Inventor
CHERRY DAVID GLENN
US16 patents
Patents
16 patentsUS6790005B2Sep 14, 2004
Compound tip notched blade
GEN ELECTRIC124 citations98
US6672829B1Jan 6, 2004
Turbine blade having angled squealer tip
GEN ELECTRIC128 citations98
US7806653B2Oct 5, 2010
Gas turbine engines including multi-curve stator vanes and methods of assembling the same
GEN ELECTRIC68 citations96
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
US7628585B2Dec 8, 2009
Airfoil leading edge end wall vortex reducing plasma
GEN ELECTRIC28 citations92
US7594388B2Sep 29, 2009
Counterrotating turbofan engine
GEN ELECTRIC35 citations92
US7588413B2Sep 15, 2009
Upstream plasma shielded film cooling
GEN ELECTRIC28 citations92
US7513102B2Apr 7, 2009
Integrated counterrotating turbofan
GEN ELECTRIC48 citations92
US7510371B2Mar 31, 2009
Forward tilted turbine nozzle
GEN ELECTRIC41 citations92
US7097426B2Aug 29, 2006
Cascade impingement cooled airfoil
GEN ELECTRIC40 citations92
US7758306B2Jul 20, 2010
Turbine assembly for a gas turbine engine and method of manufacturing the same
GEN ELECTRIC34 citations91
US7794201B2Sep 14, 2010
Gas turbine engines including lean stator vanes and methods of assembling the same
GEN ELECTRIC7 citations72