Keith Edward James BLODGETT

Person

Milford, OH, US

People

Patents Grantslast 30 patents

Information Patent Grant
Aircraft with a fuselage accommodating an unducted turbine engine
- Patent number 12,030,652
- Issue date Jul 9, 2024
- General Electric Company
- Keith Edward James Blodgett
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Cascade thrust reverser assembly for a gas turbine engine
- Patent number 11,840,987
- Issue date Dec 12, 2023
- General Electric Company
- Trevor Howard Wood
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Methods and apparatus to control air flow separation of an engine
- Patent number 11,828,237
- Issue date Nov 28, 2023
- General Electric Company
- Sai Venkata Kathik Saripella
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Methods and apparatus to detect air flow separation of an engine
- Patent number 11,674,451
- Issue date Jun 13, 2023
- General Electric Company
- Sai Venkata Karthik Saripella
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Methods and apparatus to detect air flow separation of an engine
- Patent number 11,333,079
- Issue date May 17, 2022
- General Electric Company
- Sai Venkata Kathik Saripella
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Aircraft having an engine wing assembly
- Patent number 11,267,577
- Issue date Mar 8, 2022
- General Electric Company
- Bhaskar Nanda Mondal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Hybrid electric propulsion system for an aircraft
- Patent number 10,822,100
- Issue date Nov 3, 2020
- General Electric Company
- Mustafa Dindar
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Grant
Turbine engine thrust reverser stop
- Patent number 10,578,055
- Issue date Mar 3, 2020
- MRA Systems, LLC
- David Patrick Calder
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
System and method of operating a ducted fan propulsion system durin...
- Patent number 10,343,786
- Issue date Jul 9, 2019
- General Electric Company
- Brian Francis Nestico
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
System and method of operating a ducted fan propulsion system inflight
- Patent number 10,119,495
- Issue date Nov 6, 2018
- General Electric Company
- Brian Francis Nestico
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Exhaust nozzle with non-coplanar and/or non-axisymmetric shape
- Patent number 9,810,178
- Issue date Nov 7, 2017
- General Electric Company
- Mustafa Dindar
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Variable slope exhaust nozzle
- Patent number 9,181,899
- Issue date Nov 10, 2015
- General Electric Company
- Mustafa Dindar
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
APPARATUS TO PREVENT AIR LEAKAGE IN TURBINE ENGINES
- Publication number 20240328324
- Publication date Oct 3, 2024
- GENERAL ELECTRIC COMPANY
- Ning Fang
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE
- Publication number 20240317412
- Publication date Sep 26, 2024
- GENERAL ELECTRIC COMPANY
- Keith Edward James Blodgett
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
GAS TURBINE ENGINE
- Publication number 20240060430
- Publication date Feb 22, 2024
- GENERAL ELECTRIC COMPANY
- William Joseph Bowden
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE
- Publication number 20230399114
- Publication date Dec 14, 2023
- GENERAL ELECTRIC COMPANY
- Keith Edward James Blodgett
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
CASCADE THRUST REVERSER ASSEMBLY FOR A GAS TURBINE ENGINE
- Publication number 20230313754
- Publication date Oct 5, 2023
- GENERAL ELECTRIC COMPANY
- Trevor Howard Wood
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
UNDUCTED THRUST PRODUCING SYSTEM
- Publication number 20230021836
- Publication date Jan 26, 2023
- GENERAL ELECTRIC COMPANY
- David Baker Riddle
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE
- Publication number 20220412271
- Publication date Dec 29, 2022
- GENERAL ELECTRIC COMPANY
- Sai Venkata Karthik Saripella
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE
- Publication number 20210332763
- Publication date Oct 28, 2021
- GENERAL ELECTRIC COMPANY
- Sai Venkata Kathik Saripella
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHODS AND APPARATUS TO CONTROL AIR FLOW SEPARATION OF AN ENGINE
- Publication number 20210332764
- Publication date Oct 28, 2021
- GENERAL ELECTRIC COMPANY
- Sai Venkata Kathik Saripella
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
AIRCRAFT HAVING AN ENGINE WING ASSEMBLY
- Publication number 20210171211
- Publication date Jun 10, 2021
- GENERAL ELECTRIC COMPANY
- Bhaskar Nanda Mondal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
TURBINE ENGINE THRUST REVERSER STOP
- Publication number 20190048824
- Publication date Feb 14, 2019
- MRA Systems, LLC
- David Patrick Calder
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SYSTEM AND METHOD OF OPERATING A DUCTED FAN PROPULSION SYSTEM DURIN...
- Publication number 20190002118
- Publication date Jan 3, 2019
- GENERAL ELECTRIC COMPANY
- Brian Francis Nestico
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
HYBRID ELECTRIC PROPULSION SYSTEM FOR AN AIRCRAFT
- Publication number 20180370641
- Publication date Dec 27, 2018
- GENERAL ELECTRIC COMPANY
- Mustafa Dindar
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
EXHAUST NOZZLE WITH NON-COPLANAR AND/OR NON-AXISYMMETRIC SHAPE
- Publication number 20170037813
- Publication date Feb 9, 2017
- GENERAL ELECTRIC COMPANY
- Mustafa DINDAR
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Keith Edward James BLODGETT

Person

Patents Grantslast 30 patents

Aircraft with a fuselage accommodating an unducted turbine engine

Cascade thrust reverser assembly for a gas turbine engine

Methods and apparatus to control air flow separation of an engine

Methods and apparatus to detect air flow separation of an engine

Methods and apparatus to detect air flow separation of an engine

Aircraft having an engine wing assembly

Hybrid electric propulsion system for an aircraft

Turbine engine thrust reverser stop

System and method of operating a ducted fan propulsion system durin...

System and method of operating a ducted fan propulsion system inflight

Exhaust nozzle with non-coplanar and/or non-axisymmetric shape

Variable slope exhaust nozzle

Patents Applicationslast 30 patents

APPARATUS TO PREVENT AIR LEAKAGE IN TURBINE ENGINES

AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE

GAS TURBINE ENGINE

AIRCRAFT WITH A FUSELAGE ACCOMMODATING AN UNDUCTED TURBINE ENGINE

CASCADE THRUST REVERSER ASSEMBLY FOR A GAS TURBINE ENGINE

UNDUCTED THRUST PRODUCING SYSTEM

METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE

METHODS AND APPARATUS TO DETECT AIR FLOW SEPARATION OF AN ENGINE

METHODS AND APPARATUS TO CONTROL AIR FLOW SEPARATION OF AN ENGINE

AIRCRAFT HAVING AN ENGINE WING ASSEMBLY

TURBINE ENGINE THRUST REVERSER STOP

SYSTEM AND METHOD OF OPERATING A DUCTED FAN PROPULSION SYSTEM DURIN...

HYBRID ELECTRIC PROPULSION SYSTEM FOR AN AIRCRAFT

EXHAUST NOZZLE WITH NON-COPLANAR AND/OR NON-AXISYMMETRIC SHAPE