Heat resistant super alloy and its use

Abstract

A heat resistant super alloy suffices the following conditions: carbon 0.01-0.2 percent in weight chromium 8-10 percent in weight aluminum 4-6 percent in weight titanium 2-4 percent in weight molybdenum 1.5-2.8 percent in weight tungsten 10-13.5 percent in weight niobium 1.5-2.5 percent in weight boron 0 < B ≦ 0.04 percent in weight zircon 0 < Zr ≦ 0.15 percent in weight the contents of hafnium and lanthanum together amounts to 0 < Hf + La ≦ 1.5 percent in weight, optionally traces of tantalum, the remainder being nickel. Such an alloy is preferably used for turbine wheels and particularly for turbochargers.

Dependencies are inferred from the claim text.