Inventor · disambiguated record
Anthony R. Bifulco
Also filed as: BIFULCO ANTHONY R
48 granted patents·7 pending applications·116 citations·filing 2002–2024
97Inventor score
Top patents by PatentIndex Score
55 records- 0193US11339720B2Acoustic liner with non-uniform volumetric distributionRAYTHEON TECH CORP·Filed 2020·Granted May 24, 2022·8 cites·20 claims
- 0293US11143303B2Non-metallic engine case inlet compression seal for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Oct 12, 2021·5 cites·8 claims
- 0393US10077669B2Non-metallic engine case inlet compression seal for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 18, 2018·9 cites·17 claims
- 0492US11555420B1Frame connection between fan case and core housing in a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Jan 17, 2023·2 cites·20 claims
- 0592US9121412B2Efficient, low pressure ratio propulsor for gas turbine enginesGALLAGHER EDWARD J·Filed 2011·Granted Sep 1, 2015·14 cites·11 claims
- 0691US9920708B2Nose cone assembly and method of circulating air in a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Mar 20, 2018·7 cites·19 claims
- 0787US11560811B2Stator outer platform sealing and retainerUNITED TECHNOLOGIES CORP·Filed 2020·Granted Jan 24, 2023·2 cites·5 claims
- 0887US11480106B2Acoustic liner with obliquely angled slotsUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 25, 2022·3 cites·18 claims
- 0986US12281702B2Non-metallic engine case inlet compression seal for a gas turbine engineRTX CORP·Filed 2024·Granted Apr 22, 2025·0 cites·4 claims
- 1082US12188409B2Gas turbine engine with acoustic linerRTX CORP·Filed 2021·Granted Jan 7, 2025·1 cites·14 claims
- 1180US9890711B2Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion eventsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Feb 13, 2018·4 cites·12 claims
- 1279US2025092826A1Core compartment vent during engine shutdown to reduced bowed rotor startRTX CORP·Filed 2024·Application pending·0 cites
- 1378US10024238B2Cooling system with a bearing compartment bypassUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 17, 2018·3 cites·17 claims
- 1477US11988283B2Non-metallic engine case inlet compression seal for a gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted May 21, 2024·0 cites·4 claims
- 1577US8540483B2Turbine engine rotating cavity anti-vortex cascadeBINTZ MATTHEW E·Filed 2012·Granted Sep 24, 2013·5 cites·4 claims
- 1674US12308007B2Acoustic attenuation structuresRTX CORP·Filed 2023·Granted May 20, 2025·0 cites·3 claims
- 1774US11566564B2Acoustically treated panelsRAYTHEON TECH CORP·Filed 2021·Granted Jan 31, 2023·1 cites·19 claims
- 1873US12503988B2Radial strut frame connection between fan case and core housing in a gas turbine engineRTX CORP·Filed 2023·Granted Dec 23, 2025·0 cites·16 claims
- 1973US12158107B2Core compartment vent during engine shutdown to reduced bowed rotor startRTX CORP·Filed 2023·Granted Dec 3, 2024·0 cites·16 claims
- 2073US6884025B2Shim lock/pin anti-rotation bumper designUNITED TECHNOLOGIES CORP·Filed 2002·Granted Apr 26, 2005·28 cites·23 claims
- 2172US11927106B2Frame connection between fan case and core housing in a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Mar 12, 2024·0 cites·20 claims
- 2272US10294813B2Geared unison ring for variable vane actuationUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 21, 2019·1 cites·23 claims
- 2372US10287904B2Multi-element inner shroud extension for a turbo-machineUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 14, 2019·4 cites·17 claims
