Inventor · disambiguated record
Yehia M. El-Aini
Also filed as: EL-AINI YEHIA · EL-AINI YEHIA M
13 granted patents·536 citations·filing 1991–2015
94Inventor score
Files withUNITED TECHNOLOGIES CORP7EL-AINI YEHIA M3EL-AINI YEHIA1FLORIDA TURBINE TECH INC1PRATT & WHITNEY ROCKETDYNE INC1
Top patents by PatentIndex Score
13 records- 0195US8105039B1Airfoil tip shroud damperEL-AINI YEHIA M·Filed 2011·Granted Jan 31, 2012·31 cites·23 claims
- 0295US8066479B2Non-integral platform and damper for an airfoilEL-AINI YEHIA M·Filed 2010·Granted Nov 29, 2011·40 cites·12 claims
- 0394US9151170B2Damper for an integrally bladed rotorEL-AINI YEHIA M·Filed 2011·Granted Oct 6, 2015·19 cites·1 claims
- 0492US8002286B1Aerodynamically mistuned labyrinth sealFLORIDA TURBINE TECH INC·Filed 2010·Granted Aug 23, 2011·23 cites·3 claims
- 0589US7955054B2Internally damped bladePRATT & WHITNEY ROCKETDYNE INC·Filed 2009·Granted Jun 7, 2011·27 cites·24 claims
- 0688US8600707B1Process for analyzing a labyrinth seal for flutterEL-AINI YEHIA·Filed 2011·Granted Dec 3, 2013·23 cites·6 claims
- 0788US5232344AInternally damped bladesUNITED TECHNOLOGIES CORP·Filed 1992·Granted Aug 3, 1993·77 cites·4 claims
- 0885US5498137ATurbine engine rotor blade vibration damping deviceUNITED TECHNOLOGIES CORP·Filed 1995·Granted Mar 12, 1996·95 cites·12 claims
- 0983US6055805AActive rotor stage vibration controlUNITED TECHNOLOGIES CORP·Filed 1997·Granted May 2, 2000·56 cites·17 claims
- 1081US5165860ADamped airfoil bladeUNITED TECHNOLOGIES CORP·Filed 1991·Granted Nov 24, 1992·71 cites·12 claims
- 1177US7806410B2Damping device for a stationary labyrinth sealUNITED TECHNOLOGIES CORP·Filed 2007·Granted Oct 5, 2010·18 cites·20 claims
- 1277US6125626AActive rotor stage vibration controlUNITED TECHNOLOGIES CORP·Filed 1999·Granted Oct 3, 2000·55 cites·9 claims
- 1366US10087763B2Damper for an integrally bladed rotorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 2, 2018·1 cites·20 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →