Assignee
ALLEN-BRADLEY EUNICE
US·4 granted patents·48 citations·filing 2006–2012
Top patents by PatentIndex Score
4 records- 0192US9133713B2Gas turbine engine turbine blade airfoil profileALLEN-BRADLEY EUNICE·Filed 2012·Granted Sep 15, 2015·18 cites·11 claims
- 0279US8511978B2Airfoil array with an endwall depression and components of the arrayALLEN-BRADLEY EUNICE·Filed 2006·Granted Aug 20, 2013·18 cites·20 claims
- 0376US8979499B2Gas turbine engine airfoil profileALLEN-BRADLEY EUNICE·Filed 2012·Granted Mar 17, 2015·6 cites·15 claims
- 0460US8517686B2Flow passage for gas turbine engineALLEN-BRADLEY EUNICE·Filed 2009·Granted Aug 27, 2013·6 cites·17 claims
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