Inventor
WADIA ASPI RUSTOM
US37 patents
⚠️ This page may combine multiple inventors who share the name “WADIA ASPI RUSTOM”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
GEN ELECTRIC
32 patentsUS7296973B2Nov 20, 2007
Parallel serpentine cooled blade
GEN ELECTRIC71 citations98
US7249933B2Jul 31, 2007
Funnel fillet turbine stage
GEN ELECTRIC95 citations98
US6790005B2Sep 14, 2004
Compound tip notched blade
GEN ELECTRIC124 citations98
US6672829B1Jan 6, 2004
Turbine blade having angled squealer tip
GEN ELECTRIC128 citations98
US7476086B2Jan 13, 2009
Tip cambered swept blade
GEN ELECTRIC96 citations95
US6561760B2May 13, 2003
Booster compressor deicer
GEN ELECTRIC85 citations94
US7870719B2Jan 18, 2011
Plasma enhanced rapidly expanded gas turbine engine transition duct
GEN ELECTRIC19 citations92
US7819626B2Oct 26, 2010
Plasma blade tip clearance control
GEN ELECTRIC41 citations92
US7766599B2Aug 3, 2010
Plasma lifted boundary layer gas turbine engine vane
GEN ELECTRIC20 citations92
US7736123B2Jun 15, 2010
Plasma induced virtual turbine airfoil trailing edge extension
GEN ELECTRIC31 citations92
US7695241B2Apr 13, 2010
Downstream plasma shielded film cooling
GEN ELECTRIC26 citations92
US7695243B2Apr 13, 2010
Dust hole dome blade
GEN ELECTRIC35 citations92
US7628585B2Dec 8, 2009
Airfoil leading edge end wall vortex reducing plasma
GEN ELECTRIC28 citations92
US7588413B2Sep 15, 2009
Upstream plasma shielded film cooling
GEN ELECTRIC28 citations92
US7293961B2Nov 13, 2007
Zigzag cooled turbine airfoil
GEN ELECTRIC34 citations92
US7217092B2May 15, 2007
Method and apparatus for reducing turbine blade temperatures
GEN ELECTRIC27 citations92
US7097426B2Aug 29, 2006
Cascade impingement cooled airfoil
GEN ELECTRIC40 citations92
US7827803B1Nov 9, 2010
Method and apparatus for an aerodynamic stability management system
GEN ELECTRIC43 citations91
US7758303B1Jul 20, 2010
FLADE fan with different inner and outer airfoil stagger angles at a shroud therebetween
GEN ELECTRIC42 citations91
US7320575B2Jan 22, 2008
Methods and apparatus for aerodynamically self-enhancing rotor blades
GEN ELECTRIC25 citations91
US10914318B2Feb 9, 2021
Engine casing treatment for reducing circumferentially variable distortion
GEN ELECTRIC11 citations84
US7287959B2Oct 30, 2007
Blunt tip turbine blade
GEN ELECTRIC13 citations84
US10883515B2Jan 5, 2021
Method and system for leading edge auxiliary vanes
GEN ELECTRIC9 citations82
US11149552B2Oct 19, 2021
Shroud for splitter and rotor airfoils of a fan for a gas turbine engine
GEN ELECTRIC8 citations80
US10385871B2Aug 20, 2019
Method and system for compressor vane leading edge auxiliary vanes
GEN ELECTRIC10 citations79
US10253637B2Apr 9, 2019
Method and system for improving turbine blade performance
GEN ELECTRIC4 citations69
US11125089B2Sep 21, 2021
Turbine incorporating endwall fences
GEN ELECTRIC4 citations68
US12221898B2Feb 11, 2025
Turbine incorporating splitters
GEN ELECTRIC0 citations60
US8348592B2Jan 8, 2013
Instability mitigation system using rotor plasma actuators
GEN ELECTRIC4 citations60
US10934858B2Mar 2, 2021
Method and system for improving turbine blade performance
GEN ELECTRIC1 citations59
US11002141B2May 11, 2021
Method and system for leading edge auxiliary turbine vanes
GEN ELECTRIC1 citations55
US10670037B2Jun 2, 2020
Turbofan engine's fan blade and setting method thereof
GEN ELECTRIC0 citations49