Search results
Search list
Results in:
WL 1.6722-1
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo, comsumable electrode remelted; bars and forgings
Edition
1992-08
WL 1.4943-1
Aerospace; heat-resisting precipitation-hardening nickel-chromium-titanium steel with approx. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, consumable electrode remelted; sheet, plate and strip
Edition
1992-08
WL 1.4943-2
Aerospace; heat-resisting precipitation-hardening nickel-chromium-titanium steel with approx. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, consumable elektrode remelted; bars and forgings
Edition
1992-08
WL 1.4943-3
Aerospace; heat-resisting precipitation-hardening nickel-chromium-titanium steel with approx. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, comsumable elektrode remelted; filler metal for welding
Edition
1992-08
WL 1.6658-100
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo, consumable electrode remelted; bars and forgings; design and production data, conversion
Edition
1992-08
WL 1.6722-100
Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo, comsumable electrode remelted; bars and forgings; design and production data, conversion
Edition
1992-08
WL 1.6974-1
Aerospace; high-strength hardened and tempered nickel-cobalt steel with approx. 0,3 C, 8 Ni, 4,5 Co, 1 Cr, 1 Mo, consumable electrode remelted; bars and forgings
Edition
1992-08
WL 1.6974-100
Aerospace; high-strength hardened and tempered nickel-cobalt steel with approx. 0,3 C, 8 Ni, 4,5 Co, 1 Cr, 1 Mo, consumable electrode remelted; bars and forgings; design and production data, conversion
Edition
1992-08
WL 2.4632-2
Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 18 Co - 2,5 Ti - 1,5 Al, consumable electrode remelted; bars and forgings
Edition
1993-08
WL 2.4632-3
Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 18 Co - 2,5 Ti - 1,5 Al, consumable electrode remelted; tubes
Edition
1993-08