|   C  |    S  |    P  |    Si  |    Mn  |    Ti  |    Co  |    Cr  |    Fe  |    Zr  |    Cu  |    B  |    Al  |  
|   ≤  |  ||||||||||||
|   0.13  |    0.015  |    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  |  
| ʻO ka mānoanoa (g/cm3)  |  Lae hehee (℃)  |  ʻO ke kau wela wela (W/m·℃)  |  Modulus elastic (MPa)  |  Koefficient hoʻonui wela ( 10-6℃-1)  |  
| 8.2 | 1400 | 21.76(100 ℃) | 225 | 12.71(20-100 ℃) | 
| Hoʻomaʻamaʻa wela | Ka ikaika tensile (MPa)  |  Hua ikaika (MPa)  |  ʻO ka lōʻihi (%)  |  
| Lapaʻau hoʻonā | 820 | 590 | 8 | 
| Bar/Rod | Uea | Hoʻopaʻa / ʻāwili | Pepa/Pula | Paipu/Tube | 
|   BS HR2, HR501, HR502 a me HR503;SAE AMS 5829;AECMA PrEN 2295, 2296  2297, 2400, 2401, 2669 a me 2670.   |    BS HR202, AECMA PrEN 2298   |    BS HR402, AECMA PrEn 2299   |  ||
Hoʻoikaika nui kēia huila i ka pae γ'i3(Ti、).ʻO ka hoʻololi o ka wā kahiko o ka cobalt nickel base superalloy,loaʻa ka nui o ka cobalt a
nā ʻano mea hoʻoikaika like ʻole,ka ikaika tensile kiʻekiʻe a me ke kūpaʻa ʻana i ka 815 ~ 870 ℃, kū maikaʻi maikaʻi i ka oxidation a me ke kūpaʻa corrosion,
i ke anu a me ka wela hou a ma lalo o ka hana o alternating, hōʻike kiʻekiʻe luhi ikaika a me ka maikaʻi formability a weldability.
• Turbine Engine turbine disc• Laha • apo sila a me ka mea elastic
• nā mea hoʻopaʻa wela kiʻekiʻe