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Inventor profile of:

Gregory Thomas FOSTER

City:

Greer, South Carolina

Country:

United States

Published Applications:

56

Last publication date:

2022-02-24

Top Assignees for applications by Gregory Thomas FOSTER

The entities that hold a legal rights for patent applications filed by inventor FOSTER Gregory Thomas:

Recent patent applications by FOSTER Gregory Thomas

Gregory Thomas FOSTER from Greer, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2022-02-24
US20220056805A1
Mechanical engineering

Flared central cavity aft of airfoil leading edge

 #2 | 2020-02-27
US20200063574A1
Mechanical engineering

Flared central cavity aft of airfoil leading edge

 #3 | 2018-12-20
US20180363471A1
Mechanical engineering

System and method for near wall cooling for turbine component

 #4 | 2018-12-20
US20180363470A1
Mechanical engineering

System and method for near wall cooling for turbine component

 #5 | 2018-11-15
US20180328192A1
Mechanical engineering

Cooling circuits for a multi-wall blade

 #6 | 2018-06-14
US20180163544A1
Mechanical engineering

Turbine airfoil with trailing edge cooling circuit

 #7 | 2018-05-17
US20180135430A1
Mechanical engineering

Support for a multi-wall core

 #8 | 2018-04-26
US20180112547A1
Mechanical engineering

Turbine airfoil trailing edge coolant passage created by cover

 #9 | 2018-04-26
US20180112541A1
Mechanical engineering

Cooling circuits for a multi-wall blade

 #10 | 2018-04-26
US20180112540A1
Mechanical engineering

Edge coupon including cooling circuit for airfoil

 #11 | 2018-04-26
US20180112539A1
Mechanical engineering

Cooling circuits for a multi-wall blade

 #12 | 2018-04-26
US20180112534A1
Mechanical engineering

Turbine airfoil coolant passage created in cover

 #13 | 2018-02-22
US20180051575A1
Mechanical engineering

Cooling circuit for a multi-wall blade

 #14 | 2018-02-22
US20180051574A1
Mechanical engineering

Cooling circuit for a multi-wall blade

 #15 | 2017-11-16
US20170328220A1
Mechanical engineering

Internal rib with defined concave surface curvature for airfoil

 #16 | 2017-11-16
US20170328219A1
Mechanical engineering

Blade with stress-reducing bulbous projection at turn opening of coolant passages

 #17 | 2017-11-16
US20170328218A1
Mechanical engineering

Flared central cavity aft of airfoil leading edge

 #18 | 2017-11-16
US20170328211A1
Mechanical engineering

Intermediate central passage spanning outer walls aft of airfoil leading edge passage

 #19 | 2017-06-22
US20170175580A1
Mechanical engineering

System and method for cooling turbine shroud

 #20 | 2017-06-22
US20170175576A1
Mechanical engineering

SYSTEM AND METHOD FOR UTILIZING TARGET FEATURES IN FORMING INLET PASSAGES IN MICRO-CHANNEL CIRCUIT

 #21 | 2017-06-22
US20170175574A1
Mechanical engineering

METHOD FOR METERING MICRO-CHANNEL CIRCUIT

 #22 | 2017-06-22
US20170175550A1
Mechanical engineering

Turbine airfoil with trailing edge cooling circuit

 #23 | 2017-06-22
US20170175549A1
Mechanical engineering

Turbine airfoil with trailing edge cooling circuit

 #24 | 2017-06-22
US20170175548A1
Mechanical engineering

Cooling circuits for a multi-wall blade

 #25 | 2017-06-22
US20170175547A1
Mechanical engineering

Cooling circuit for a multi-wall blade

 #26 | 2017-06-22
US20170175546A1
Mechanical engineering

Cooling circuit for a multi-wall blade

 #27 | 2017-06-22
US20170175545A1
Mechanical engineering

Platform core feed for a multi-wall blade

 #28 | 2017-06-22
US20170175541A1
Mechanical engineering

Cooling circuit for a multi-wall blade

 #29 | 2017-06-22
US20170173672A1
Performing operations; transporting

Center plenum support for a multiwall turbine airfoil casting

 #30 | 2016-06-16
US20160169524A1
Mechanical engineering

Injection systems for fuel and gas

 #31 | 2016-06-16
US20160169520A1
Mechanical engineering

Injector apparatus with reheat combustor and turbomachine

 #32 | 2016-06-16
US20160169519A1
Mechanical engineering

Injector apparatus and reheat combustor

 #33 | 2016-06-16
US20160169518A1
Mechanical engineering

Injecting apparatus with reheat combustor and turbomachine

 #34 | 2015-12-03
US20150345300A1
Mechanical engineering

Cooling structure for stationary blade

 #35 | 2015-08-06
US20150218962A1
Mechanical engineering

Micro channel and methods of manufacturing a micro channel

 #36 | 2015-07-02
US20150184530A1
Mechanical engineering

Turbine nozzle and method for cooling a turbine nozzle of a gas turbine engine

 #37 | 2015-07-02
US20150184520A1
Mechanical engineering

Interior cooling circuits in turbine blades

 #38 | 2015-07-02
US20150184519A1
Mechanical engineering

Structural configurations and cooling circuits in turbine blades

 #39 | 2015-04-30
US20150118022A1
Mechanical engineering

Re-use of internal cooling by medium in turbine hot gas path components

 #40 | 2015-04-16
US20150101346A1
Mechanical engineering

Locking spacer assembly

 #41 | 2015-04-09
US20150098808A1
Mechanical engineering

Method and system to facilitate sealing in gas turbines

 #42 | 2015-02-05
US20150037165A1
Mechanical engineering

Turbine blade with sectioned pins

 #43 | 2015-01-15
US20150013345A1
Mechanical engineering

GAS TURBINE SHROUD COOLING

 #44 | 2014-11-20
US20140338772A1
Mechanical engineering

Active sealing member

 #45 | 2014-03-13
US20140070457A1
Chemistry; metallurgy

Methods of forming a ceramic component and a high temperature mold component for use therewith

 #46 | 2013-11-28
US20130315719A1
Mechanical engineering

Turbine Shroud Cooling Assembly for a Gas Turbine System

 #47 | 2013-10-10
US20130266435A1
Mechanical engineering

Turbine shroud assembly and method of forming

 #48 | 2013-07-11
US20130177384A1
Mechanical engineering

Turbine nozzle compartmentalized cooling system

 #49 | 2013-07-11
US20130175357A1
Mechanical engineering

Turbine nozzle cooling assembly

 #50 | 2013-03-07
US20130058764A1
Mechanical engineering

Stepped, conical honeycomb seal carrier

 #51 | 2012-11-29
US20120297792A1
Mechanical engineering

THERMOCOUPLE WELL FOR A TURBOMACHINE

 #52 | 2012-10-18
US20120263582A1
Mechanical engineering

Ceramic matrix composite shroud attachment system

 #53 | 2012-10-18
US20120260670A1
Mechanical engineering

Apparatus to seal with a turbine blade stage in a gas turbine

 #54 | 2012-08-30
US20120219404A1
Mechanical engineering

Turbine shroud and a method for manufacturing the turbine shroud

 #55 | 2012-05-31
US20120134791A1
Mechanical engineering

Gas turbine nozzle attachment scheme and removal/installation method

 #56 | 2005-11-03
US20050244267A1
Mechanical engineering

System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor
InventorID:

126474 ⎘