Search results
Search list
Results in:
DIN EN 2213
Aerospace series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - Dₑ ≤ 16 mm - 980 MPa ≤ Rₘ ≤ 1 180 MPa; German and English version EN 2213:2012
Edition
2012-07
DIN EN 2252
Aerospace series - Steel FE-PL1505 (15CrMoV6) - 1 080 MPa ≤ Rₘ ≤ 1 250 MPa - Forgings - Dₑ ≤ 100 mm; German and English version EN 2252:2012
Edition
2012-04
DIN EN 3355
Aerospace series - Titanium alloy TI-P64001 (Ti-6AI-4V) - Annealed - Extruded section - Dₑ ≤ 150 mm - 900 MPa ≤ Rₘ ≤ 1 160 MPa; German and English version EN 3355:2012
Edition
2012-05
DIN EN 2481
Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 250 MPa ≤ Rₘ ≤ 1 400 MPa - Forgings - Dₑ ≤ 75 mm; German and English version EN 2481:2010
Edition
2011-06
DIN EN 2482
Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rₘ ≤ 1 300 MPa - Bars - Dₑ ≤ 100 mm; German and English version EN 2482:2010
Edition
2011-06
DIN EN 2483
Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa ≤ Rₘ ≤ 1 300 MPa - Forgings - Dₑ ≤ 100 mm; German and English version EN 2483:2010
Edition
2011-06
DIN EN 3329
Aerospace series - Steel FE-PL1503 (35CrMo4) - Annealed - Sheet and strip - 0,3 mm ≤ a ≤ 2 mm - For prevailing torque nuts; German and English version EN 3329:2009
Edition
2009-08
DIN EN 3486
Aerospace series - Steel X3CrNiMoAl13-8-2 (1.4534) - Solution annealed and precipitation hardened - 1 400 ≤ Rₘ ≤ 1 550 MPa - Forgings - Dₑ ≤ 100 mm; German and English version EN 3486:2019
Edition
2020-02
DIN EN 3481
Aerospace series - Steel X8CrNiTi18-10 (1.4878/1.4544) - Annealed - Reference heat treatment: softened - Hollow bars - 5 mm ≤ a ≤ 12 mm; German and English version EN 3481:2019
Edition
2020-02
DIN EN 2280
Aerospace series - Steel FE-PM37 - 900 MPa ≤ Rₘ ≤ 1 100 MPa - Sheet - a ≤ 6 mm; German and English version EN 2280:2018
Edition
2018-09