Inventor
ABDEL-MESSEH WILLIAM
CA34 patents
⚠️ This page may combine multiple inventors who share the name “ABDEL-MESSEH WILLIAM”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
16 patentsUS7744347B2Jun 29, 2010
Peripheral microcircuit serpentine cooling for turbine airfoils
UNITED TECHNOLOGIES CORP16 citations92
US7607891B2Oct 27, 2009
Turbine component with tip flagged pedestal cooling
UNITED TECHNOLOGIES CORP26 citations92
US7311498B2Dec 25, 2007
Microcircuit cooling for blades
UNITED TECHNOLOGIES CORP30 citations92
US7303375B2Dec 4, 2007
Refractory metal core cooling technologies for curved leading edge slots
UNITED TECHNOLOGIES CORP27 citations92
US6997675B2Feb 14, 2006
Turbulated hole configurations for turbine blades
UNITED TECHNOLOGIES CORP24 citations92
US7553128B2Jun 30, 2009
Blade outer air seals
UNITED TECHNOLOGIES CORP49 citations91
US7445432B2Nov 4, 2008
Enhanced serpentine cooling with U-shaped divider rib
UNITED TECHNOLOGIES CORP20 citations90
US7988418B2Aug 2, 2011
Microcircuits for small engines
UNITED TECHNOLOGIES CORP11 citations84
US7695246B2Apr 13, 2010
Microcircuits for small engines
UNITED TECHNOLOGIES CORP13 citations84
US7553131B2Jun 30, 2009
Integrated platform, tip, and main body microcircuits for turbine blades
UNITED TECHNOLOGIES CORP9 citations84
US7513745B2Apr 7, 2009
Advanced turbulator arrangements for microcircuits
UNITED TECHNOLOGIES CORP10 citations84
US8016546B2Sep 13, 2011
Systems and methods for providing vane platform cooling
UNITED TECHNOLOGIES CORP17 citations83
US7114916B2Oct 3, 2006
Tailored turbulation for turbine blades
UNITED TECHNOLOGIES CORP15 citations83
US7901180B2Mar 8, 2011
Enhanced turbine airfoil cooling
UNITED TECHNOLOGIES CORP18 citations78
US7708525B2May 4, 2010
Industrial gas turbine blade assembly
UNITED TECHNOLOGIES CORP18 citations78
US8348614B2Jan 8, 2013
Coolable airfoil trailing edge passage
UNITED TECHNOLOGIES CORP14 citations77
PRATT & WHITNEY CANADA
5 patentsUS6406260B1Jun 18, 2002
Heat transfer promotion structure for internally convectively cooled airfoils
PRATT & WHITNEY CANADA69 citations96
US6257831B1Jul 10, 2001
Cast airfoil structure with openings which do not require plugging
PRATT & WHITNEY CANADA71 citations96
US6508620B2Jan 21, 2003
Inner platform impingement cooling by supply air from outside
PRATT & WHITNEY CANADA90 citations95
US5779437AJul 14, 1998
Cooling passages for airfoil leading edge
PRATT & WHITNEY CANADA94 citations94
US5711650AJan 27, 1998
Gas turbine airfoil cooling
PRATT & WHITNEY CANADA54 citations92
ABDEL-MESSEH WILLIAM
4 patentsUS8105030B2Jan 31, 2012
Cooled airfoils and gas turbine engine systems involving such airfoils
ABDEL-MESSEH WILLIAM49 citations93
US8109725B2Feb 7, 2012
Airfoil with wrapped leading edge cooling passage
ABDEL-MESSEH WILLIAM25 citations92
US8210812B2Jul 3, 2012
Advanced turbulator arrangements for microcircuits
ABDEL-MESSEH WILLIAM8 citations83
US8333233B2Dec 18, 2012
Airfoil with wrapped leading edge cooling passage
ABDEL-MESSEH WILLIAM4 citations62