This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. AMS6494A results from a correction of the temperature used for the response to heat treatment in 3.3.3.
Steel Bars, Forgings, and Tubing 1.0Cr - 2.50Ni - 2.0Mo - 1.10Si (0.10 - 0.20C) Aircraft-Quality
2011-07-22
Aufsatz (Konferenz)
Englisch
Manganese , Chemicals , Iron , Alloys , Heat treatment , Identification numbers , Steel , Chromium , Nickel , Tensile strength
Steel Bars, Forgings, and Tubing 1.0Cr – 2.50Ni – 2.0Mo – 1.10Si (0.10 – 0.20C) Aircraft-Quality
SAE Technical Papers | 2009
Steel Bars, Forgings, and Tubing 1.0Cr – 2.50Ni – 2.0Mo – 1.10Si (0.10 – 0.20C) Aircraft-Quality
SAE Technical Papers | 2016