Inventor profile of:

Wei Chen

City:

Greer, South Carolina

Country:

United States

Published Applications:

37

Last publication date:

2018-11-15

Top Assignees for applications by Wei Chen

The entities that hold a legal rights for patent applications filed by inventor Chen Wei:

Recent patent applications by Chen Wei

Wei Chen from Greer, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2018-11-15
US20180328588A1
Mechanical engineering

Dual fuel injectors and methods of use in gas turbine combustor

#2 | 2017-08-10
US20170226929A1
Mechanical engineering

FUEL INJECTOR COVERS AND METHODS OF FABRICATING SAME

#3 | 2016-04-28
US20160115799A1
Mechanical engineering

METHOD OF FORMING TURBULATORS ON A TURBOMACHINE SURFACE AND APPARATUS

#4 | 2015-03-05
US20150059348A1
Mechanical engineering

SYSTEM AND METHOD FOR CONTROLLING FUEL DISTRIBUTIONS IN A COMBUSTOR IN A GAS TURBINE ENGINE

#5 | 2014-09-18
US20140260279A1
Mechanical engineering

Hot gas path duct for a combustor of a gas turbine

#6 | 2014-06-26
US20140174090A1
Mechanical engineering

SYSTEM FOR SUPPLYING FUEL TO A COMBUSTOR

#7 | 2014-05-15
US20140130504A1
Mechanical engineering

SYSTEM FOR COOLING A HOT GAS COMPONENT FOR A COMBUSTOR OF A GAS TURBINE

#8 | 2014-05-15
US20140130477A1
Mechanical engineering

Turbomachine and staged combustion system of a turbomachine

#9 | 2014-05-08
US20140123653A1
Mechanical engineering

ENHANCEMENT FOR FUEL INJECTOR

#10 | 2014-05-08
US20140123650A1
Mechanical engineering

Micro-mixer nozzle

#11 | 2014-05-01
US20140116058A1
Mechanical engineering

Assemblies and apparatus related to combustor cooling in turbine engines

#12 | 2014-05-01
US20140116053A1
Mechanical engineering

Fuel injection assemblies in combustion turbine engines

#13 | 2014-04-10
US20140096530A1
Mechanical engineering

Air management arrangement for a late lean injection combustor system and method of routing an airflow

#14 | 2014-02-13
US20140041391A1
Performing operations; transporting

APPARATUS INCLUDING A FLOW CONDITIONER COUPLED TO A TRANSITION PIECE FORWARD END

#15 | 2014-02-06
US20140033726A1
Mechanical engineering

LINER COOLING ASSEMBLY FOR A GAS TURBINE SYSTEM

#16 | 2014-02-06
US20140033725A1
Mechanical engineering

Injector seal for a gas turbomachine

#17 | 2014-01-16
US20140013758A1
Mechanical engineering

System for supplying a working fluid to a combustor

#18 | 2013-12-05
US20130318991A1
Mechanical engineering

Combustor With Multiple Combustion Zones With Injector Placement for Component Durability

#19 | 2013-09-19
US20130239575A1
Mechanical engineering

System for supplying a fuel and a working fluid through a liner to a combustion chamber

#20 | 2013-09-12
US20130236301A1
Mechanical engineering

Apparatus And System For Directing Hot Gas

#21 | 2013-09-12
US20130232980A1
Mechanical engineering

System for supplying a fuel and working fluid mixture to a combustor

#22 | 2013-07-09
US13546398
-

System for supplying a working fluid to a combustor

#23 | 2013-04-18
US20130091847A1
Mechanical engineering

COMBUSTOR LINER

#24 | 2013-04-11
US20130089823A1
Mechanical engineering

COMBUSTOR

#25 | 2013-04-11
US20130086920A1
Mechanical engineering

COMBUSTOR AND METHOD FOR SUPPLYING FLOW TO A COMBUSTOR

#26 | 2012-12-06
US20120304659A1
Mechanical engineering

Impingement sleeve and methods for designing and forming impingement sleeve

#27 | 2012-11-08
US20120279226A1
Mechanical engineering

Hula seal with preferential cooling having spring fingers and/or adjacent slots with different widths

#28 | 2012-09-20
US20120234012A1
Mechanical engineering

Impingement sleeve and methods for designing and forming impingement sleeve

#29 | 2011-07-07
US20110162378A1
Mechanical engineering

TUNABLE TRANSITION PIECE AFT FRAME

#30 | 2010-11-25
US20100293957A1
Mechanical engineering

System and method for cooling a wall of a gas turbine combustor

#31 | 2010-10-07
US20100251723A1
Mechanical engineering

Thimble, sleeve, and method for cooling a combustor assembly

#32 | 2010-07-29
US20100186416A1
Mechanical engineering

Flow conditioner for use in gas turbine component in which combustion occurs

#33 | 2010-07-08
US20100170249A1
Mechanical engineering

Method and apparatus to facilitate cooling of a diffusion tip within a gas turbine engine

#34 | 2010-02-18
US20100037622A1
Mechanical engineering

Contoured Impingement Sleeve Holes

#35 | 2010-01-14
US20100005804A1
Mechanical engineering

COMBUSTOR STRUCTURE

#36 | 2009-10-15
US20090255267A1
Mechanical engineering

Combustor seal having multiple cooling fluid pathways

#37 | 2008-07-10
US20080166220A1
Mechanical engineering

Airfoil, sleeve, and method for assembling a combustor assembly

InventorID:

181411 ⎘