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Udimet 520

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Series: ASM Handbook
Volume: 6
Publisher: ASM International
Published: 01 January 1993
DOI: 10.31399/asm.hb.v06.a0001424
EISBN: 978-1-62708-173-3
..., 2.5 Ti, 0.06 Zr, 0.008 B Udimet 500 … 0.08 18.0 bal 18.5 … 4.0 … 2.9 Al, 2.9 Ti, 0.05 Zr, 0.006 B Udimet 520 … 0.05 19.0 bal 12.0 … 6.0 1.0 2.0 Al, 3.0 Ti, 0.005 B Udimet 630 … 0.03 18.0 bal … 18.0 3.0 3.0 6.5 Nb, 0.5 Al, 1.0 Ti Udimet 700 … 0.03 15.0 bal...
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.a0001049
EISBN: 978-1-62708-161-0
... … … … 0.15 0.010 0.05 … Udimet 400 (a) bal 17.5 14.0 4.0 … 0.5 1.5 2.5 … … … 0.06 0.008 0.06 … Udimet 500 54.0 18.0 18.5 4.0 … … 2.9 2.9 … … … 0.08 0.006 0.05 … Udimet 520 57.0 19.0 12.0 6.0 1.0 … 2.0 3.0 … … … 0.05 0.005 … … Udimet 630 (a) bal...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003120
EISBN: 978-1-62708-199-3
... N07500 19.0 48.0 19.0 4.0 … … 3.0 3.0 4.0 max 0.08 0.005 B Udimet 520 … 19.0 57.0 12.0 6.0 1.0 … 3.0 2.0 … 0.08 0.005 B Udimet 630 … 17.0 50.0 … 3.0 3.0 6.5 1.0 0.7 18.0 0.04 0.004 B Udimet 700 … 15.0 53.0 18.5 5.0 … … 3.4 4.3 <1.0 0.07 0.03 B...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0003999
EISBN: 978-1-62708-185-6
... <0.3 0.16 0.01 0.05Zr Udimet 500 19 bal 19 4 … … 3 3 <4.0 0.08 0.005 … Udimet 520 19 bal 12 6 1 … 3 2 … 0.08 0.005 … Udimet 700 15 bal 17 5 … … 3.5 4 <1.0 0.07 0.02 0.02Zr Udimet 710 18 bal 14.8 3 1.5 … 5 2.5 … 0.07 0.01 … V57...
Series: ASM Handbook
Volume: 4E
Publisher: ASM International
Published: 01 June 2016
DOI: 10.31399/asm.hb.v04e.a0006265
EISBN: 978-1-62708-169-6
... B, 0.05 Zr René 100 (b) … 9.5 61.0 15.0 3.0 … … 4.2 5.5 1.0 max 0.16 0.015 B, 0.06 Zr, 1.0 V Udimet 500 (b) N07500 19.0 48.0 19.0 4.0 … … 3.0 3.0 4.0 max 0.08 0.005 B Udimet 520 … 19.0 57.0 12.0 6.0 1.0 … 3.0 2.0 … 0.08 0.005 B Udimet 630 (b...
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.a0001050
EISBN: 978-1-62708-161-0
... … … … bal 1.5 Fe 8.17 Nimocast 90 0.06 19.5 18.0 … … … … 1.4 2.4 … … … bal 1.5 Fe 8.18 Nimocast 95 0.07 19.5 18.0 … … … … 2.0 2.9 … 0.02 0.015 bal … … Nimocast 100 0.20 11.0 20.0 5.0 … … … 5.0 1.5 … 0.03 0.015 bal … … Udimet 500 0.08 18.5 16.5...
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0003517
EISBN: 978-1-62708-180-1
..., and nozzles Alloy designation Description Alloys for blades and buckets Udimet 520 Wrought nickel-base alloy Udimet 500 Cast nickel-base alloy IN 738 Conventionally cast nickel-base alloy, high carbon IN 738LC Conventionally cast nickel-base alloy, low carbon DS CM 247 LC...
