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UDIMET 700

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Journal Articles
Alloy Digest (1987) 36 (1): Ni-51.
Published: 01 January 1987
... UDIMET 700 is a wrought nickel-base alloy produced by vacuum-induction melting and further refined by vacuum-arc remelting. It has excellent mechanical properties at high temperatures. Among its applications are blades for aircraft, marine and land-based gas turbines and rotor discs...
Journal Articles
Alloy Digest (2004) 53 (4): Ni-620.
Published: 01 April 2004
... to Udimet 700 due to its lower aluminum content. Sulfidation Resistance. The 18% Cr content of this alloy pro- vides excellent resistance to general hot sulfidation attack. In addition, since the amount of chromium carbide forming at the grain boundary is small due to the low carbon content, the amount...
Journal Articles
Alloy Digest (1993) 42 (4): Ni-428.
Published: 01 April 1993
...-2475 7.5 x 1w 7.6 x lv 7.98 x lv 9.65 x 106 See Table 1 Modulus of elasticity See Table 1 *Physical properties have not yet been determined for this powder production version. Values listed are from Udimet 700 (Alloy Digest Ni-SZ), a wrought version of this alloy. PROPERTiES Table 1 - THERMAL...
Journal Articles
Alloy Digest (2004) 53 (12): Co-109.
Published: 01 December 2004
... Udimet L-605 is a high-temperature aerospace alloy with excellent strength and oxidation resistance. It is used in applications such as gas turbine blades and combustion area parts. This datasheet provides information on composition, physical properties, and tensile properties as well as creep...
Journal Articles
Alloy Digest (1964) 13 (11): Ni-95.
Published: 01 November 1964
... Udimet N-115 is a vacuum-induction melted nickel-base alloy that responds to precipitation hardening. It is a superalloy for extended service to 1850 F. It has been thus far limited to barstock for turbine blading applications and may be suitable for existing or future large forging applications...
Journal Articles
Alloy Digest (1966) 15 (2): Ni-111.
Published: 01 February 1966
... Udimet 901 is a nickel-base alloy having high creep and rupture strength at 1000 to 500 F. It is used in disc and other heavy forgings for commercial aircraft gas turbines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep...