Patrick Daniel Noble

Person

Greeville, SC, US

People

Patents Grantslast 30 patents

Information Patent Grant
System having blade segment with curved mounting geometry
- Patent number 10,633,985
- Issue date Apr 28, 2020
- General Electric Company
- Andrés Jose Garcia-Crespo
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Airfoil shape for first stage compressor rotor blade
- Patent number 10,287,886
- Issue date May 14, 2019
- General Electric Company
- Paul Griffin Delvernois
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Gas turbine engine rotor assembly and method of assembling the same
- Patent number 9,896,946
- Issue date Feb 20, 2018
- General Electric Company
- Patrick Daniel Noble
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Flowpath boundary and rotor assemblies in gas turbines
- Patent number 9,664,058
- Issue date May 30, 2017
- General Electric Company
- Michael James Healy
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbomachine blade with improved stiffness to weight ratio
- Patent number 9,249,667
- Issue date Feb 2, 2016
- General Electric Company
- Patrick Daniel Noble
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Coupled blade platforms and methods of sealing
- Patent number 8,888,459
- Issue date Nov 18, 2014
- General Electric Company
- Patrick Daniel Noble
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
AIRFOIL SHAPE FOR FIRST STAGE COMPRESSOR ROTOR BLADE
- Publication number 20180080328
- Publication date Mar 22, 2018
- GENERAL ELECTRIC COMPANY
- Paul Griffin DeIvernois
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
FLOWPATH BOUNDARY AND ROTOR ASSEMBLIES IN GAS TURBINES
- Publication number 20160186591
- Publication date Jun 30, 2016
- General Electric Company
- Michael James Healy
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
GAS TURBINE ENGINE ROTOR ASSEMBLY AND METHOD OF ASSEMBLING THE SAME
- Publication number 20150118055
- Publication date Apr 30, 2015
- GENERAL ELECTRIC COMPANY
- Patrick Daniel Noble
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Application
SYSTEM HAVING BLADE SEGMENT WITH CURVED MOUNTING GEOMETRY
- Publication number 20130343895
- Publication date Dec 26, 2013
- GENERAL ELECTRIC COMPANY
- Andrés Jose Garcia-Crespo
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBOMACHINE BLADE WITH IMPROVED STIFFNESS TO WEIGHT RATIO
- Publication number 20130243600
- Publication date Sep 19, 2013
- GENERAL ELECTRIC COMPANY
- Patrick Daniel Noble
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
COUPLED BLADE PLATFORMS AND METHODS OF SEALING
- Publication number 20130052020
- Publication date Feb 28, 2013
- GENERAL ELECTRIC COMPANY
- Patrick Daniel Noble
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patrick Daniel Noble

Person

Patents Grantslast 30 patents

System having blade segment with curved mounting geometry

Airfoil shape for first stage compressor rotor blade

Gas turbine engine rotor assembly and method of assembling the same

Flowpath boundary and rotor assemblies in gas turbines

Turbomachine blade with improved stiffness to weight ratio

Coupled blade platforms and methods of sealing

Patents Applicationslast 30 patents

AIRFOIL SHAPE FOR FIRST STAGE COMPRESSOR ROTOR BLADE

FLOWPATH BOUNDARY AND ROTOR ASSEMBLIES IN GAS TURBINES

GAS TURBINE ENGINE ROTOR ASSEMBLY AND METHOD OF ASSEMBLING THE SAME

SYSTEM HAVING BLADE SEGMENT WITH CURVED MOUNTING GEOMETRY

TURBOMACHINE BLADE WITH IMPROVED STIFFNESS TO WEIGHT RATIO

COUPLED BLADE PLATFORMS AND METHODS OF SEALING