Inventor · disambiguated record
Eunice Allen-Bradley
Also filed as: ALLEN-BRADLEY EUNICE
9 granted patents·4 pending applications·129 citations·filing 2006–2023
88Inventor score
Files withALLEN-BRADLEY EUNICE4UNITED TECHNOLOGIES CORP4PRAISNER THOMAS J3AGGARWALA ANDREW S1RAYTHEON TECH CORP1
Top patents by PatentIndex Score
13 records- 0193US7887297B2Airfoil array with an endwall protrusion and components of the arrayUNITED TECHNOLOGIES CORP·Filed 2006·Granted Feb 15, 2011·46 cites·30 claims
- 0292US9133713B2Gas turbine engine turbine blade airfoil profileALLEN-BRADLEY EUNICE·Filed 2012·Granted Sep 15, 2015·18 cites·11 claims
- 0379US8511978B2Airfoil array with an endwall depression and components of the arrayALLEN-BRADLEY EUNICE·Filed 2006·Granted Aug 20, 2013·18 cites·20 claims
- 0476US8979499B2Gas turbine engine airfoil profileALLEN-BRADLEY EUNICE·Filed 2012·Granted Mar 17, 2015·6 cites·15 claims
- 0574US8061980B2Separation-resistant inlet duct for mid-turbine framesPRAISNER THOMAS J·Filed 2008·Granted Nov 22, 2011·14 cites·12 claims
- 0672US8075259B2Turbine vane airfoil with turning flow and axial/circumferential trailing edge configurationPRAISNER THOMAS J·Filed 2009·Granted Dec 13, 2011·13 cites·25 claims
- 0764US8366399B2Blade or vane with a laterally enlarged baseUNITED TECHNOLOGIES CORP·Filed 2006·Granted Feb 5, 2013·8 cites·20 claims
- 0863US2020024984A1Endwall ControuringUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 0960US8517686B2Flow passage for gas turbine engineALLEN-BRADLEY EUNICE·Filed 2009·Granted Aug 27, 2013·6 cites·17 claims
- 1053US2014154068A1Endwall ControuringUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 1146US2024302042A1Turbine engine combustor wall with aperture deflectorRAYTHEON TECH CORP·Filed 2023·Application pending·0 cites
- 1241US9957801B2Airfoil design having localized suction side curvaturesAGGARWALA ANDREW S·Filed 2012·Granted May 1, 2018·0 cites·16 claims
- 1337US2012275922A1High area ratio turbine vanePRAISNER THOMAS J·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →