Inventor
GRAZIOSI PAOLO
US8 patents
Patents
8 patentsUS6655632B1Dec 2, 2003
System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine
GEN ELECTRIC104 citations97
US6851264B2Feb 8, 2005
Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine
GEN ELECTRIC87 citations95
US6896475B2May 24, 2005
Fluidic actuation for improved diffuser performance
GEN ELECTRIC61 citations94
US7549282B2Jun 23, 2009
Multi-slot inter-turbine duct assembly for use in a turbine engine
GEN ELECTRIC25 citations92
US7137245B2Nov 21, 2006
High area-ratio inter-turbine duct with inlet blowing
GEN ELECTRIC23 citations92
US7631483B2Dec 15, 2009
Method and system for reduction of jet engine noise
GEN ELECTRIC47 citations91
US6775983B2Aug 17, 2004
Flow control device for a combustor
GEN ELECTRIC4 citations61
US7581692B2Sep 1, 2009
Fluidic chevrons and configurable thermal shield for jet noise reduction
GEN ELECTRIC5 citations60