ʻO Maraging C350 ka mea hao i loko o 18.5% Ni, 12% Co, 4.8% Mo, Cobalt ma ke ʻano he mea hoʻoikaika ikaika.He mea palupalu akā paʻakikī, hiki ke hana ʻia a hana ʻia.Hoʻokiʻekiʻe ke kaʻina hana ʻelemakule Maraging C350 i ka paʻakikī i kahi pae ma luna o ka paʻakikī awelika no ka hapa nui o nā noi mea hana.Loaʻa iā C350 nā waiwai mechanical maikaʻi loa, hiki ke hana a me nā hiʻohiʻona mālama wela.
Alloy | % | C | Mn | Fe | Si | P | S | Ni | Co | Mo | Ti | Al | Cr | Cu |
350 | Min. | kaulike | 18.0 | 11.5 | 4.6 | 1.3 | 0.05 | |||||||
Max. | 0.03 | 0.10 | 0.1 | 0.010 | 0.010 | 19.0 | 12.5 | 5.2 | 1.6 | 0.15 | 0.5 | 0.5 |
ʻO ka mānoanoa | 8.2 g/cm³ |
Lae hehee | 1260-1320 ℃
|
Kūlana | Ka ikaika tensile Rm N/mm² | Hua ikaika Rp 0. 2N/mm² | ʻO ka lōʻihi E like me % | ʻO Brinell paʻakikī HRC |
Lapaʻau ʻelemakule | 2234 | 2275 | 2.8 | ≥ 56HRC |
MIL-S-46850, AMS6515A
'O'ole'a loa ka huila, 'ano palupalu (RC 30/35), hiki ke hana 'ia a hana 'ia paha.Hāʻawi ʻo Maraging i kahi waiwai kiʻekiʻe no nā ʻāpana koʻikoʻi i ka aerospace, structural, component and tooling applications
1.High yield a me ka ikaika tensile hope loa
2.High toughness, ductility a me ka ikaika hopena me ka ikaika luhi kiʻekiʻe a me ka ikaika compressive
3.Hardness a me ka lole pale i lawa no na mea paahana he nui
4. Hana maʻalahi - anu, mahana, wela (w/o i ka hana anneals)
5.Good weldability w / o preheating a pou hoʻomehana a me ka maikaʻi plishability
Waiwai kiʻekiʻe no nā ʻāpana koʻikoʻi i ka aerospace, structural, component and tooling applications.wind tunnel models, landing gear parts, missile and rocket motor cases, high performance shafting, gears, and fasteners.