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G-E ALLOY P-6

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Journal Articles
Alloy Digest (1959) 8 (11): Co-18.
Published: 01 November 1959
... G-E ALLOY P-6 is a carbon-free permanent magnet material which, when properly heat-treated, exhibits a high residual induction, high permeability, and high hysteresis loss characteristics. This datasheet provides information on composition and physical properties. It also includes information on...
Journal Articles
Alloy Digest (1963) 12 (6): Co-19.
Published: 01 June 1963
... G-E ALLOY X-63 is a cobalt-base alloy having excellent oxidation and corrosion resistance. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high...
Journal Articles
Alloy Digest (1990) 39 (7): Cp-16.
Published: 01 July 1990
... Source: G. E. Plastics Copyright © ASM International® 1996 1996 ASM International compressive strength corrosion-resistant alloys fracture toughness hardness military electrical components physical properties shear strength tensile properties ULTEM 6100 ULTEM 6200 ULTEM 6202 y= s...
Journal Articles
Alloy Digest (1992) 41 (3): P-33.
Published: 01 March 1992
... provides information on composition, physical properties, hardness, tensile properties, and compressive strength as well as fracture toughness. It also includes information on wear resistance as well as casting and powder metal forms. Filing Code: P-33. Producer or source: G. E. Plastics. Producer or...
Journal Articles
Alloy Digest (1992) 41 (3): Cp-21.
Published: 01 March 1992
... properties, and compressive and shear strength as well as fracture toughness. It also includes information on wear resistance. Filing Code: Cp-21. Producer or source: G. E. Plastics. Producer or Source: G. E. Plastics Copyright © ASM International® 1996 1996 ASM International coefficient of...
Journal Articles
Alloy Digest (1990) 39 (5): P-13.
Published: 01 May 1990
... and shear strength as well as fracture toughness. Filing Code: P-13. Producer or source: G. E. Plastics. Originally published December 1989, revised May 1990. Producer or Source: G. E. Plastics Copyright © ASM International® 1996 1996 ASM International compressive strength fracture...
Journal Articles
Alloy Digest (1989) 38 (6): P-5.
Published: 01 June 1989
... industrial products. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well asfracture toughness and fatigue. Filing Code: P-5. Producer or source: G. E. Plastics. Producer or Source: G. E. Plastics...
Journal Articles
Alloy Digest (1990) 39 (2): Cp-5.
Published: 01 February 1990
... ULTEM 2300 ULTEM 2400 viscosity ULTEM2100,2200,2300&2400 Q-5 -DIGEST FEBRUARY 1990 - DATA ON WORLD WIDE METALS AND ALLOYS p-12 -Yeyp - PutJishedby: AbytJQal.In~1291-677.9161 e+leddmarF*. 27 CanlId !Stmet. Orange. NJ. 070!50 I USA. ULTEM 2100,2200,2300 & 2400 (Glass Reinforced Amorphous...
Journal Articles
Alloy Digest (1992) 41 (1): Ni-400.
Published: 01 January 1992
... THERMOCOUPLES ISA MOY Temperature Range Limit of Error Type Pair C OF Standard Special K TOPHEL@/NIAL 0- 1250 (32-2282) ti.2pc f 1.3/q f 1.1 C (H.6 F) or +.75% or ti.4* E TOPHEL@/CUPRON@ O-900 (32-1652) f1.7 C (H°F) +0.83 C (H.6 l=) or !zO.50% or 0.4%* *% of the actuai temperature, not temperature range...
Journal Articles
Alloy Digest (1992) 41 (1): Cu-568.
Published: 01 January 1992
...) 14m;E g.63) 0 0 20/0.032$0.81) 24/00($51) 28/O;F;0($33) C( F) 760 (1401) 593 (1 loo) 482 (900) 371 (700) 371(700) 371(700) 260 (500) 204 (400) 204 (400) 871 (1600) 649 (1200) 537 (looo) 427 (800) 427 (800) Table 4 - STANDARD EMF TOLERANCES OF CUPRON THERMOCOUPLES ISA Alloy Temperature Range Limit of...
Journal Articles
Alloy Digest (1993) 42 (2): Ni-423.
Published: 01 February 1993
.... 75 mi ILS. and 700 mi CO. (pressure at temu Extension Rate: 4 x 10-6/set. 300 350 425 450 . 1 L. . 1 _ Time E / lime A Elongation; /Elongation A ROA EIROAA 1.06 1.06 0.98 1.25 1.16 0.90 1.06 1.05 1.00 1.44 1.00 0.87 Table 9 - C-RING DATA COLD WORKED G-5p ALLOY C-RING RESULTS Actual Stress 100% -No...
Journal Articles
Alloy Digest (1960) 9 (2): SS-12.
