William Proscia

Person

Marlborough, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Reducing noise from a combustor of a gas turbine engine
- Patent number 12,359,814
- Issue date Jul 15, 2025
- RTX Corporation
- Justin M Locke
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Reducing noise from a combustor of a gas turbine engine
- Patent number 11,598,527
- Issue date Mar 7, 2023
- Raytheon Technologies Corporation
- Justin M. Locke
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
High shear swirler with recessed fuel filmer for a gas turbine engine
- Patent number 11,378,275
- Issue date Jul 5, 2022
- Raytheon Technologies Corporation
- Justin M. Locke
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Radial fuel shifting and biasing in an axial staged combustor for a...
- Patent number 11,365,884
- Issue date Jun 21, 2022
- Raytheon Technologies Corporation
- William Proscia
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Controlled contact surface for a secondary seal in a non-contact se...
- Patent number 11,230,940
- Issue date Jan 25, 2022
- Raytheon Technologies Corporation
- Michael G. McCaffrey
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Radial fuel shifting and biasing in an axial staged combustor for a...
- Patent number 10,739,003
- Issue date Aug 11, 2020
- United Technologies Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Pilot/main fuel shifting in an axial staged combustor for a gas tur...
- Patent number 10,738,704
- Issue date Aug 11, 2020
- Raytheon Technologies Corporation
- William Proscia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Circumferential fuel shifting and biasing in an axial staged combus...
- Patent number 10,508,811
- Issue date Dec 17, 2019
- United Technologies Corporation
- William Proscia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Pilot injector fuel shifting in an axial staged combustor for a gas...
- Patent number 10,393,030
- Issue date Aug 27, 2019
- United Technologies Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel-air mixture distribution for gas turbine engine combustors
- Patent number 9,631,560
- Issue date Apr 25, 2017
- United Technologies Corporation
- James B. Hoke
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Low pressure drop, low NOx, induced draft gas heaters
- Patent number 9,127,837
- Issue date Sep 8, 2015
- Carrier Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Method for control of thermoacoustic instabilities in a combustor
- Patent number 8,037,688
- Issue date Oct 18, 2011
- United Technologies Corporation
- Gregory S. Hagen
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Turbine engine tailcone resonator
- Patent number 7,552,796
- Issue date Jun 30, 2009
- United Technologies Corporation
- Jenny N. Baarck
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Architecture for an acoustic liner
- Patent number 7,401,682
- Issue date Jul 22, 2008
- United Technologies Corporation
- William Proscia
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
High admittance acoustic liner
- Patent number 7,337,875
- Issue date Mar 4, 2008
- United Technologies Corporation
- William Proscia
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Grant
Acoustic liner with bypass cooling
- Patent number 7,311,175
- Issue date Dec 25, 2007
- United Technologies Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Valve assembly for use in a gas fuel nozzle
- Patent number 6,543,232
- Issue date Apr 8, 2003
- United Technologies Corporation
- Torger J. Anderson
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Method and apparatus to enhance combustion rates and extend extinct...
- Patent number 5,394,685
- Issue date Mar 7, 1995
- United Technologies Corporation
- Arthur S. Kesten
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINE
- Publication number 20240102655
- Publication date Mar 28, 2024
- Raytheon Technologies Corporation
- Justin M Locke
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
HIGH SHEAR SWIRLER WITH RECESSED FUEL FILMER
- Publication number 20210172604
- Publication date Jun 10, 2021
- Justin M. Locke
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
RADIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUSTOR FOR A...
- Publication number 20200217508
- Publication date Jul 9, 2020
- United Technologies Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
PILOT/MAIN FUEL SHIFTING IN AN AXIAL STAGED COMBUSTOR FOR A GAS TUR...
- Publication number 20180163629
- Publication date Jun 14, 2018
- United Technologies Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
CIRCUMFERENTIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUS...
- Publication number 20180094817
- Publication date Apr 5, 2018
- United Technologies Corporation
- William Proscia
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PILOT INJECTOR FUEL SHIFTING IN AN AXIAL STAGED COMBUSTOR FOR A GAS...
- Publication number 20180094590
- Publication date Apr 5, 2018
- United Technologies Corporatoin
- William Proscia
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
RADIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUSTOR FOR A...
- Publication number 20180094814
- Publication date Apr 5, 2018
- United Technologies Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINE
- Publication number 20170356654
- Publication date Dec 14, 2017
- United Technologies Corporation
- Justin M. Locke
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
FUEL-AIR MIXTURE DISTRIBUTION FOR GAS TURBINE ENGINE COMBUSTORS
- Publication number 20130125556
- Publication date May 23, 2013
- James B. Hoke
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Low Pressure Drop, Low NOx, Induced Draft Gas Heaters
- Publication number 20110311924
- Publication date Dec 22, 2011
- Carrier Corporation
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Method for control of thermoacoustic instabilities in a combustor
- Publication number 20080072605
- Publication date Mar 27, 2008
- United Technologies Corporation
- Gregory S. Hagen
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Turbine engine tailcone resonator
- Publication number 20070251760
- Publication date Nov 1, 2007
- United Technologies Corporation
- Jenny N. Baarck
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Acoustic liner with bypass cooling
- Publication number 20070034447
- Publication date Feb 15, 2007
- William Proscia
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Architecture for an acoustic liner
- Publication number 20070034446
- Publication date Feb 15, 2007
- William Proscia
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
Augmentor liner
- Publication number 20060137352
- Publication date Jun 29, 2006
- United Technologies Corporation
- Dilip Prasad
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
High admittance acoustic liner
- Publication number 20050284690
- Publication date Dec 29, 2005
- William Proscia
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
VALVE ASSEMBLY FOR USE IN A GAS FUEL NOZZLE
- Publication number 20030056490
- Publication date Mar 27, 2003
- Torger J. Anderson
- Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC

