US 12,000,025 B2 · Powder composition for additive manufacturing

Abstract

738LC composition belongs to Ni-based super-alloy family. The alloy has been successfully used for hot section of turbine engine. Blades, Vanes and heat shields are made out of the alloy which can sustain a working temperature of 700 to 850 deg C. Additive manufacturing processes like Selective laser melting or PBF-L are not successful in using the alloy powder due to cracking issues. 738LC is also known to fall under the category of non-weldable alloys due to high content of gamma prime phase. The invention of the new composition is outside the standard 738LC with different concentration, morphology and size distribution of gamma prime phase. The invention has shown to eliminate the cracking issue in AM laser based process. The room temperature tensile properties observed are much better than cast 738LC properties.

Claims2

Dependent claims

A Ni-based alloy powder comprising a composition corresponding to a modified 738LC alloy powder, wherein the composition comprises:

Chromium between 15.7 and 16.3 wt %,
Cobalt between 8 and 9 wt %,
Aluminum between 3.2 and 3.7 wt %,
Titanium between 3.2 and 3.7 wt %,
Tungsten between 2.4 and 2.8 wt %,
Tantalum between 1.5 and 2 wt %,
Molybdenum between 1.5 and 2 wt %,
Niobium between 0.6 and 1.1 wt %,
Carbon between 0.09 and 0.13 wt %,
Zirconium between 0.03 and 0.08 wt %,
Boron at most 0.007 wt %,
Iron between 3.5 and 4 wt %,
Copper at most 0.1 wt %,
Manganese at most 0.02 wt %,
Silicon at most 0.03 wt %,
Phosphorus at most 0.015 wt %,
Sulfur at most 0.006 wt %
Oxygen at most 0.03 wt %,
Nitrogen at most 0.08%,
Total all others at most 0.15 wt %, and
remainder Nickel;
wherein the powder comprises a total of 6.5 to 7.2 wt % Aluminum and Titanium.

19 more elements

Dependencies are inferred from the claim text.

Powder composition for additive manufacturing

Life of this patent

Powder composition for additive manufacturing

Life of this patent

Abstract

Claims2