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Inventor profile of:

Derrick Walter Simons

City:

Greer, South Carolina

Country:

United States

Published Applications:

24

Last publication date:

2016-09-08

Top Assignees for applications by Derrick Walter Simons

The entities that hold a legal rights for patent applications filed by inventor Simons Derrick Walter:

Recent patent applications by Simons Derrick Walter

Derrick Walter Simons from Greer, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2016-09-08
US20160258629A1
Mechanical engineering

Fuel staging in a gas turbine engine

 #2 | 2015-09-10
US20150253011A1
Mechanical engineering

ANNULAR PREMIXED PILOT IN FUEL NOZZLE

 #3 | 2014-09-18
US20140260261A1
Mechanical engineering

Turbomachine with transition piece having dilution holes and fuel injection system coupled to transition piece

 #4 | 2014-05-15
US20140130477A1
Mechanical engineering

Turbomachine and staged combustion system of a turbomachine

 #5 | 2013-08-29
US20130219899A1
Mechanical engineering

ANNULAR PREMIXED PILOT IN FUEL NOZZLE

 #6 | 2013-07-18
US20130180260A1
Mechanical engineering

Combustor recovery method and system

 #7 | 2013-01-31
US20130025283A1
Mechanical engineering

Sector nozzle mounting systems

 #8 | 2013-01-17
US20130014514A1
Mechanical engineering

SYSTEMS AND METHODS FOR BULK TEMPERATURE VARIATION REDUCTION OF A GAS TURBINE THROUGH CAN-TO-CAN FUEL TEMPERATURE MODULATION

 #9 | 2012-10-04
US20120247108A1
Physics

Combustor probe for gas turbine

 #10 | 2011-10-13
US20110247340A1
Mechanical engineering

APPARATUS AND METHOD FOR MINIMIZING AND/OR ELIMINATING DILUTION AIR LEAKAGE IN A COMBUSTION LINER ASSEMBLY

 #11 | 2011-07-07
US20110162377A1
Mechanical engineering

TURBOMACHINE NOZZLE

 #12 | 2010-12-30
US20100332103A1
Mechanical engineering

NOX compliant peak for gas turbine

 #13 | 2010-08-05
US20100192587A1
Mechanical engineering

COMBUSTOR ASSEMBLY FOR USE IN A GAS TURBINE ENGINE AND METHOD OF ASSEMBLING SAME

 #14 | 2010-08-05
US20100192580A1
Mechanical engineering

Combustion System Burner Tube

 #15 | 2010-03-11
US20100058767A1
Mechanical engineering

SWIRL ANGLE OF SECONDARY FUEL NOZZLE FOR TURBOMACHINE COMBUSTOR

 #16 | 2009-08-27
US20090211255A1
Mechanical engineering

GAS TURBINE COMBUSTOR FLAME STABILIZER

 #17 | 2009-02-26
US20090053054A1
Mechanical engineering

LEAKAGE REDUCING VENTURI FOR DRY LOW NITRIC OXIDES (NOx) COMBUSTORS

 #18 | 2009-01-22
US20090019854A1
Mechanical engineering

APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTOR

 #19 | 2008-12-04
US20080295521A1
Mechanical engineering

Method and apparatus for assembling turbine engines

 #20 | 2008-03-13
US20080060358A1
Mechanical engineering

Mixing hole arrangement and method for improving homogeneity of an air and fuel mixture in a combustor

 #21 | 2007-07-12
US20070157620A1
Mechanical engineering

Method for controlling fuel splits to gas turbine combustor

 #22 | 2006-08-03
US20060168967A1
Mechanical engineering

Inboard radial dump venturi for combustion chamber of a gas turbine

 #23 | 2005-09-22
US20050204741A1
Mechanical engineering

Turbine combustor transition piece having dilution holes

 #24 | 2005-05-26
US20050114010A1
Mechanical engineering

Method for controlling fuel splits to gas turbine combustor
InventorID:

34668 ⎘