Ibrahim Sezer

Person

Greenville, SC, US

People

Patents Grantslast 30 patents

Information Patent Grant
Curved seal for adjacent gas turbine components
- Patent number 11,773,739
- Issue date Oct 3, 2023
- General Electric Company
- Neelesh Nandkumar Sarawate
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine airfoil with leading edge cooling passage(s) coupled via pl...
- Patent number 11,572,803
- Issue date Feb 7, 2023
- General Electric Company
- Benjamin Paul Lacy
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Gas turbine component with ejection circuit for removing debris fro...
- Patent number 11,525,397
- Issue date Dec 13, 2022
- General Electric Company
- Brendon James Leary
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Integrated combustor nozzles with continuously curved liner segments
- Patent number 11,231,175
- Issue date Jan 25, 2022
- General Electric Company
- Jonathan Dwight Berry
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Curved seal for adjacent gas turbine components
- Patent number 11,047,248
- Issue date Jun 29, 2021
- General Electric Company
- Neelesh Nandkumar Sarawate
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine shroud including plurality of cooling passages
- Patent number 10,989,068
- Issue date Apr 27, 2021
- General Electric Company
- Travis J Packer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
System and method for shroud cooling in a gas turbine engine
- Patent number 10,975,724
- Issue date Apr 13, 2021
- General Electric Company
- Ibrahim Sezer
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Turbine shroud including cooling passages in communication with col...
- Patent number 10,837,315
- Issue date Nov 17, 2020
- General Electric Company
- Benjamin Paul Lacy
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Transition manifolds for cooling channel connections in cooled stru...
- Patent number 10,519,861
- Issue date Dec 31, 2019
- General Electric Company
- Daniel Robert Burnos
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Gas turbine seals
- Patent number 10,472,980
- Issue date Nov 12, 2019
- General Electric Company
- Gary Michael Itzel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Article and manifold for thermal adjustment of a turbine component
- Patent number 9,995,151
- Issue date Jun 12, 2018
- General Electric Company
- Ibrahim Sezer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbomachine and turbine nozzle therefor
- Patent number 9,963,985
- Issue date May 8, 2018
- General Electric Company
- Rohit Chouhan
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Seal in a gas turbine engine having a shim base and a honeycomb str...
- Patent number 9,816,388
- Issue date Nov 14, 2017
- General Electric Company
- Kevin Richard Kirtley
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Sealing arrangement for a turbine system and method of sealing betw...
- Patent number 9,464,536
- Issue date Oct 11, 2016
- General Electric Company
- Xiuzhang James Zhang
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Grant
Shroud block segment for a gas turbine
- Patent number 9,464,538
- Issue date Oct 11, 2016
- General Electric Company
- Ibrahim Sezer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Nozzle mounting and sealing assembly for a gas turbine system and m...
- Patent number 9,127,557
- Issue date Sep 8, 2015
- General Electric Company
- Charles Lewis Davis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Patents Applicationslast 30 patents

