Inventor · disambiguated record
William Proscia
Also filed as: PROSCIA WILLIAM · PROSCIA WILLIAM M
18 granted patents·1 pending application·253 citations·filing 1990–2023
94Inventor score
Files withUNITED TECHNOLOGIES CORP14RAYTHEON TECH CORP2HOKE JAMES B1PROSCIA WILLIAM1UNITED TECH CORPORATOIN1
Top patents by PatentIndex Score
19 records- 0194US7401682B2Architecture for an acoustic linerUNITED TECHNOLOGIES CORP·Filed 2005·Granted Jul 22, 2008·43 cites·26 claims
- 0292US8037688B2Method for control of thermoacoustic instabilities in a combustorUNITED TECHNOLOGIES CORP·Filed 2006·Granted Oct 18, 2011·32 cites·24 claims
- 0391US11230940B1Controlled contact surface for a secondary seal in a non-contact seal assemblyRAYTHEON TECH CORP·Filed 2020·Granted Jan 25, 2022·11 cites·20 claims
- 0491US7311175B2Acoustic liner with bypass coolingUNITED TECHNOLOGIES CORP·Filed 2005·Granted Dec 25, 2007·36 cites·21 claims
- 0590US7337875B2High admittance acoustic linerUNITED TECHNOLOGIES CORP·Filed 2004·Granted Mar 4, 2008·60 cites·16 claims
- 0689US10739003B2Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 11, 2020·4 cites·28 claims
- 0786US11378275B2High shear swirler with recessed fuel filmer for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2019·Granted Jul 5, 2022·4 cites·13 claims
- 0883US10393030B2Pilot injector fuel shifting in an axial staged combustor for a gas turbine engineUNITED TECH CORPORATOIN·Filed 2016·Granted Aug 27, 2019·3 cites·19 claims
- 0978US11365884B2Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2020·Granted Jun 21, 2022·1 cites·17 claims
- 1076US10738704B2Pilot/main fuel shifting in an axial staged combustor for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 11, 2020·2 cites·8 claims
- 1171US9127837B2Low pressure drop, low NOx, induced draft gas heatersPROSCIA WILLIAM·Filed 2011·Granted Sep 8, 2015·3 cites·6 claims
- 1269US12359814B2Reducing noise from a combustor of a gas turbine engineRAYTHEON TECH CORP·Filed 2023·Granted Jul 15, 2025·0 cites·14 claims
- 1369US10508811B2Circumferential fuel shifting and biasing in an axial staged combustor for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Dec 17, 2019·1 cites·23 claims
- 1469US5394685AMethod and apparatus to enhance combustion rates and extend extinction limits in high speed propulsion unitsUNITED TECHNOLOGIES CORP·Filed 1990·Granted Mar 7, 1995·30 cites·10 claims
- 1563US9631560B2Fuel-air mixture distribution for gas turbine engine combustorsHOKE JAMES B·Filed 2011·Granted Apr 25, 2017·2 cites·19 claims
- 1653US11598527B2Reducing noise from a combustor of a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 7, 2023·0 cites·19 claims
- 1753US7552796B2Turbine engine tailcone resonatorUNITED TECHNOLOGIES CORP·Filed 2006·Granted Jun 30, 2009·7 cites·27 claims
- 1853US6543232B1Valve assembly for use in a gas fuel nozzleUNITED TECHNOLOGIES CORP·Filed 2001·Granted Apr 8, 2003·14 cites·17 claims
- 1932US2006137352A1Augmentor linerUNITED TECHNOLOGIES CORP·Filed 2004·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →