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Inventor profile of:

Gary Collopy

City:

Vernon, Connecticut

Country:

United States

Published Applications:

Last publication date:

2026-06-02

Top Assignees for applications by Gary Collopy

The entities that hold a legal rights for patent applications filed by inventor Collopy Gary:

Raytheon Technologies Corporation 10 Farmington, CT United States
RTX Corporation 10 Farmington, CT United States
UNITED TECHNOLOGIES CORPORATION 3 Farmington, CT United States
UNITED TECHNOLOGIES CORPORATION 1 Hartford, CT United States

Recent patent applications by Collopy Gary

Gary Collopy from Vernon, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-06-02

US19337346

Mechanical engineering

Spool-to-spool powertrain assembly for an aircraft propulsion system

#2 | 2026-05-28

US20260146564A1

Mechanical engineering

INTEGRATED ELECTRO-AERO-THERMAL TURBINE ENGINE

#3 | 2025-07-17

US20250230756A1

Mechanical engineering

INTEGRATED ELECTRO-AERO-THERMAL TURBINE ENGINE

#4 | 2025-06-19

US20250197019A1

Performing operations; transporting

HYBRID AIRCRAFT ENGINE WITH COMPRESSOR CONTROL FOR ELECTRIC MOTOR FAILURE

#5 | 2025-01-23

US20250027425A1

Mechanical engineering

TURBINE ENGINE TIP CLEARANCE CONTROL UTILIZING ELECTRIC MACHINE

#6 | 2025-01-23

US20250027424A1

Mechanical engineering

Turbine engine tip clearance control utilizing electric machine

#7 | 2025-01-23

US20250026333A1

Performing operations; transporting

Hybrid Electric Power Dependent Active Clearance Control

#8 | 2024-09-12

US20240301834A1

Mechanical engineering

SURGE RECOVERY SYSTEM AND METHODS

#9 | 2024-07-18

US20240240569A1

Mechanical engineering

Gas turbine engine with idle thrust ratio

#10 | 2023-07-13

US20230220784A1

Mechanical engineering

Integrated electro-aero-thermal turbine engine

#11 | 2023-05-25

US20230160358A1

Mechanical engineering

HYBRID GAS TURBINE ENGINE STARTING CONTROL

#12 | 2023-05-04

US20230138476A1

Mechanical engineering

HYBRID ELECTRIC SINGLE ENGINE DESCENT RESTART

#13 | 2023-01-26

US20230028552A1

Mechanical engineering

Gas turbine engine with idle thrust ratio

#14 | 2022-11-03

US20220349354A1

Mechanical engineering

Surge recovery system and methods

#15 | 2022-05-05

US20220136401A1

Mechanical engineering

Integrated electro-aero-thermal turbine engine

#16 | 2022-04-21

US20220120215A1

Mechanical engineering

Gas turbine engine having electric motor for applying power to a spool shaft and method for operating same

#17 | 2021-08-12

US20210246837A1

Mechanical engineering

Surge recovery systems and methods

#18 | 2021-05-13

US20210140372A1

Mechanical engineering

Gas turbine engine having electric motor applying power to the high pressure spool shaft and method for operating same

#19 | 2021-04-22

US20210115857A1

Mechanical engineering

Electric power assist for in-flight engine re-start

#20 | 2021-02-18

US20210050810A1

Electricity

Aircraft engine power-assist start stability control

#21 | 2021-02-18

US20210047970A1

Mechanical engineering

Rotor dynamics accommodation using electrical power assist

#22 | 2021-02-11

US20210040896A1

Mechanical engineering

Gas turbine engine spool coupling

#23 | 2021-01-28

US20210025339A1

Mechanical engineering

Hybrid gas turbine engine starting control

#24 | 2020-12-17

US20200392904A1

Mechanical engineering

Dual drive electro-aero-thermal turbine engine

#25 | 2020-12-17

US20200392861A1

Mechanical engineering

Integrated electro-aero-thermal turbine engine

#26 | 2014-09-04

US20140245749A1

Mechanical engineering

Nacelle anti-ice valve utilized as compressor stability bleed valve during starting

#27 | 2013-09-12

US20130236296A1

Mechanical engineering

Low pressure compressor variable vane control for two-spool turbofan or turboprop engine

InventorID:

432569 ⎘