- 2469US11608796B1Radial strut frame connection between fan case and core housing in a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Mar 21, 2023·0 cites·18 claims
- 2567US10358934B2Method and apparatus for adjusting variable vanesUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 23, 2019·1 cites·18 claims
- 2666US11887571B2Acoustic attenuation structuresRAYTHEON TECH CORP·Filed 2020·Granted Jan 30, 2024·0 cites·13 claims
- 2763US10370971B2Reinforced gas turbine engine rotor diskUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·1 cites·20 claims
- 2861US12326114B2Gas turbine engine with core debris protectionRTX CORP·Filed 2023·Granted Jun 10, 2025·0 cites·16 claims
- 2961US11286856B2Diversion of fan air to provide cooling air for gas turbine engineRAYTHEON TECH CORP·Filed 2019·Granted Mar 29, 2022·0 cites·20 claims
- 3060US8287242B2Turbine engine rotor hubBIFULCO ANTHONY R·Filed 2008·Granted Oct 16, 2012·9 cites·27 claims
- 3159US10612405B2Stator outer platform sealing and retainerUNITED TECHNOLOGIES CORP·Filed 2017·Granted Apr 7, 2020·0 cites·12 claims
- 3259US8177503B2Turbine engine rotating cavity anti-vortex cascadeBINTZ MATTHEW E·Filed 2009·Granted May 15, 2012·5 cites·4 claims
- 3358US11686220B2H-frame connection between fan case and core housing in a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Jun 27, 2023·0 cites·20 claims
- 3458US10584598B2Complaint cantilevered airfoilUNITED TECHNOLOGIES CORP·Filed 2013·Granted Mar 10, 2020·1 cites·19 claims
- 3555US10648479B2Stator segment circumferential gap sealUNITED TECHNOLOGIES CORP·Filed 2017·Granted May 12, 2020·0 cites·9 claims
- 3654US11572800B2Borescope port engine fluid washRAYTHEON TECH CORP·Filed 2021·Granted Feb 7, 2023·0 cites·14 claims
- 3754US10309235B2Shiplap cantilevered statorJACQUES NORMAND P·Filed 2012·Granted Jun 4, 2019·2 cites·16 claims
- 3853US11708772B2Triangular-frame connection between fan case and core housing in a gas turbine engineRAYTHEON TECH CORP·Filed 2022·Granted Jul 25, 2023·0 cites·20 claims
- 3953US10253694B2Diversion of fan air to provide cooling air for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 9, 2019·0 cites·16 claims
- 4052US11268388B2Composite reinforced rotorRAYTHEON TECH CORP·Filed 2020·Granted Mar 8, 2022·0 cites·14 claims
- 4151US11834997B2Face sheet of acoustic liner having streamlined holes with elongated edgesRTX CORP·Filed 2022·Granted Dec 5, 2023·0 cites·19 claims
- 4251US11512608B2Passive transpirational flow acoustically lined guide vaneRAYTHEON TECH CORP·Filed 2020·Granted Nov 29, 2022·0 cites·20 claims
- 4351US2014144151A1Engine Compressor Wash SystemUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 4449US10975915B2Assembly alignment handling damage tolerant splineUNITED TECHNOLOGIES CORP·Filed 2018·Granted Apr 13, 2021·0 cites·11 claims
- 4549US10330009B2Lock for threaded in place nosecone or spinnerUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 25, 2019·0 cites·19 claims
- 4648US10794217B2Bleed valve systemUNITED TECHNOLOGIES CORP·Filed 2017·Granted Oct 6, 2020·0 cites·14 claims
- 4748US2017002834A1Cooled compressorUNITED TECHNOLOGIES CORP·Filed 2014·Application pending·0 cites
- 4847US2015247461A1Geared turbofan with high fan rotor power intensityUNITED TECHNOLOGIES CORP·Filed 2013·Application pending·0 cites
- 4946US10029336B2Rotor with blades secured by woven fiber attachment systemUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 24, 2018·0 cites·16 claims
- 5046US2021317785A1Cooling system for a gas turbine engineRAYTHEON TECH CORP·Filed 2020·Application pending·0 cites
Showing the top 50 of 55 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →