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Fabrication Of Hybird Gas Turbine Disk Material System By Additive Manufacturing Project
<p>AM offers the potential to be revolutionary for GRC hybrid disk concept as it: i) bypasses joining through direct deposition or &ldquo;building&rdquo; of the PX bore alloy on a SX rim and ii) circumvents interface heating issues that may cause microstructural degradation during welding. Our objective is to demonstrate the feasibility of the high payoff AM hydrid disk concept described through test specimens built up using electron beam melting (EBM).</p>
Complete Metadata
| bureauCode |
[ "026:00" ] |
|---|---|
| identifier | TECHPORT_14701 |
| issued | 2014-04-01 |
| landingPage | http://techport.nasa.gov/view/14701 |
| programCode |
[ "026:000" ] |
| references |
[ "http://techport.nasa.gov/doc/home/TechPort_Advanced_Search.pdf", "http://techport.nasa.gov/fetchFile?objectId=3447", "http://techport.nasa.gov/fetchFile?objectId=3448", "http://techport.nasa.gov/fetchFile?objectId=3456", "http://techport.nasa.gov/fetchFile?objectId=6560", "http://techport.nasa.gov/fetchFile?objectId=6561", "http://techport.nasa.gov/fetchFile?objectId=6584", "http://techport.nasa.gov/home" ] |
| temporal | 2014-04-01T00:00:00Z/2014-09-01T00:00:00Z |
