C | S | P | Si | Mn | Ti | Co | Cr | Fe | Zr | Cu | B | Al |
≤ | ||||||||||||
0.13 | 0.014 | 0.02 | 0.8 | 0.4 | 2.0-3.0 | 15.0-21.0 | 18.0-21.0 | ≤1.5 | ≤0.15 | ≤0.2 | ≤0.02 | 1.0-2.0 |
Density (g/cm*3) | Liquescens punctum (℃) | Scelerisque conductivity (W/m·℃) | Modulus elasticus MPa | Scelerisque expansion coefficientes 10-6℃-1. |
8.2 | 1400 | 21.76(100℃) | 225 | 12.71(20-100℃) |
Calor treatment | Distrahentes fortitudo (MPa) | Cedat imperium (MPa) | Prolongatio (%) |
Solutio curatio | 820 | 590 | 8 |
Bar/Rod | Filum | Exue/Coil | Sheet/Plate | Pipe/Tube |
BS HR2, HR501, HR502 et HR503;SAE AMS 5829;AECMA PreN 2295, 2296 2297, 2400, 2401, 2669 et 2670 . | BS HR202, AECMA PreN 2298 | BS HR402, AECMA Pren 2299 |
Hoc mixtura maxime confirmat tempus γ'i3(Ti、).Senescit deformatio cobalt nickel basi superalloy;quibus magno moles cobalt et
variis subsidii elementis;superiores vires distrahentes et resistentia serpunt in 815 ~ 870 , resistentia bona oxidationis et resistentiae corrosioni;
in frigido et calido iterum atque iterum actione alternante, ostendens summum laborem vires et bonam formabilitatem et weldability
• Turbine Engine Turbine disc• Lamina • signantes anulum et elementum elasticum
• fastigium caliditatis • Fibulae anulum et elementum elasticum, etc