Published: 01 February 1960
...® 1996 fabk 6 - EFFECT OF COLD WORK ON PROPERTIES OF SOLUTION TREATED 1 RD. BAR STOCK (Co&i worked after qwwhing previous to mnpcring at 12OO P for 4 hours) Yield Point. vsi Yield saws* 0.2% set. r&l y!g$F RtdlKdon 0 of Ibe& % Ii!%zi -gpd";sb" piJ g i%z z 2? 180 2& tz 71000 136000 :i%i :zE 24 50 ;i Ei...
Journal Articles
Alloy Digest (1997) 46 (2): SS-672.
Published: 01 February 1997
...% TriaclleauoyTs-3 slelliIe.aooyNo. 1 : U S U E S E sIdiuauoyNo.6 E E U E Lbmpy(d).l3nnnlyera):G.5-20~~0.lM5lmmlyear):S051-1~ mmlyearj;U.Shpy(A27dye.ar) General Characteristics: The Ttistelle alloys were designed to resist corrosion and all forms of wear. in particular, they were developed to withstand galling...
Journal Articles
Alloy Digest (1961) 10 (12): Co-5.
Published: 01 December 1961
...- -- 34,6W 39fW :3iE 34,100 37.100 36;750 G!fSW 32;ObO 29.600 34m 31.700 34300 35;OOO 33.700 u.600 - 33,000 33&m 3%E 32,200 ji;8oi1 32,600 33300 Tablo 3 -STRESSRUPTURE PROPERWHRRT Table 4- STRESS RUPTURE PROPERTIECBAR Tut =w Average Stress, psi, for Rupmfc in Deg. F. 10 Hcmn 100 Hours I.000 Haurs 1.500 i...
Journal Articles
Alloy Digest (1960) 9 (11): Co-8.
Published: 01 November 1960
... ptopetties in ptecision astingr Composition: Physical Constants carbon chromium 0.2; E 0.2; expMsiori,in,ilL,~F. 70-6OO P. NickeI EC?= g t; yi5- 2:00 mai. mM:pp cob& Remainder Thermal conducrivity, BTU/ff/in./hrP. z i9&. at 1112+. * Haynes SteIlite is a regismed trade-mark of Union Carbide and Catbon...
Journal Articles
Alloy Digest (1956) 5 (2): Ni-23.
Published: 01 February 1956
... International® 1996 Table 5 - AVERAGE STRFSS-RUPTURF PROPRRTIES est T Stress, psi. for Rupture in 126( Gmdition 100 hrs. 1000 Ill-s. 42500 :sEi 25& :%i :Ei %Z :% Wrought and Iklnealed :z ;g i!E! 10000 6000 Table 6 - EFFECT OF AGING --CAST (Aged at 1475 F. tested at worn temperatum) Tens& Strength eId Reduction...
Journal Articles
Alloy Digest (1963) 12 (6): Co-10.
Published: 01 June 1963
... 40200 20.0 33.5 33.5 x 106 As Gut 43.60 2% 14:1 22:; ; m$ As cast 19:3 x 106 22 g p&. Q mm&. 18.1 19.0 x 106 aged 50 HIS: % 135OOF: Table 2 - STRESS RLIFTURE PROPERTIES (Cast test specimens) Test Temperawe OF. 1200 1300 :z 1600 1700 1800 2000 T= T cmFF== StresS . psi 1350 ::E z:: 12000 :E 14000 9 1600...
Journal Articles
Alloy Digest (1993) 42 (1): Ni-421.
Published: 01 January 1993
...-421 - DIGEST- DATA ON WORLD WIDE METALS AND ALLOYS JANUARY 1993 %P"" P-w AkayLl@8tkl201~Z'-6161 27CanfiiSlrem.OranNJ.O7050lUSA INCONEL@ ALLOY 686 (Ni-Cr-Mo-W Corrosion Resistant Nickel-Base Alloy) INCONEL ALLOY 686 has a higher Cr + MO + W content than the current generation of corrosion-resistant...
Journal Articles
Alloy Digest (1954) 3 (1): Cu-14.
Published: 01 January 1954
... 0.12 0.11 0.047 0.077 0.0000190 0.0000173 83-88 50-75 2.1-1.97 3.5-2.3 -0 000125 + 0.00024 I S.OOO,OOO 2 1,000,000 6JOO.000 7,100,000 1.0030 1.0015 Tensize Yidd Proportiond Sk Strength Limit e W?Jo~ p psi 98000 80000 36000 108000 9oooo 55000 115000 loo000 65000 138000 115000 70000 150000 130000 75000...
Journal Articles
Alloy Digest (1968) 17 (1): Fe-32.
Published: 01 January 1968
... tapping speed. .re 10-l 5 sfpm. Workability: Alloy 902 is readily cold-formed using standard practices. Forming should be done on unaged materiel. Weldability: Alloy 902 an be joined by stendard brazing, soldering end weldfng proce..e.. The gs. tung.tm-.rc proce done either autogenoumly or with P filler...