Series: ASM Handbook
Volume: 11A
Publisher: ASM International
Published: 30 August 2021
DOI: 10.31399/asm.hb.v11A.a0006824
EISBN: 978-1-62708-329-4
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003192
EISBN: 978-1-62708-199-3
... 370 0.040 C-6 … … … 150–200 Cold drawn 0.040 210 0.007 M2, M3 680 820 0.007 C-7 1225 0.007 CC-7 0.150 160 0.015 M2, M3 520 625 0.020 C-6 800 0.015 CC-6 0.300 125 0.020 M2, M3 410 495 0.030 C-6 650 0.020 CC-6 0.625 100 0.030 M2, M3 330 385 0.040 C...
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0003737
EISBN: 978-1-62708-177-1
... + Ta, 0.7 Al ZMI-3U 0.08 … bal 5.5 13 5.0 1.2 5.0 W, 3.0 Al, 0.015 B CNK7 0.08 … bal 9.0 14.8 4.2 0.4 7.0 W, 0.01 B, 0.02 Ce René 41 0.09 … bal 11.0 19.0 3.1 10.0 1.5 Al, 0.010 B max René 95 0.15 … bal 8.0 14.0 2.5 3.5 3.5 Al, 3.5 W, 3.5 Nb U-520 0.05...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002472
EISBN: 978-1-62708-194-8
... mixture at 705 °C (1300 °F) ( Ref 57 ). These results were explained in terms of grain-boundary penetration of sulfur, which leads to rapid crack propagation. The coated specimen was far less susceptible, and the addition of a grain-boundary modifier (in this case, boron) in Udimet 720 gave an enormous...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002391
EISBN: 978-1-62708-193-1
Series: ASM Handbook
Volume: 1
Publisher: ASM International
Published: 01 January 1990
DOI: 10.31399/asm.hb.v01.9781627081610
EISBN: 978-1-62708-161-0
Series: ASM Handbook
Volume: 4D
Publisher: ASM International
Published: 01 October 2014
DOI: 10.31399/asm.hb.v04d.a0005938
EISBN: 978-1-62708-168-9
... test machine, and applied it to Udimet 720Li. The toughness was derived by measuring the failing load when growing a single edge precrack explosively in a dog-bone-shaped sheet specimen. For the ASTM 6 to 8 intermediate grain size, KQ was approximately 35 to 50 MPa m 1/2 in the 850 to 950 °C (1560...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003164
EISBN: 978-1-62708-199-3
... Al alloyed with hafnium and boron is superior to that of Udimet 115 at 760 °C (1400 °F). Fig. 9 Crack growth rates of nickel aluminide (Ni-23.5Al-0.5Hf-0.1B, at.%), LRO alloys [(Fe,Ni) 3 (V,Ti)], and several high-temperature alloys tested in air at 25 °C (80 °F) Corrosion Resistance...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 November 1995
DOI: 10.31399/asm.hb.emde.a0003005
EISBN: 978-1-62708-200-6
... steels ASTM No. and type UNS designation Tensile strength Yield strength Elongation, % MPa ksi MPa ksi A242 type 1 K11510 435–480 63–70 290–345 42–50 21 A572 grade 50 … 450 65 345 50 21 A607 grade 60 … 520 75 415 60 16–18 A607 grade 70 … 590 85 485 70...
Series: ASM Handbook
Volume: 20
Publisher: ASM International
Published: 01 January 1997
DOI: 10.31399/asm.hb.v20.a0002462
EISBN: 978-1-62708-194-8
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005459
EISBN: 978-1-62708-196-2
... = 0.4659 ⋅ 10 − 2 ε ˙ 0.1238 exp ( 49 , 520 / R T ) Critical strain ε c = 5 / 6 ε p Metadynamic or recrystallized fraction X mdrx = 1 − exp [ − ln 2 ( t / t 0.5 ) n ] with n = 1 Time...
Series: ASM Handbook
Volume: 14A
Publisher: ASM International
Published: 01 January 2005
DOI: 10.31399/asm.hb.v14a.a0003976
EISBN: 978-1-62708-185-6
... but have been found to be useful in operations such as isothermal forging of titanium alloys where these attributes are not important. Among the cast superalloys most often employed are IN-100, Udimet 500, Nimocast 80 and 90, and Inconel 713LC. These alloys have hot yield strengths comparable...
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.9781627081993
EISBN: 978-1-62708-199-3