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WL 1.4954 Beiblatt 1 High temperature precipitation-hardening nickel-chromium-titanium steel with about 0,05 C, 25 Ni, 15 Cr, 2,1 Ti; filler metal; inДействующий for new design WL 1.4954 Beiblatt 1 High temperature precipitation-hardening nickel-chromium-titanium steel with ... WL 1.6723-100 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo; bars and forgings; design and production data, conversion WL 1.6723-100 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr... WL 1.6657-1 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo; bars and forgings WL 1.6657-1 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,14 C, 3 Ni, 1 Cr... 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 WL 1.4943-1 Aerospace; heat-resisting precipitation-hardening nickel-chromium-titanium steel with appr... 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 WL 1.6722-1 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr... WL 1.4943-100 Aerospace; high-strength precipitation-hardening nickel-chromium-titanium steel with aprox. 0,03 C, 25 Ni, 15 Cr, 1,8 Ti, consumable electrode remelted; sheets, plate, strip, bars, forgings and filler metal for welding; design and production WL 1.4943-100 Aerospace; high-strength precipitation-hardening nickel-chromium-titanium steel with aprox... 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 WL 1.6658-100 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,14 C, 3 Ni, 1 Cr... 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 WL 1.6974-1 Aerospace; high-strength hardened and tempered nickel-cobalt steel with approx. 0,3 C, 8 N... WL 1.5924-100 Aerospace; case-hardening chromium-nickel steel with approx. 0,15 C, 1,5 Cr, 1,5 Ni; bars and forgings; design and production data, conversion WL 1.5924-100 Aerospace; case-hardening chromium-nickel steel with approx. 0,15 C, 1,5 Cr, 1,5 Ni; bars ... WL 1.5924-1 Aerospace; case-hardening chromium-nickel-steel with approx. 0,15 C, 1,5 Cr, 1,5 Ni; bars and forgings WL 1.5924-1 Aerospace; case-hardening chromium-nickel-steel with approx. 0,15 C, 1,5 Cr, 1,5 Ni; bars ... WL 1.6657-100 Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo; bars and forgings; design and production data, conversion WL 1.6657-100 Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr,... 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 WL 1.6722-100 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr... WL 1.6658-1 Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr, 0,2 Mo, consumable electrode remelted; bars and forgings WL 1.6658-1 Aerospace; case-hardening nickel-chromium-molydenum steel with approx. 0,14 C, 3 Ni, 1 Cr,... WL 1.5934 Beiblatt 1 Case-hardening chromium-nickel steel with about 0,18 C, 2 Cr, 2 Ni; rods and forgings WL 1.5934 Beiblatt 1 Case-hardening chromium-nickel steel with about 0,18 C, 2 Cr, 2 Ni; rods and ... WL 1.5934 Case-hardening chromium-nickel steel with about 0,18 C, 2 Cr, 2 Ni; rods and forgings; inДействующий for new design WL 1.5934 Case-hardening chromium-nickel steel with about 0,18 C, 2 Cr, 2 Ni; rods and forgings; inДейст... WL 1.6723-1 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr, 0,2 Mo; bars and forgings WL 1.6723-1 Aerospace; case-hardening nickel-chromium-molybdenum steel with approx. 0,15 C, 4 Ni, 1 Cr... WL 1.7324-100 Aerospace; chromium-molybdenum steel with approx. 0,2C-0,5Cr-0,4Mo; filler metal for welding; design and production data, conversion WL 1.7324-100 Aerospace; chromium-molybdenum steel with approx. 0,2C-0,5Cr-0,4Mo; filler metal for weldi... WL 1.7214-1 Aerospace; weldable hardened and tempered chromium-molybdenum steel with approx. 0,25C-1Cr-0,2Mo; sheet, plate and strip WL 1.7214-1 Aerospace; weldable hardened and tempered chromium-molybdenum steel with approx. 0,25C-1Cr... WL 1.7254-100 Aerospace; weldable hardened and tempered cast chromium-molybdenum steel with approx. 0,25C-1Cr-0,25Mo; sand casting and investment casting; design and production data, conversion WL 1.7254-100 Aerospace; weldable hardened and tempered cast chromium-molybdenum steel with approx. 0,25... WL 1.7220 Heat-treatable chromium-molybdenum steel with about 0,35C-1Cr-0,2Mo; rods and wire for screws and nuts to be cold-formed or hot-formed; inДействующий for a new design WL 1.7220 Heat-treatable chromium-molybdenum steel with about 0,35C-1Cr-0,2Mo; rods and wire for screws ... WL 1.7324-1 Aerospace; chromium-molybdenum steel with approx. 0,2C-0,5Cr-0,4Mo; filler metal for welding WL 1.7324-1 Aerospace; chromium-molybdenum steel with approx. 0,2C-0,5Cr-0,4Mo; filler metal for weldi... WL 1.7254-1 Aerospace; weldable hardened and tempered cast chromium-molybdenum steel casting with approx. 0,25C-1Cr-0,25Mo; sand casting and investment casting WL 1.7254-1 Aerospace; weldable hardened and tempered cast chromium-molybdenum steel casting with appr... WL 1.7224-1 Aerospace; hardened and tempered chromium-molybdenum steel with approx. 0,35C-1Cr-2Mo; bars and wire for bolts and nuts to be cold or hot formed WL 1.7224-1 Aerospace; hardened and tempered chromium-molybdenum steel with approx. 0,35C-1Cr-2Mo; bar... WL 1.7224-100 Aerospace; hardened and tempered chromium-molybdenum steel with approx. 0,35C-1Cr-0,2Mo; bars and wire for bolts and nuts to be cold or hot formed; design and production data, conversion WL 1.7224-100 Aerospace; hardened and tempered chromium-molybdenum steel with approx. 0,35C-1Cr-0,2Mo; b...

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