Thomas G. Cloft

Person

Glastonbury, CT, US

People

Patents Grantslast 30 patents

Information Patent Grant
Gas turbine engine accessory gearbox
- Patent number 10,641,181
- Issue date May 5, 2020
- United Technologies Corporation
- Thomas G. Cloft
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Geared gas turbine engine accessory gearbox
- Patent number 10,184,404
- Issue date Jan 22, 2019
- United Technologies Corporation
- Thomas G. Cloft
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Nacelle inner flow structure leading edge latching system
- Patent number 10,054,006
- Issue date Aug 21, 2018
- United Technologies Corporation
- Claude Mercier
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nacelle assembly having integrated afterbody mount case
- Patent number 9,828,105
- Issue date Nov 28, 2017
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Gas turbine engine with accessory gear box
- Patent number 9,297,314
- Issue date Mar 29, 2016
- United Technologies Corporation
- Thomas G. Cloft
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Nacelle electrical locking system for leading edge of openable panel
- Patent number 9,239,030
- Issue date Jan 19, 2016
- United Technologies Corporation
- Claude Mercier
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Access door for gas turbine engine components
- Patent number 9,126,691
- Issue date Sep 8, 2015
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Nacelle inner flow structure leading edge latching system
- Patent number 9,108,736
- Issue date Aug 18, 2015
- United Technologies Corporation
- Claude Mercier
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Reduced gearbox size by separate electrically powered engine oil sy...
- Patent number 9,091,214
- Issue date Jul 28, 2015
- United Technologies Corporation
- Thomas G. Cloft
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Pylon and engine mount configuration
- Patent number 8,950,702
- Issue date Feb 10, 2015
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Translatable cascade thrust reverser
- Patent number 8,869,507
- Issue date Oct 28, 2014
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine assembly including accessory components within t...
- Patent number 8,769,924
- Issue date Jul 8, 2014
- United Technologies Corporation
- Thomas G. Cloft
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Nacelle compartment plenum for bleed air flow delivery system
- Patent number 8,657,567
- Issue date Feb 25, 2014
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Integral suction device with acoustic panel
- Patent number 8,459,597
- Issue date Jun 11, 2013
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Generator with separate oil system for improved nacelle performance
- Patent number 8,312,728
- Issue date Nov 20, 2012
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Systems and methods involving multiplexed engine control signals
- Patent number 8,140,242
- Issue date Mar 20, 2012
- United Technologies Corp.
- Thomas G. Cloft
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Integrated inlet fan case
- Patent number 8,092,169
- Issue date Jan 10, 2012
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Tangential anti-swirl air supply
- Patent number 8,082,726
- Issue date Dec 27, 2011
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Integral suction device with acoustic panel
- Patent number 7,766,280
- Issue date Aug 3, 2010
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flow distribution system for inlet flow control
- Patent number 7,708,230
- Issue date May 4, 2010
- United Technologies Corporation
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
Gas Turbine Engine With Accessory Gear Box
- Publication number 20160186598
- Publication date Jun 30, 2016
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GAS TURBINE ENGINE ACCESSORY GEARBOX
- Publication number 20160010561
- Publication date Jan 14, 2016
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE INNER FLOW STRUCTURE LEADING EDGE LATCHING SYSTEM
- Publication number 20150274307
- Publication date Oct 1, 2015
- United Technologies Corporation
- Claude Mercier
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GEARED GAS TURBINE ENGINE ACCESSORY GEARBOX
- Publication number 20150233300
- Publication date Aug 20, 2015
- United Technologies Corporation
- Thomas G. Cloft
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
Gas Turbine Engine With Accessory Gear Box
- Publication number 20140165589
- Publication date Jun 19, 2014
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
GEARED TURBOFAN WITH FAN AND CORE MOUNTED ACCESSORY GEARBOXES
- Publication number 20140090386
- Publication date Apr 3, 2014
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE LEADING EDGE ELECTRICAL LATCHING SYSTEM
- Publication number 20140075918
- Publication date Mar 20, 2014
- United Technologies Corporation
- Claude Mercier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE INNER FLOW STRUCTURE LEADING EDGE LATCHING SYSTEM
- Publication number 20130323013
- Publication date Dec 5, 2013
- Claude Mercier
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
NACELLE ASSEMBLY HAVING INTEGRATED AFTERBODY MOUNT CASE
- Publication number 20130052005
- Publication date Feb 28, 2013
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TRANSLATABLE CASCADE THRUST REVERSER
- Publication number 20110167790
- Publication date Jul 14, 2011
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
INTEGRAL SUCTION DEVICE WITH ACOUSTIC PANEL
- Publication number 20100205975
- Publication date Aug 19, 2010
- Thomas G. Cloft
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
INTEGRATED INLET FAN CASE
- Publication number 20100068051
- Publication date Mar 18, 2010
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE ENGINE ASSEMBLY
- Publication number 20090293497
- Publication date Dec 3, 2009
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Systems and Methods Involving Multiplexed Engine Control Signals
- Publication number 20090292437
- Publication date Nov 26, 2009
- United Technologies Corp.
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
PYLON AND ENGINE MOUNT CONFIGURATION
- Publication number 20090184197
- Publication date Jul 23, 2009
- Thomas G. Cloft
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Application
ACCESS DOOR FOR GAS TURBINE ENGINE COMPONENTS
- Publication number 20090129922
- Publication date May 21, 2009
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Systems Involving Inlet-Mounted Engine Controls
- Publication number 20090064684
- Publication date Mar 12, 2009
- UNITED TECHNOLOGIES CORP.
- Thomas G. Cloft
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TANGENTIAL ANTI-SWIRL AIR SUPPLY
- Publication number 20090000272
- Publication date Jan 1, 2009
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Generator with separate oil system for improved nacelle performance
- Publication number 20090000308
- Publication date Jan 1, 2009
- United Technologies Corporation
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Reduced gearbox size by separate electrically powered engine oil sy...
- Publication number 20090003992
- Publication date Jan 1, 2009
- United Technologies Corporation
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
NACELLE COMPARTMENT PLENUM FOR BLEED AIR FLOW DELIVERY SYSTEM
- Publication number 20080298950
- Publication date Dec 4, 2008
- Thomas G. Cloft
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
FLOW DISTRIBUTION SYSTEM FOR INLET FLOW CONTROL
- Publication number 20080296440
- Publication date Dec 4, 2008
- Thomas G. Cloft
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INTEGRAL SUCTION DEVICE WITH ACOUSTIC PANEL
- Publication number 20080296439
- Publication date Dec 4, 2008
- Thomas G. Cloft
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Thomas G. Cloft

