P

Inventor

BINEK LAWRENCE A

US89 patents
⚠️ This page may combine multiple inventors who share the name “BINEK LAWRENCE A”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

RAYTHEON TECH CORP

25 patents
US11649964B2May 16, 2023

Fuel injector assembly for a turbine engine

RAYTHEON TECH CORP5 citations86
US11377977B2Jul 5, 2022

Lubrication network for an attritable engine

RAYTHEON TECH CORP5 citations81
US12013120B1Jun 18, 2024

Turbine engine support structure with airflow ports

RAYTHEON TECH CORP3 citations75
US11846421B2Dec 19, 2023

Integrated fuel swirlers

RAYTHEON TECH CORP4 citations75
US12116934B2Oct 15, 2024

Turbine engine fuel injector with oxygen circuit

RAYTHEON TECH CORP3 citations74
US11753994B2Sep 12, 2023

Fuel feed passages for an attritable engine

RAYTHEON TECH CORP4 citations74
US12044409B2Jul 23, 2024

Casing integrated fluid distribution system

RAYTHEON TECH CORP2 citations73
US11754287B2Sep 12, 2023

Fuel injector assembly for a turbine engine

RAYTHEON TECH CORP3 citations73
US11525359B1Dec 13, 2022

Heat pipe for a turbine engine

RAYTHEON TECH CORP2 citations73
US11421883B2Aug 23, 2022

Fuel injector assembly with a helical swirler passage for a turbine engine

RAYTHEON TECH CORP3 citations73
US11614002B2Mar 28, 2023

Split case structure for a gas turbine engine

RAYTHEON TECH CORP3 citations68
US12270543B2Apr 8, 2025

Multi-function monolithic combustion liner

RAYTHEON TECH CORP1 citations64
US12264624B2Apr 1, 2025

Build plate integrated into additive manufactured component

RAYTHEON TECH CORP0 citations62
US12253003B1Mar 18, 2025

Integral stator vane weld shield

RAYTHEON TECH CORP0 citations62
US12234986B2Feb 25, 2025

Article and method for manufacturing an expanded combustor liner

RAYTHEON TECH CORP0 citations62
US12203386B2Jan 21, 2025

Compressor-turbine rotating assembly with integral cooling circuit(s)

RAYTHEON TECH CORP0 citations62
US12179436B2Dec 31, 2024

Systems and methods for support material removal

RAYTHEON TECH CORP0 citations62
US12055062B2Aug 6, 2024

Gas turbine engine support structure with internal lattice

RAYTHEON TECH CORP0 citations62
US11936091B2Mar 19, 2024

Waveguide apparatus including channel segments having surfaces that are angularly joined at a junction or a corner

RAYTHEON TECH CORP0 citations62
US11846249B1Dec 19, 2023

Gas turbine engine with integral bypass duct

RAYTHEON TECH CORP1 citations62
US11808455B2Nov 7, 2023

Gas turbine engine combustor with integral fuel conduit(s)

RAYTHEON TECH CORP1 citations62
US11739690B2Aug 29, 2023

Attritable engine additively manufactured inlet cap

RAYTHEON TECH CORP0 citations62
US11732656B2Aug 22, 2023

Turbine engine with soaring air conduit

RAYTHEON TECH CORP0 citations62
US11732610B2Aug 22, 2023

Sectioned engine structure for a gas turbine engine

RAYTHEON TECH CORP1 citations62
US11713695B2Aug 1, 2023

Unitized manufacturing of a gas turbine engine

RAYTHEON TECH CORP0 citations62

RTX CORP

17 patents
US12313001B2May 27, 2025

Support structure for bearing compartment

RTX CORP2 citations71
US12422142B2Sep 23, 2025

Fuel injector assembly for a turbine engine

RTX CORP0 citations63
US12595909B2Apr 7, 2026

Article and method for manufacturing an expanded combustor liner

RTX CORP0 citations62
US12571330B2Mar 10, 2026

Oil nozzle for bearing chamber

RTX CORP0 citations62
US12516610B2Jan 6, 2026

Oil passage built into bearing compartment spring

RTX CORP0 citations62
US12480658B2Nov 25, 2025

Cooling fuel injector system for an attritable engine

RTX CORP0 citations62
US12473842B2Nov 18, 2025

Annular oil distributor for bearing chamber

RTX CORP0 citations62
US12460559B2Nov 4, 2025

Support structure and spring for bearing compartment

RTX CORP0 citations62
US12421872B2Sep 23, 2025

Spring damping for bearing compartment

RTX CORP0 citations62
US12398662B2Aug 26, 2025

Gas turbine engine support structure with internal lattice

RTX CORP0 citations62
US12392489B2Aug 19, 2025

Turbine engine support structure with airflow ports

RTX CORP0 citations62
US12385407B1Aug 12, 2025

Additively manufactured turbine vane cluster

RTX CORP0 citations62
US12292016B2May 6, 2025

Axial expandable exhaust duct

RTX CORP0 citations62
US12215604B1Feb 4, 2025

Cooling nozzle vanes of a turbine engine

RTX CORP0 citations62
US12129768B2Oct 29, 2024

Unitized manufacturing of a gas turbine engine

RTX CORP0 citations62
US12078077B2Sep 3, 2024

Sectioned engine structure for a gas turbine engine

RTX CORP0 citations62
US12000360B2Jun 4, 2024

Axial expandable exhaust duct

RTX CORP0 citations62

UNITED TECHNOLOGIES CORP

7 patents

HAMILTON SUNDSTRAND CORP

1 patent

Showing the top 50 of 89 patents by PatentIndex Score.