Inconel® alloy 706
The substantial nickel and chromium contents provide good resistance to oxidation and corrosion. The primary precipitation-hardening constituents of the alloy are niobium and titanium. The aluminum content also contributes to the hardening response.
The precipitation-hardening system in INCONEL alloy 706 provides the desirable characteristic of delayed hardening response during exposure to precipitation temperatures. That characteristic gives the alloy excellent resistance to postweld strain-age cracking.
INCONEL alloy 706 is used for a variety of applications that require high strength combined with ease of fabrication. In the aerospace field, the alloy is used for turbine discs, shafts, and cases; diffuser cases; compressor discs and shafts; engine mounts; and fasteners. In addition to aerospace applications, the alloy is used for turbine discs in large industrial gas turbines.
一般属性
使用 Prospector 建立免費帳戶時,可造訪 Inconel® alloy 706 的完整資料表詳細資訊。您將找到有關物理、機械和硬度規格的完整資訊
Technical Datasheet (English)
下载文档加工
Find specific processing information for Inconel® as well as general information for the Nickel - Wrought - Ni-Fe-Cr Alloy generic family. 注册 或 登录 了解更多信息。