Inventor
PROSCIA WILLIAM
US17 patents
⚠️ This page may combine multiple inventors who share the name “PROSCIA WILLIAM”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
12 patentsUS7337875B2Mar 4, 2008
High admittance acoustic liner
UNITED TECHNOLOGIES CORP60 citations97
US7401682B2Jul 22, 2008
Architecture for an acoustic liner
UNITED TECHNOLOGIES CORP43 citations92
US7311175B2Dec 25, 2007
Acoustic liner with bypass cooling
UNITED TECHNOLOGIES CORP36 citations92
US8037688B2Oct 18, 2011
Method for control of thermoacoustic instabilities in a combustor
UNITED TECHNOLOGIES CORP32 citations91
US6543232B1Apr 8, 2003
Valve assembly for use in a gas fuel nozzle
UNITED TECHNOLOGIES CORP14 citations82
US10738704B2Aug 11, 2020
Pilot/main fuel shifting in an axial staged combustor for a gas turbine engine
UNITED TECHNOLOGIES CORP2 citations72
US10739003B2Aug 11, 2020
Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine
UNITED TECHNOLOGIES CORP4 citations72
US11378275B2Jul 5, 2022
High shear swirler with recessed fuel filmer for a gas turbine engine
UNITED TECHNOLOGIES CORP4 citations71
US7552796B2Jun 30, 2009
Turbine engine tailcone resonator
UNITED TECHNOLOGIES CORP7 citations65
US11365884B2Jun 21, 2022
Radial fuel shifting and biasing in an axial staged combustor for a gas turbine engine
UNITED TECHNOLOGIES CORP1 citations62
US10508811B2Dec 17, 2019
Circumferential fuel shifting and biasing in an axial staged combustor for a gas turbine engine
UNITED TECHNOLOGIES CORP1 citations62
US11598527B2Mar 7, 2023
Reducing noise from a combustor of a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations53