Inventor
BIFULCO ANTHONY R
US50 patents
⚠️ This page may combine multiple inventors who share the name “BIFULCO ANTHONY R”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
UNITED TECHNOLOGIES CORP
23 patentsUS6884025B2Apr 26, 2005
Shim lock/pin anti-rotation bumper design
UNITED TECHNOLOGIES CORP28 citations91
US11143303B2Oct 12, 2021
Non-metallic engine case inlet compression seal for a gas turbine engine
UNITED TECHNOLOGIES CORP5 citations84
US10077669B2Sep 18, 2018
Non-metallic engine case inlet compression seal for a gas turbine engine
UNITED TECHNOLOGIES CORP9 citations84
US9920708B2Mar 20, 2018
Nose cone assembly and method of circulating air in a gas turbine engine
UNITED TECHNOLOGIES CORP7 citations84
US11560811B2Jan 24, 2023
Stator outer platform sealing and retainer
UNITED TECHNOLOGIES CORP2 citations73
US11480106B2Oct 25, 2022
Acoustic liner with obliquely angled slots
UNITED TECHNOLOGIES CORP3 citations73
US10287904B2May 14, 2019
Multi-element inner shroud extension for a turbo-machine
UNITED TECHNOLOGIES CORP4 citations71
US9890711B2Feb 13, 2018
Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events
UNITED TECHNOLOGIES CORP4 citations71
US10024238B2Jul 17, 2018
Cooling system with a bearing compartment bypass
UNITED TECHNOLOGIES CORP3 citations70
US10358934B2Jul 23, 2019
Method and apparatus for adjusting variable vanes
UNITED TECHNOLOGIES CORP1 citations62
US10294813B2May 21, 2019
Geared unison ring for variable vane actuation
UNITED TECHNOLOGIES CORP1 citations62
US10584598B2Mar 10, 2020
Complaint cantilevered airfoil
UNITED TECHNOLOGIES CORP1 citations61
US10370971B2Aug 6, 2019
Reinforced gas turbine engine rotor disk
UNITED TECHNOLOGIES CORP1 citations59
US10975915B2Apr 13, 2021
Assembly alignment handling damage tolerant spline
UNITED TECHNOLOGIES CORP0 citations54
US10612405B2Apr 7, 2020
Stator outer platform sealing and retainer
UNITED TECHNOLOGIES CORP0 citations52
US10253694B2Apr 9, 2019
Diversion of fan air to provide cooling air for gas turbine engine
UNITED TECHNOLOGIES CORP0 citations52
US10648479B2May 12, 2020
Stator segment circumferential gap seal
UNITED TECHNOLOGIES CORP0 citations51
US10648481B2May 12, 2020
Fiber reinforced spacer for a gas turbine engine
UNITED TECHNOLOGIES CORP0 citations49
US10029336B2Jul 24, 2018
Rotor with blades secured by woven fiber attachment system
UNITED TECHNOLOGIES CORP0 citations49
US10330009B2Jun 25, 2019
Lock for threaded in place nosecone or spinner
UNITED TECHNOLOGIES CORP0 citations42
US10794217B2Oct 6, 2020
Bleed valve system
UNITED TECHNOLOGIES CORP0 citations40
US10808613B2Oct 20, 2020
Assembly for releasable locking of a spinner or nosecone to an engine structure
UNITED TECHNOLOGIES CORP0 citations38
US10480533B2Nov 19, 2019
Fluid injector for cooling a gas turbine engine component
UNITED TECHNOLOGIES CORP0 citations38
RAYTHEON TECH CORP
13 patentsUS11339720B2May 24, 2022
Acoustic liner with non-uniform volumetric distribution
RAYTHEON TECH CORP8 citations81
US11555420B1Jan 17, 2023
Frame connection between fan case and core housing in a gas turbine engine
RAYTHEON TECH CORP2 citations73
US11988283B2May 21, 2024
Non-metallic engine case inlet compression seal for a gas turbine engine
RAYTHEON TECH CORP0 citations62
US11927106B2Mar 12, 2024
Frame connection between fan case and core housing in a gas turbine engine
RAYTHEON TECH CORP0 citations62
US11887571B2Jan 30, 2024
Acoustic attenuation structures
RAYTHEON TECH CORP0 citations62
US11608796B1Mar 21, 2023
Radial strut frame connection between fan case and core housing in a gas turbine engine
RAYTHEON TECH CORP0 citations62
US11286856B2Mar 29, 2022
Diversion of fan air to provide cooling air for gas turbine engine
RAYTHEON TECH CORP0 citations62
US11268388B2Mar 8, 2022
Composite reinforced rotor
RAYTHEON TECH CORP0 citations60
US11566564B2Jan 31, 2023
Acoustically treated panels
RAYTHEON TECH CORP1 citations53
US11708772B2Jul 25, 2023
Triangular-frame connection between fan case and core housing in a gas turbine engine
RAYTHEON TECH CORP0 citations52
US11686220B2Jun 27, 2023
H-frame connection between fan case and core housing in a gas turbine engine
RAYTHEON TECH CORP0 citations52
US11572800B2Feb 7, 2023
Borescope port engine fluid wash
RAYTHEON TECH CORP0 citations52
US11512608B2Nov 29, 2022
Passive transpirational flow acoustically lined guide vane
RAYTHEON TECH CORP0 citations52
RTX CORP
8 patentsUS12188409B2Jan 7, 2025
Gas turbine engine with acoustic liner
RTX CORP1 citations64
US12503988B2Dec 23, 2025
Radial strut frame connection between fan case and core housing in a gas turbine engine
RTX CORP0 citations62
US12308007B2May 20, 2025
Acoustic attenuation structures
RTX CORP0 citations62
US12281702B2Apr 22, 2025
Non-metallic engine case inlet compression seal for a gas turbine engine
RTX CORP0 citations62
US12158107B2Dec 3, 2024
Core compartment vent during engine shutdown to reduced bowed rotor start
RTX CORP0 citations62
US12540563B2Feb 3, 2026
Bowed rotor start reduction via internal cooling
RTX CORP0 citations52
US12326114B2Jun 10, 2025
Gas turbine engine with core debris protection
RTX CORP0 citations52
US11834997B2Dec 5, 2023
Face sheet of acoustic liner having streamlined holes with elongated edges
RTX CORP0 citations49