Paul E. Sabla

Person

Cincinnati, OH, US

People

Patents Grantslast 30 patents

Information Patent Grant
Anti-carboning fuel-air mixer for a gas turbine engine combustor
- Patent number 6,571,559
- Issue date Jun 3, 2003
- General Electric Company
- Douglas M. Fortuna
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Methods and apparatus for cooling gas turbine engine combustors
- Patent number 6,546,732
- Issue date Apr 15, 2003
- General Electric Company
- Craig Douglas Young
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Methods and apparatus for cooling gas turbine engine combustors
- Patent number 6,530,227
- Issue date Mar 11, 2003
- General Electric Co.
- Craig Douglas Young
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel nozzle assembly for reduced exhaust emissions
- Patent number 6,389,815
- Issue date May 21, 2002
- General Electric Company
- Harjit Singh Hura
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Dilution pole combustor and method
- Patent number 5,239,818
- Issue date Aug 31, 1993
- General Electric Company
- Richard W. Stickles
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Double dome combustor and method of operation
- Patent number 5,197,278
- Issue date Mar 30, 1993
- General Electric Company
- Paul E. Sabla
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Lean staged combustion assembly
- Patent number 5,099,644
- Issue date Mar 31, 1992
- General Electric Company
- Paul E. Sabla
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine carburetor
- Patent number 4,653,278
- Issue date Mar 31, 1987
- General Electric Company
- John W. Vinson
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Paul E. Sabla

Person

Patents Grantslast 30 patents

Anti-carboning fuel-air mixer for a gas turbine engine combustor

Methods and apparatus for cooling gas turbine engine combustors

Methods and apparatus for cooling gas turbine engine combustors

Fuel nozzle assembly for reduced exhaust emissions

Dilution pole combustor and method

Double dome combustor and method of operation

Lean staged combustion assembly

Gas turbine engine carburetor