): Ni-87.
Published: 01 October 1963
.../asm.ad.ni0087 Copyright © ASM International® 1996 Table 5 - TYPICAL TENSILE AND IMPACT PROPERTIES (5.?8 round hot rolled bar) Test Yield Srrennrh Tensile Strength Dsi 14oooF-16 235500 220500 213500 206000 200000 Reduction of Area n A (Rc 40-42) 16.5 17.5 21.0 23.5 23.5 Chnrpy Impact V-Notch ft. Ibs. Temperarue...
Journal Articles
Alloy Digest (1954) 3 (10): SS-19.
Published: 01 October 1954
...-0.80 a . apansion/ F 18.00-20.00 70 to -1SO F Nidcel 8.00-11.00 70 to 2OO F MO- TW3-J :EE: 70 o .WOO°F Columbium + Ta ois:o:6o ThamaI cony$-n+ =U/H/idW F Titanitlm 0.50 max. at 1112 F xton Remainder Modulus of eiascicicy, psi Modulus of rigidity, psi Table 1 - TYPICAL TENSILE PROPERTIES-ROOM...
Journal Articles
Alloy Digest (1959) 8 (12): TS-87.
Published: 01 December 1959
... marked hardness and brittleness in the fusion zone. Specification Equivalents: AISI Type L6 Fig? BetMeheol Allegheny Ludlum ElpaIOY e Tough No. 4 EFsE Jessop Universal-Cyclops General Characteristics: N&o-M is a chromium-nickel-molybdenum tool steel con- taining 0.70% carbon. This is a deep hardening...
Journal Articles
Alloy Digest (1967) 16 (11): Ni-129.
Published: 01 November 1967
...-RUPTURE PROPERTIES Test TetXile Yield Reduction (Age-hardened condxtion) Tempera-e strength Strength Elongation of Area Test Stress, psi to Produce Rupture OF psi psi (0.2%) % in 2. -0 remperature SWeSS Time Elongation - - 78 195000 122000 28 28 CF hours -- psi n -104 203000 132000 24 26 1350 70000 48 8...
Journal Articles
Alloy Digest (1956) 5 (5): TS-46.
Published: 01 May 1956
... 46.0-47.0 Table 2 - TYPICAL TENSILE PROPERTIES - WATER HARDENED bars were head for 1 hour M 1650°F.. warer quenched, then tempered 2 hours at mperature). Tensile Suengrb Yield Point mqyie2:n adutioP Area Brinell Pi HdlESS ::o 27.0 28.5 E lizi 270000 10.5 38.5 532 213000 203000 11.5 29.5 444 T-puing...
Journal Articles
Alloy Digest (1956) 5 (7): TS-48.
Published: 01 July 1956
... cvdaess _- _ 337000 67.0 9 :!I: 314000 35 298000 %t 2~8~ 10 54:o :: :3-i 800 253000 so:0 900 238000 10.5 1000 1100 %E :: 1200 185000 14 HARDNESS VERSUS TEMPERING (Specimens W dia ~~b:el?n~quencbed in oil from 1750°F. and tempered for 1 hour). Tempering Temperature, OF. Rockwell Hardness, c None 61 E...