Inventor · disambiguated record
William Abdel-Messeh
Also filed as: ABDEL-MESSEH WILLIAM
34 granted patents·4 pending applications·1,042 citations·filing 1981–2012
98Inventor score
Files withUNITED TECHNOLOGIES CORP19ABDEL-MESSEH WILLIAM5PRATT & WHITNEY CANADA5CUNHA FRANK J2CUNHA FRANCISCO J1
Top patents by PatentIndex Score
38 records- 0197US4416585ABlade cooling for gas turbine enginePRATT & WHITNEY AIRCRAFT·Filed 1981·Granted Nov 22, 1983·99 cites·11 claims
- 0295US7744347B2Peripheral microcircuit serpentine cooling for turbine airfoilsUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jun 29, 2010·16 cites·14 claims
- 0394US8105030B2Cooled airfoils and gas turbine engine systems involving such airfoilsABDEL-MESSEH WILLIAM·Filed 2008·Granted Jan 31, 2012·49 cites·20 claims
- 0494US7553128B2Blade outer air sealsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jun 30, 2009·49 cites·20 claims
- 0592US8807945B2Cooling system for turbine airfoil including ice-cream-cone-shaped pedestalsSPANGLER BRANDON W·Filed 2011·Granted Aug 19, 2014·15 cites·30 claims
- 0692US6508620B2Inner platform impingement cooling by supply air from outsidePRATT & WHITNEY CANADA·Filed 2001·Granted Jan 21, 2003·90 cites·4 claims
- 0791US5052889AOffset ribs for heat transfer surfacePRATT & WHINTEY CANADA·Filed 1990·Granted Oct 1, 1991·87 cites·8 claims
- 0890US7988418B2Microcircuits for small enginesUNITED TECHNOLOGIES CORP·Filed 2010·Granted Aug 2, 2011·11 cites·6 claims
- 0990US7311498B2Microcircuit cooling for bladesUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 25, 2007·30 cites·24 claims
- 1089US8109725B2Airfoil with wrapped leading edge cooling passageABDEL-MESSEH WILLIAM·Filed 2008·Granted Feb 7, 2012·25 cites·16 claims
- 1189US7695246B2Microcircuits for small enginesUNITED TECHNOLOGIES CORP·Filed 2006·Granted Apr 13, 2010·13 cites·13 claims
- 1288US7303375B2Refractory metal core cooling technologies for curved leading edge slotsUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 4, 2007·27 cites·10 claims
- 1387US5779437ACooling passages for airfoil leading edgePRATT & WHITNEY CANADA·Filed 1996·Granted Jul 14, 1998·94 cites·7 claims
- 1486US7607891B2Turbine component with tip flagged pedestal coolingUNITED TECHNOLOGIES CORP·Filed 2006·Granted Oct 27, 2009·26 cites·13 claims
- 1585US8157527B2Airfoil with tapered radial cooling passagePIGGUSH JUSTIN D·Filed 2008·Granted Apr 17, 2012·24 cites·9 claims
- 1685US6257831B1Cast airfoil structure with openings which do not require pluggingPRATT & WHITNEY CANADA·Filed 1999·Granted Jul 10, 2001·71 cites·15 claims
- 1784US7901180B2Enhanced turbine airfoil coolingUNITED TECHNOLOGIES CORP·Filed 2007·Granted Mar 8, 2011·18 cites·29 claims
- 1882US6406260B1Heat transfer promotion structure for internally convectively cooled airfoilsPRATT & WHITNEY CANADA·Filed 1999·Granted Jun 18, 2002·69 cites·41 claims
- 1980US7445432B2Enhanced serpentine cooling with U-shaped divider ribUNITED TECHNOLOGIES CORP·Filed 2006·Granted Nov 4, 2008·20 cites·19 claims
- 2079US8210812B2Advanced turbulator arrangements for microcircuitsABDEL-MESSEH WILLIAM·Filed 2008·Granted Jul 3, 2012·8 cites·17 claims
- 2179US7708525B2Industrial gas turbine blade assemblyUNITED TECHNOLOGIES CORP·Filed 2005·Granted May 4, 2010·18 cites·19 claims
- 2276US8348614B2Coolable airfoil trailing edge passageUNITED TECHNOLOGIES CORP·Filed 2008·Granted Jan 8, 2013·14 cites·21 claims
- 2376US8016546B2Systems and methods for providing vane platform coolingUNITED TECHNOLOGIES CORP·Filed 2007·Granted Sep 13, 2011·17 cites·20 claims
- 2475US8333233B2Airfoil with wrapped leading edge cooling passageABDEL-MESSEH WILLIAM·Filed 2012·Granted Dec 18, 2012·4 cites·9 claims
- 2574US8105031B2Cooling arrangement for turbine componentsTRINDADE RICARDO·Filed 2008·Granted Jan 31, 2012·16 cites·17 claims
- 2673US5711650AGas turbine airfoil coolingPRATT & WHITNEY CANADA·Filed 1996·Granted Jan 27, 1998·54 cites·6 claims
- 2771US8220522B2Peripheral microcircuit serpentine cooling for turbine airfoilsCUNHA FRANK J·Filed 2011·Granted Jul 17, 2012·2 cites·10 claims
- 2871US7513745B2Advanced turbulator arrangements for microcircuitsUNITED TECHNOLOGIES CORP·Filed 2006·Granted Apr 7, 2009·10 cites·6 claims
- 2968US6997675B2Turbulated hole configurations for turbine bladesUNITED TECHNOLOGIES CORP·Filed 2004·Granted Feb 14, 2006·24 cites·18 claims
- 3067US8177506B2Microcircuit cooling with an aspect ratio of unityCUNHA FRANCISCO J·Filed 2006·Granted May 15, 2012·10 cites·22 claims
- 3167US7553131B2Integrated platform, tip, and main body microcircuits for turbine bladesUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jun 30, 2009·9 cites·18 claims
- 3260US8690538B2Leading edge cooling using chevron trip stripsLEVINE JEFFREY R·Filed 2006·Granted Apr 8, 2014·8 cites·6 claims
- 3357US8215374B2Peripheral microcircuit serpentine cooling for turbine airfoilsCUNHA FRANK J·Filed 2010·Granted Jul 10, 2012·0 cites·8 claims
- 3455US7114916B2Tailored turbulation for turbine bladesUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 3, 2006·15 cites·22 claims
- 3546US2013052037A1Airfoil with nonlinear cooling passageABDEL-MESSEH WILLIAM·Filed 2011·Application pending·0 cites
- 3643US2010054915A1Airfoil insertUNITED TECHNOLOGIES CORP·Filed 2008·Application pending·0 cites
- 3741US2008008599A1Integral main body-tip microcircuits for bladesUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
- 3838US2007297916A1Leading edge cooling using wrapped staggered-chevron trip stripsUNITED TECHNOLOGIES CORP·Filed 2006·Application pending·0 cites
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