Graziosi; Paolo

Patent Applications and Registrations

Patent applications and USPTO patent grants for Graziosi; Paolo.The latest application filed is for "multi-slot inter-turbine duct assembly for use in a turbine engine".

Company Profile

0.8.7

Graziosi; Paolo - Clifton Park NY
Graziosi; Paolo - Rome IT

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Method and system for reduction of jet engine noise Grant 7,631,483 - Mani , et al. December 15, 2	2009-12-15
Fluidic chevrons and configurable thermal shield for jet noise reduction Grant 7,581,692 - Graziosi , et al. September 1, 2	2009-09-01
Multi-slot inter-turbine duct assembly for use in a turbine engine Grant 7,549,282 - Widenhoefer , et al. June 23, 2	2009-06-23
Multi-slot inter-turbine duct assembly for use in a turbine engine App 20070089422 - Widenhoefer; James Fredric ; et al.	2007-04-26
High area-ratio inter-turbine duct with inlet blowing Grant 7,137,245 - Graziosi , et al. November 21, 2	2006-11-21
High area-ratio inter-turbine duct with inlet blowing App 20050279100 - Graziosi, Paolo ; et al.	2005-12-22
Fluidic actuation for improved diffuser performance Grant 6,896,475 - Graziosi , et al. May 24, 2	2005-05-24
Method and system for reduction of jet engine noise App 20050060982 - Mani, Ramani ; et al.	2005-03-24
Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine Grant 6,851,264 - Kirtley , et al. February 8, 2	2005-02-08
Fluidic chevrons and configurable thermal shield for jet noise reduction App 20040262447 - Graziosi, Paolo ; et al.	2004-12-30
Flow control device for a combustor Grant 6,775,983 - Sanderson , et al. August 17, 2	2004-08-17
Fluidic actuation for improved diffuser performance App 20040091350 - Graziosi, Paolo ; et al.	2004-05-13
Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine App 20040079084 - Kirtley, Kevin ; et al.	2004-04-29
System and method for actively changing an effective flow-through area of an inlet region of an aircraft engine Grant 6,655,632 - Gupta , et al. December 2, 2	2003-12-02
Flow control device for a combustor App 20030217544 - Sanderson, Simon Ralph ; et al.	2003-11-27

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