Donald Lee Gardner

Person

West Chester, OH, US

People

Patents Grantslast 30 patents

Information Patent Grant
Engine backbone bending reduction
- Patent number 12,214,891
- Issue date Feb 4, 2025
- General Electric Company
- Jonathan E. Coleman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Heat exchanger having curved fluid passages for a gas turbine engine
- Patent number 12,196,502
- Issue date Jan 14, 2025
- General Electric Company
- Ramon Martinez
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Turbo machine combustor assembly having separable portions coupled...
- Patent number 12,173,897
- Issue date Dec 24, 2024
- General Electric Company
- Ryan Christopher Jones
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Heat exchanger having curved fluid passages for a gas turbine engine
- Patent number 11,662,150
- Issue date May 30, 2023
- General Electric Company
- Ramon Martinez
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Grant
Method of operating a combustion system with main and pilot fuel ci...
- Patent number 11,408,356
- Issue date Aug 9, 2022
- General Electric Company
- Steven Clayton Vise
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Flow control wall for heat engine
- Patent number 11,339,966
- Issue date May 24, 2022
- General Electric Company
- Andrew Scott Bilse
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Combustor assembly for a turbo machine
- Patent number 11,280,492
- Issue date Mar 22, 2022
- General Electric Company
- Ryan Christopher Jones
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Combustion system and method of assembling the same
- Patent number 8,893,382
- Issue date Nov 25, 2014
- General Electric Company
- David Bruce Patterson
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Integrated nacelle assembly
- Patent number 8,876,042
- Issue date Nov 4, 2014
- General Electric Company
- Donald George LaChapelle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Method for reducing tip rub loading
- Patent number 8,662,834
- Issue date Mar 4, 2014
- General Electric Company
- Nicholas Joseph Kray
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Rotor blade with reduced rub loading
- Patent number 8,657,570
- Issue date Feb 25, 2014
- General Electric Company
- Nicholas Joseph Kray
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Aircraft gas turbine engine blade tip clearance control
- Patent number 8,126,628
- Issue date Feb 28, 2012
- General Electric Company
- John Erik Hershey
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Rich double dome combustor
- Patent number 6,474,070
- Issue date Nov 5, 2002
- General Electric Company
- Allen M. Danis
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Gas turbine engine case counterflow thermal control
- Patent number 5,205,115
- Issue date Apr 27, 1993
- General Electric Company
- Larry W. Plemmons
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Patents Applicationslast 30 patents

Information Patent Application
COMBUSTOR ASSEMBLY FOR A TURBO MACHINE
- Publication number 20250129939
- Publication date Apr 24, 2025
- GENERAL ELECTRIC COMPANY
- Ryan Christopher Jones
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
ENGINE BACKBONE BENDING REDUCTION
- Publication number 20240150027
- Publication date May 9, 2024
- GENERAL ELECTRIC COMPANY
- Jonathan E. Coleman
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HEAT EXCHANGER HAVING CURVED FLUID PASSAGES FOR A GAS TURBINE ENGINE
- Publication number 20230258407
- Publication date Aug 17, 2023
- GENERAL ELECTRIC COMPANY
- Ramon Martinez
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
COMBUSTOR ASSEMBLY FOR A TURBO MACHINE
- Publication number 20220325889
- Publication date Oct 13, 2022
- GENERAL ELECTRIC COMPANY
- Ryan Christopher Jones
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
FLOW CONTROL WALL FOR HEAT ENGINE
- Publication number 20220268443
- Publication date Aug 25, 2022
- GENERAL ELECTRIC COMPANY
- Andrew Scott Bilse
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
HEAT EXCHANGER HAVING CURVED FLUID PASSAGES FOR A GAS TURBINE ENGINE
- Publication number 20220049904
- Publication date Feb 17, 2022
- GENERAL ELECTRIC COMPANY
- Ramon Martinez
- F28 - HEAT EXCHANGE IN GENERAL
Information Patent Application
ENGINE BACKBONE BENDING REDUCTION
- Publication number 20210300577
- Publication date Sep 30, 2021
- GENERAL ELECTRIC COMPANY
- Jonathan E. Coleman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
Flow Control Wall for Heat Engine
- Publication number 20200063583
- Publication date Feb 27, 2020
- GENERAL ELECTRIC COMPANY
- Andrew Scott Bilse
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Combustor Assembly for a Turbo Machine
- Publication number 20200063961
- Publication date Feb 27, 2020
- GENERAL ELECTRIC COMPANY
- Ryan Christopher Jones
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
METHOD OF OPERATING A COMBUSTION SYSTEM WITH MAIN AND PILOT FUEL CI...
- Publication number 20190101062
- Publication date Apr 4, 2019
- GENERAL ELECTRIC COMPANY
- Steven Clayton Vise
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME
- Publication number 20130081270
- Publication date Apr 4, 2013
- David Bruce Patterson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Integrated Nacelle Assembly
- Publication number 20110146230
- Publication date Jun 23, 2011
- Donald George LaChapelle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ROTOR BLADE WITH REDUCED RUB LOADING
- Publication number 20100329875
- Publication date Dec 30, 2010
- Nicholas Joseph Kray
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
METHOD FOR REDUCING TIP RUB LOADING
- Publication number 20100329863
- Publication date Dec 30, 2010
- Nicholas Joseph Kray
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT GAS TURBINE ENGINE BLADE TIP CLEARANCE CONTROL
- Publication number 20090037035
- Publication date Feb 5, 2009
- John Erik Hershey
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES

Donald Lee Gardner

Person

Patents Grantslast 30 patents

Engine backbone bending reduction

Heat exchanger having curved fluid passages for a gas turbine engine

Turbo machine combustor assembly having separable portions coupled...

Heat exchanger having curved fluid passages for a gas turbine engine

Method of operating a combustion system with main and pilot fuel ci...

Flow control wall for heat engine

Combustor assembly for a turbo machine

Combustion system and method of assembling the same

Integrated nacelle assembly

Method for reducing tip rub loading

Rotor blade with reduced rub loading

Aircraft gas turbine engine blade tip clearance control

Rich double dome combustor

Gas turbine engine case counterflow thermal control

Patents Applicationslast 30 patents

COMBUSTOR ASSEMBLY FOR A TURBO MACHINE

ENGINE BACKBONE BENDING REDUCTION

HEAT EXCHANGER HAVING CURVED FLUID PASSAGES FOR A GAS TURBINE ENGINE

COMBUSTOR ASSEMBLY FOR A TURBO MACHINE

FLOW CONTROL WALL FOR HEAT ENGINE

HEAT EXCHANGER HAVING CURVED FLUID PASSAGES FOR A GAS TURBINE ENGINE

ENGINE BACKBONE BENDING REDUCTION

Flow Control Wall for Heat Engine

Combustor Assembly for a Turbo Machine

METHOD OF OPERATING A COMBUSTION SYSTEM WITH MAIN AND PILOT FUEL CI...

COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME

Integrated Nacelle Assembly

ROTOR BLADE WITH REDUCED RUB LOADING

METHOD FOR REDUCING TIP RUB LOADING

AIRCRAFT GAS TURBINE ENGINE BLADE TIP CLEARANCE CONTROL