Inventor

Gary D. Roberge

Inventor
Tolland, CT, US

Overview

94→
Patents
1987–2021
Patent span
Mechanical engineering
Primary field (CPC F)

Patents· 94 as inventor

Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.

F05Dprimary
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants16%
F02CGas-turbine plants14%
F01DNon-positive displacement machines or engines, e.g. steam turbines13%
F02KJet-propulsion plants11%
Y02TClimate change mitigation technologies related to transportation9%
F04DNon-positive-displacement pumps3%
B22FWorking metallic powder3%
C23CCoating metallic material3%
B32BLayered products, i.e. products built-up of strata of flat or non-flat, e.g. cellular or honeycomb, form2%
B23KSoldering or unsoldering2%
PatentTitleYear
11,078,843Thermal management of a gas turbine engine shaft202111,047,307Hybrid expander cycle with intercooling and turbo-generator202111,040,780Inertial energy storage device202111,040,372Light weight component with internal reinforcement202111,041,439Hybrid expander cycle with turbo-generator and cooled power electronics202111,028,697Low speed fan for gas turbine engines202111,002,187Low rotor boost compressor for engine cooling circuit202111,002,615Thermochromatic test device for gas turbine engine202110,989,117Hybrid expander cycle with pre-compression cooling and turbo-generator202110,982,597Isolation seals for gas turbine engines202110,968,760Gas turbine engine component for acoustic attenuation202110,961,865Gas turbine engine structure with integrated actuation features202110,927,707Diffuser case heat shields202110,920,671Thrust balance control with differential power extraction202110,907,256Reinforcement of a deposited structure forming a metal matrix composite202110,883,380Airfoil deicing system202110,837,294Multi-material turbine airfoil202010,837,403Exhaust nozzle control including tapered control effector for a gas turbine engine202010,837,364Thermal shield for gas turbine engine diffuser case202010,823,081Concentric power takeoff transmission202010,822,999Systems and methods for fan blade de-icing202010,815,885Anti-ice systems for engine airfoils202010,814,445Airfoil machining202010,815,823Anti-windmilling system for a gas turbine engine202010,801,413Electromagnetic anti-windmilling system202010,801,410Thermal management of tail cone mounted generator202010,781,772Integrated heat exchangers for low fan pressure ratio geared turbofan202010,746,181Variable speed boost compressor for gas turbine engine cooling air supply202010,724,543Bridge bracket for variable-pitch vane system202010,724,131Light weight component and method of making202010,648,084Material deposition to form a sheet structure202010,619,949Light weight housing for internal component with integrated thermal management features and method of making202010,612,414Panel based heat exchanger202010,612,462Turbomachinery with high relative velocity202010,598,378Bonded combustor wall for a turbine engine202010,563,537Energy absorbing beam and sandwich panel structure202010,563,310Multi-wall deposited thin sheet structure202010,563,577Low rotor boost compressor for engine cooling circuit202010,550,764Architecture for an axially compact, high performance propulsion system202010,526,913Anti-windmilling system for a gas turbine engine202010,519,552Deposited material structure with integrated component201910,513,939Seal interface with a deflection control feature201910,458,255Removable film for airfoil surfaces201910,399,117Method of making light weight component with internal metallic foam and polymer reinforcement201910,400,709Auxiliary device for three air flow path gas turbine engine201910,378,478Flow path routing within a gas turbine engine201910,363,634Deposited structure with integral cooling enhancement features201910,335,850Light weight housing for internal component and method of making201910,337,349Anti-windmilling system for a gas turbine engine201910,323,325Light weight housing for internal component and method of making201910,302,017Light weight component with acoustic attenuation and method of making201910,294,870Distributed engine accessory drive201910,287,976Split gear system for a gas turbine engine201910,252,292Method of making light weight component with internal metallic foam and polymer reinforcement201910,221,701Multi-material turbine airfoil201910,221,771Fan drive gear system201910,197,008Gas turbine engine including a third flowpath exhaust nozzle201910,145,245Bonded multi-piece gas turbine engine component201810,145,302Gas turbine engine lubrication system201810,125,724Start system for gas turbine engines201810,119,412Turbine engine adaptive low leakage air seal201810,119,475Gas turbine engine geared architecture201810,107,157Gas turbine engine lubrication system201810,024,610Light weight housing for internal component with integrated thermal management features and method of making20189,982,628Exhaust system having a flow path liner supported by structural duct segments20189,964,069Exhaust nozzle control for a gas turbine engine20189,945,325Integrated heat exchangers for low fan pressure ratio geared turbofan20189,932,902Turbine section support for a gas turbine engine20189,915,164'Geared turbofan with high speed generator'20189,909,494'Tip turbine engine with aspirated compressor'20189,909,529'Flow path routing within a gas turbine engine'20189,291,123'Gas turbine engine exhaust duct'20169,003,759'Particle separator for tip turbine engine'20158,943,792'Gas-driven propulsor with tip turbine fan'20158,726,633'Gas turbine engine systems and related methods involving multiple gas turbine cores'20148,590,286'Gas turbine engine systems involving tip fans'20138,402,742'Gas turbine engine systems involving tip fans'20138,336,289'Gas turbine engine systems and related methods involving multiple gas turbine cores'20128,241,003'Systems and methods involving localized stiffening of blades'20128,176,725'Reversed-flow core for a turbofan with a fan drive gear system'20128,127,528'Auxiliary propulsor for a variable cycle gas turbine engine'20128,104,257'Tip turbine engine with multiple fan and turbine stages'20128,087,885'Stacked annular components for turbine engines'20128,082,727'Rear propulsor for a variable cycle gas turbine engine'20118,033,094'Cantilevered tip turbine engine'20117,980,054'Ejector cooling of outer case for tip turbine engine'20117,882,695'Turbine blow down starter for turbine engine'20117,854,112'Vectoring transition duct for turbine engine'20107,845,157'Axial compressor for tip turbine engine'20107,752,835'Pulsed combustion engine'20107,624,942'Decoupled ducting for twin-engine reaction rotor drive'20097,201,558'Seal arrangement for a fan-turbine rotor assembly'20075,209,432'Aircraft reverser port door'19934,667,774'Bevel gear lubrication and cooling'1987

Career & activity timeline

Assembled from patent assignee/location history and declaration credentials.

1987–2021Patents assigned to UNITED TECHNOLOGIES CORP (88)· patent assignee history
1987–1993Based in Jupiter, FL, US· patent location history
2007–2021Based in Tolland, CT, US· patent location history
2011–2018Patents assigned to ROBERGE GARY D (12)· patent assignee history
2012–2013Patents assigned to SUCIU GABRIEL L (3)· patent assignee history
2012–2018Patents assigned to BERRYANN ANDREW P (2)· patent assignee history
2020–2021Patents assigned to RAYTHEON TECH CORP (28)· patent assignee history

Inventor activity

Assignee and location history derived from the patent record.

Assignees
AssigneePatentsSpan
UNITED TECHNOLOGIES CORP881987–2021
RAYTHEON TECH CORP282020–2021
ROBERGE GARY Dself122011–2018
SUCIU GABRIEL L32012–2013
BERRYANN ANDREW P22012–2018
Locations
LocationPatentsSpan
Tolland, CT, US922007–2021
Jupiter, Florida, US21987–1993