Calor- resistens Steels ad machinas aeronauticas
1. GH2132 (Inconel 718)
Materia compositio: Ni 55-58%, Cr 17-21%, Mo 2.8-3.3%, Nb 4.75-5.5%, Ti 0.65-1.15%, Al 0.2-0.8%
Duritia: HRC 30-45
Calor- caloris resistens range: -253 gradus ad DCC gradum
2. GH4169 (Inconel 625);
Materia compositio: Ni 58%, Cr 20%, Mo 8%, Ti 3.8%, Al 1.9%
Duritia: HRC 34-40
Calor- caloris resistens range: -253 gradus ad 1000 gradum
1. Calor ferro obsistens industriae petrochemicae
1.1Cr5Mo (P5) Materia compositio: C 0.15%, Si Minor quam vel aequalis ad 0.50%, Mn 0.30 - 0.60%, Cr 4.00 - 6.00%, Mo 0.45 - 0.65% Duritia: HB Minor quam vel aequalis 187 Calor temperatus resistens: -29 gradus ad 550 gradum
2. 15CrMo (P11) Materia compositio: C 0.12-0.18%, Si 0.17-0.37%, Mn 0.40-0.70%, Cr 0.80-1.10%, Mo 0.40-0.55%. Duritia: HB Minor quam vel aequalis 217. Calor resistentiae temperatus range: -29 gradus ad 550 gradum.
Calor- chalybe resistens pro boiloribus et vasis pressionis
1.15CrMoR Materia compositio: C 0.12-0.18%, Si 0.17-0.37%, Mn 0.40-0.70%, Cr 0.80-1.10%, Mo 0.40-0.55%. Duritia: HB Minor quam vel aequalis 217. Calor resistentiae temperatus range: -29 gradus ad 550 gradum.
2. 13CrMo44 Compositio materialis: C 0.15-0.18%, Si Minus quam vel=0.50%, Mn 0.40-0.70%, Cr 0.70-1.10%, Mo 0.40-0.60%. Duritia: HB Minor quam vel aequalis 229. Calor resistentiae temperatus range: -29 gradus ad 550 gradum . Sunt superiores communes gradus caloris obsistens chalybeis eorumque parametri temperie. Omnes hi gradus certae caloris proprietates resistentiae habent, sed electio specifica necessaria comprehendi debet in ambitu ac requisitis laborantibus.
