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Technical rule [CURRENT]

WL 1.7734 Beiblatt 1

Weldable heat-treatable chromium-molybdenum-vanadium steel with about 0.15C-1.4Cr-0.9Mo-0.25V; sheets, plates, strips, rods, forgings, pipes and filler metal
Edition 1982-03

Standards [CURRENT]

WL 1.7734-4

Weldable heat-treatable chromium-molybdenum-vanadium steel with about 0.15C-1.4Cr-0.9Mo-0.25V; filler metal
Edition 1982-03

Standards [CURRENT]

WL 1.7784-5

Ultra high-strength chromium-molybdenum-vanadium steel with about 0.4C-5Cr-1.3Mo-0.5V; filler metal
Edition 1976-11

Standards [CURRENT]

WL 1.7784-100

Aerospace series - Ultrahigh-strength chromium-molybdenum-vanadium steel with approx. 0,4 C - 5 Cr - 1,3 Mo - 0,5 V - Part 100: Sheet, plate, bar, forging, bar and wire for cold-or-hot-formed bolts and nuts, tubing, filler metal - Design and production data, cross-referencing
Edition 2012-10

Standards [CURRENT]

WL 2.4370

Nickel-copper wrought alloy; NiCu30Ti, creep-resistant, filler metal (Monel 60)
Edition 1961-03

Standards [CURRENT]

WL 2.4374-2

Nickel-copper wrought alloy; NiCu30Al, creep-resistant, filler metal (K-Monel)
Edition 1961-03

Standards [CURRENT]

WL 2.4632-4

Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 18 Co - 2,5 Ti - 1,5 Al, consumable electrode remelted; filler metal for welding
Edition 1993-08

Standards [CURRENT]

WL 2.4632-100

Aerospace; heat-resisting nickel alloy with approx. 0,1 C - 20 Cr - 18 Co - 2,5 Ti - 1,5 Al; sheet, strip, bars, forgings, tubes and filler metal for welding; design and production data, conversion
Edition 1993-08

Standards [CURRENT]

WL 2.4639-1

Aerospace series - High-temperature nickel alloy with approx. 0,2 C - 20 Cr - Part 1: Welding filler metal
Edition 2012-10

Standards [CURRENT]

WL 2.4639-100

Aerospace series - High temperature nickel alloy with approx. 0,2 C - 20 Cr - Part 100: Welding filler metal - Notes for design and production, cross-reference
Edition 2012-10

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