ICS 49.025.05
Ferrous alloys in general
Standards in This Category
LVS EN 4315:2026
Aerospace series - Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) - Consumable electrode remelted - Solution treated and precipitation treated - Bars and sections - a or D ≤ 100 mm - Rm ≥ 900 MPa
This document establishes technical specifications for the preparation and heat treatment of consumable electrode remelted rods and profiles made from the heat-resistant superalloy designated as
LVS EN 4314:2026
Aerospace series - Heat-resisting alloy X4NiCrTiMoV26-15 (1.4680) - Consumable electrode remelted - Not heat treated - Forging stock - a or D ≤ 250 mm
This technical specification addresses the manufacturing and quality requirements for aerospace-grade nickel-based heat-resistant alloys, specifically focusing on the composition designated as
LVS EN 4318:2026
Aerospace series - Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) - Consumable electrode remelted - Solution treated and precipitation treated - Bars and sections - De ≤ 100 mm - Rm ≥ 960 MPa
This technical specification addresses the material requirements and processing protocols for high-temperature resistant alloys specifically designated as X6NiCrTiMoV26-15, known by the commercial
LVS EN 4317:2026
Aerospace series - Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) - Consumable electrode remelted - Not heat treated - Forging stock - a or D ≤ 200 mm
This document specifies requirements for a specialized nickel-based superalloy, designated as X6NiCrTiMoV26-15, which corresponds to material number 1.4980 within the aerospace sector. The standard
LVS EN 4526:2013
Aerospace series - Metallic materials - Test methods - Sharp edge-notch tensile testing for sheet and strip
This standard outlines the procedures for conducting tensile tests on thin sheets and strips made of metallic materials used in aerospace applications. It specifically addresses specimens featuring
LVS EN 4575:2020
Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated and descaled - Sheets and plates - 3 mm < a ≤ 50 mm
This document specifies the technical requirements for solid solution treated and pickled flat products made of the high-temperature resistant alloy designated as X12CrNiCoMoW21-20. It applies to
LVS EN 4571:2020
Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Bars and sections - De ≤ 100 mm
This document establishes technical specifications for solution treated bars and profiles made from heat-resistant alloy X12CrNiCoMoW21-20, intended for use in aerospace applications. The material is
LVS EN 4574:2020
Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated and precipitation treated - Forgings - De ≤ 100 mm
This technical specification establishes the heat treatment procedures for specific aerospace forged components made from the high-temperature resistant alloy X12CrNiCoW21-20, covering diameters up
LVS EN 4572:2020
Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Sheets and strips - a ≤ 3 mm
This technical document specifies the requirements for heat-treated sheets and strips made from the high-temperature alloy designated as X12CrNiCoMoW21-20. The material is subjected to a solution
LVS EN 4573:2020
Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated and precipitation treated - Bars and sections - De ≤ 100 mm
This technical specification establishes comprehensive guidelines for the heat treatment processes applied to specific high-temperature nickel-based alloy products, identified as X12CrNiCoW21-20. The
LVS EN 4570:2020
Aerospace series - Heat resisting alloy X12CrNiCoMoW21-20 - Solution treated - Forgings - De ≤ 100 mm
This technical specification outlines the requirements for heat-treated solid-solution forged components made from X12CrNiCoMoW21-20 heat-resistant alloy, specifically designed for the aviation
LVS EN 4678:2011
Aerospace series - Weldments and brazements for aerospace structures - Joints of metallic materials by laser beam welding - Quality of weldments
This technical specification establishes comprehensive requirements for the quality of metal joints produced via laser beam welding within aerospace and aviation structural applications. It addresses
LVS EN 6018:2018
Aerospace series - Test methods for metallic materials - Determination of density according to displacement method
This document outlines a technical specification developed within the aviation and aerospace sector, focusing on the characterization of metallic materials. The procedure describes a specific
LVS EN 6072:2010
Aerospace series - Metallic materials - Test methods - Constant amplitude fatigue testing
This document outlines procedures for conducting constant amplitude fatigue tests on metallic materials, specifically within the context of the aerospace sector. It provides a standardized
SM EN 4315:2026
Space series. Heat-resistant alloy X6NiCrTiMoV26-15 (1.4980). Vacuum re-melted with consumable electrode. Solution and precipitation treated. Bars and profiles. a or D ≤ 100 mm. Rm ≥ 900 MPa
This technical specification establishes requirements for a specialized nickel-chromium titanium molybdenum vanadium alloy, designated as X6NiCrTiMoV26-15, falling under the aerospace materials
SM EN 4314:2026
Aerospace series. High-temperature resistant alloy 4NiCrTiMoV26-15 (1.4680). Remelted with consumable electrode. Untreated thermally, products intended for forging. a or D ≤ 250 mm
This document establishes technical specifications for a specialized nickel-chromium-titanium-molybdenum-vanadium alloy designated as 4NiCrTiMoV26-15, corresponding to material number 1.4680. It
SM EN 3762:2023
Aerospace series. Heat-resistant alloy X6NiCrTiMnMoV26-15 (1.4944). Annealed and cold worked. Wire for forged fasteners. D ≤ 15 mm. 1 100 MPa ≤ Rm ≤ 1 300 MPa
This technical specification establishes comprehensive requirements for a specific grade of aerospace-grade heat-resistant alloy designated as X6NiCrTiMnMoV26-15, corresponding to material number
SM EN 3639:2021
Aerospace Series. Heat-Resistant Alloy X6NiCrTiMoV26-15 (1.4980). Annealed and Cold-Worked. Cold-Drawn Forged Fastener Wires. D ≤ 15 mm. 900 MPa ≤ Rm ≤ 1 100 MPa
This specification outlines the technical requirements for a specific type of wire rod used in the aerospace sector. The material in question is a heat-resistant
SM EN 3761:2021
Spatial series. Heat-resistant alloy FE-PA2601. Quenched and cold-drawn. Bars for forged assembly components. D ≤ 50 mm. 1 100 MPa ≤ Rm ≤ 1 300 MPa
This specification outlines requirements for round bars intended for use in aerospace applications, specifically for forged components with diameters not exceeding 50 millimeters. The material
SM EN 4573:2020
Series aerospace. Heat-resistant alloy X12CrNiCoMoW21-20. Solution treated and precipitated. Bars and profiles. Up to ≤ 100 mm
This technical specification addresses the heat treatment protocols specifically designed for X12CrNiCoMoW21-20 precipitation-hardening alloy products within the aviation sector. The document