William Proscia

Person

Patents Grantslast 30 patents

Reducing noise from a combustor of a gas turbine engine

Reducing noise from a combustor of a gas turbine engine

High shear swirler with recessed fuel filmer for a gas turbine engine

Radial fuel shifting and biasing in an axial staged combustor for a...

Controlled contact surface for a secondary seal in a non-contact se...

Radial fuel shifting and biasing in an axial staged combustor for a...

Pilot/main fuel shifting in an axial staged combustor for a gas tur...

Circumferential fuel shifting and biasing in an axial staged combus...

Pilot injector fuel shifting in an axial staged combustor for a gas...

Fuel-air mixture distribution for gas turbine engine combustors

Low pressure drop, low NOx, induced draft gas heaters

Method for control of thermoacoustic instabilities in a combustor

Turbine engine tailcone resonator

Architecture for an acoustic liner

High admittance acoustic liner

Acoustic liner with bypass cooling

Valve assembly for use in a gas fuel nozzle

Method and apparatus to enhance combustion rates and extend extinct...

Patents Applicationslast 30 patents

REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINE

HIGH SHEAR SWIRLER WITH RECESSED FUEL FILMER

RADIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUSTOR FOR A...

PILOT/MAIN FUEL SHIFTING IN AN AXIAL STAGED COMBUSTOR FOR A GAS TUR...

CIRCUMFERENTIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUS...

PILOT INJECTOR FUEL SHIFTING IN AN AXIAL STAGED COMBUSTOR FOR A GAS...

RADIAL FUEL SHIFTING AND BIASING IN AN AXIAL STAGED COMBUSTOR FOR A...

REDUCING NOISE FROM A COMBUSTOR OF A GAS TURBINE ENGINE

FUEL-AIR MIXTURE DISTRIBUTION FOR GAS TURBINE ENGINE COMBUSTORS

Low Pressure Drop, Low NOx, Induced Draft Gas Heaters

Method for control of thermoacoustic instabilities in a combustor

Turbine engine tailcone resonator

Acoustic liner with bypass cooling

Architecture for an acoustic liner

Augmentor liner

High admittance acoustic liner

VALVE ASSEMBLY FOR USE IN A GAS FUEL NOZZLE