Abstract
Alloy development for gas turbine components has produced materials able to maintain strength and integrity at operating temperatures up to similar to 1050 degrees C. Next-generation RR1000 nickel-based superalloy reflects this philosophy, albeit at the expense of machinability. Experimental data for drilling showed flank wear when operating at 45 m/min to be
Original language | English |
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Pages (from-to) | 89-92 |
Number of pages | 4 |
Journal | CIRP Annals - Manufacturing Technology |
Volume | 60 |
Issue number | 1 |
DOIs | |
Publication status | Published - 1 Jan 2011 |
Keywords
- Nickel alloy
- Surface integrity
- Drilling