发明名称 |
Titanium alloy composition for the production of high-performance parts, in particular for the aeronautical industry |
摘要 |
A titanium alloy having at least 4% by weight aluminum and at least 0.1% by weight oxygen, the alloy also including at least one element selected from vanadium, molybdenum, chromium, and iron. The titanium alloy also includes hafnium in a proportion by weight of at least 0.1%. |
申请公布号 |
US9399806(B2) |
申请公布日期 |
2016.07.26 |
申请号 |
US201013376882 |
申请日期 |
2010.06.08 |
申请人 |
MESSIER-BUGATTI-DOWTY |
发明人 |
Soniak Francis;De Monicault Jean-Michel |
分类号 |
C22C14/00;C22F1/18 |
主分类号 |
C22C14/00 |
代理机构 |
Sughrue Mion, PLLC |
代理人 |
Sughrue Mion, PLLC |
主权项 |
1. A forged aircraft landing gear composed of a titanium alloy, in addition to titanium constituting the majority proportion by weight, the alloy including at least the following elements, in the proportions by weight that are specified:aluminum4.0% to 7.5%vanadium3.5% to 5.5%molybdenum4.5% to 7.5%chromium1.8% to 3.6%iron0.2% to 0.5%hafnium0.1% to 0.7%oxygen0.1% to 0.3%carbon0.01% to 0.2%zirconium 0.1% to less than 0.7%, wherein the combined proportion by weight of hafnium plus zirconium does not exceed 1%. |
地址 |
Velizy Villacoublay FR |