Person

Patents Grantslast 30 patents

Gas turbine engine accessory gearbox

Geared gas turbine engine accessory gearbox

Nacelle inner flow structure leading edge latching system

Nacelle assembly having integrated afterbody mount case

Gas turbine engine with accessory gear box

Nacelle electrical locking system for leading edge of openable panel

Access door for gas turbine engine components

Nacelle inner flow structure leading edge latching system

Reduced gearbox size by separate electrically powered engine oil sy...

Pylon and engine mount configuration

Translatable cascade thrust reverser

Gas turbine engine assembly including accessory components within t...

Nacelle compartment plenum for bleed air flow delivery system

Integral suction device with acoustic panel

Generator with separate oil system for improved nacelle performance

Systems and methods involving multiplexed engine control signals

Integrated inlet fan case

Tangential anti-swirl air supply

Integral suction device with acoustic panel

Flow distribution system for inlet flow control

Patents Applicationslast 30 patents

Gas Turbine Engine With Accessory Gear Box

GAS TURBINE ENGINE ACCESSORY GEARBOX

NACELLE INNER FLOW STRUCTURE LEADING EDGE LATCHING SYSTEM

GEARED GAS TURBINE ENGINE ACCESSORY GEARBOX

Gas Turbine Engine With Accessory Gear Box

GEARED TURBOFAN WITH FAN AND CORE MOUNTED ACCESSORY GEARBOXES

NACELLE LEADING EDGE ELECTRICAL LATCHING SYSTEM

NACELLE INNER FLOW STRUCTURE LEADING EDGE LATCHING SYSTEM

NACELLE ASSEMBLY HAVING INTEGRATED AFTERBODY MOUNT CASE

TRANSLATABLE CASCADE THRUST REVERSER

INTEGRAL SUCTION DEVICE WITH ACOUSTIC PANEL

INTEGRATED INLET FAN CASE

GAS TURBINE ENGINE ASSEMBLY

Systems and Methods Involving Multiplexed Engine Control Signals

PYLON AND ENGINE MOUNT CONFIGURATION

ACCESS DOOR FOR GAS TURBINE ENGINE COMPONENTS

Systems Involving Inlet-Mounted Engine Controls

TANGENTIAL ANTI-SWIRL AIR SUPPLY

Generator with separate oil system for improved nacelle performance

Reduced gearbox size by separate electrically powered engine oil sy...

NACELLE COMPARTMENT PLENUM FOR BLEED AIR FLOW DELIVERY SYSTEM

FLOW DISTRIBUTION SYSTEM FOR INLET FLOW CONTROL

INTEGRAL SUCTION DEVICE WITH ACOUSTIC PANEL