Information Patent Application
GAS TURBINE COMPONENT WITH EJECTION CIRCUIT FOR REMOVING DEBRIS FRO...
- Publication number 20220065165
- Publication date Mar 3, 2022
- GENERAL ELECTRIC COMPANY
- Brendon James Leary
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
CURVED SEAL FOR ADJACENT GAS TURBINE COMPONENTS
- Publication number 20210324754
- Publication date Oct 21, 2021
- Neelesh Nandkumar Sarawate
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
HOT GAS PATH COMPONENTS INCLUDING AFT END EXHAUST CONDUITS AND AFT...
- Publication number 20210246829
- Publication date Aug 12, 2021
- GENERAL ELECTRIC COMPANY
- Jason Ray Gregg
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING...
- Publication number 20200392853
- Publication date Dec 17, 2020
- GENERAL ELECTRIC COMPANY
- Benjamin Paul Lacy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE SHROUD INCLUDING COOLING PASSAGES IN COMMUNICATION WITH COL...
- Publication number 20200131929
- Publication date Apr 30, 2020
- Benjamin Paul Lacy
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
SYSTEM AND METHOD FOR SHROUD COOLING IN A GAS TURBINE ENGINE
- Publication number 20200131932
- Publication date Apr 30, 2020
- GENERAL ELECTRIC COMPANY
- Ibrahim Sezer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
TURBINE SHROUD INCLUDING PLURALITY OF COOLING PASSAGES
- Publication number 20200025026
- Publication date Jan 23, 2020
- Travis J Packer
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
CURVED SEAL FOR ADJACENT GAS TURBINE COMPONENTS
- Publication number 20190383156
- Publication date Dec 19, 2019
- GENERAL ELECTRIC COMPANY
- Neelesh Nandkumar Sarawate
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
INTEGRATED COMBUSTOR NOZZLES WITH CONTINUOUSLY CURVED LINER SEGMENTS
- Publication number 20190383488
- Publication date Dec 19, 2019
- GENERAL ELECTRIC COMPANY
- Jonathan Dwight Berry
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
GAS TURBINE SEALS
- Publication number 20180230841
- Publication date Aug 16, 2018
- GENERAL ELECTRIC COMPANY
- Gary Michael Itzel
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING...
- Publication number 20180223673
- Publication date Aug 9, 2018
- GENERAL ELECTRIC COMPANY
- Benjamin Paul Lacy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT
- Publication number 20180187557
- Publication date Jul 5, 2018
- GENERAL ELECTRIC COMPANY
- Ibrahim SEZER
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Transition Manifolds for Cooling Channel Connections in Cooled Stru...
- Publication number 20180128174
- Publication date May 10, 2018
- GENERAL ELECTRIC COMPANY
- Daniel Robert Burnos
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBOMACHINE AND TURBINE NOZZLE THEREFOR
- Publication number 20170175555
- Publication date Jun 22, 2017
- General Electric Company
- Rohit Chouhan
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT
- Publication number 20170051612
- Publication date Feb 23, 2017
- GENERAL ELECTRIC COMPANY
- Ibrahim SEZER
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
TURBOMACHINE INCLUDING A COMPONENT HAVING A TRENCH
- Publication number 20150192020
- Publication date Jul 9, 2015
- GENERAL ELECTRIC COMPANY
- Anshuman Singh
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SHROUD BLOCK SEGMENT FOR A GAS TURBINE
- Publication number 20150007581
- Publication date Jan 8, 2015
- Ibrahim Sezer
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
SEALING ARRANGEMENT FOR A TURBINE SYSTEM AND METHOD OF SEALING BETW...
- Publication number 20140112753
- Publication date Apr 24, 2014
- GENERAL ELECTRIC COMPANY
- Xiuzhang James Zhang
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
HOT GAS PATH COMPONENT COOLING FILM HOLE PLATEAU
- Publication number 20140102684
- Publication date Apr 17, 2014
- GENERAL ELECTRIC COMPANY
- Ibrahim Sezer
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SOLID SEAL WITH COOLING PATHWAYS
- Publication number 20140093353
- Publication date Apr 3, 2014
- GENERAL ELECTRIC COMPANY
- Ibrahim Sezer
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Application
NOZZLE MOUNTING AND SEALING ASSEMBLY FOR A GAS TURBINE SYSTEM AND M...
- Publication number 20130327854
- Publication date Dec 12, 2013
- GENERAL ELECTRIC COMPANY
- Charles Lewis Davis
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...

Ibrahim Sezer

Person

Patents Grantslast 30 patents

Curved seal for adjacent gas turbine components

Turbine airfoil with leading edge cooling passage(s) coupled via pl...

Gas turbine component with ejection circuit for removing debris fro...

Integrated combustor nozzles with continuously curved liner segments

Curved seal for adjacent gas turbine components

Turbine shroud including plurality of cooling passages

System and method for shroud cooling in a gas turbine engine

Turbine shroud including cooling passages in communication with col...

Transition manifolds for cooling channel connections in cooled stru...

Gas turbine seals

Article and manifold for thermal adjustment of a turbine component

Turbomachine and turbine nozzle therefor

Seal in a gas turbine engine having a shim base and a honeycomb str...

Sealing arrangement for a turbine system and method of sealing betw...

Shroud block segment for a gas turbine

Nozzle mounting and sealing assembly for a gas turbine system and m...

Patents Applicationslast 30 patents

GAS TURBINE COMPONENT WITH EJECTION CIRCUIT FOR REMOVING DEBRIS FRO...

CURVED SEAL FOR ADJACENT GAS TURBINE COMPONENTS

HOT GAS PATH COMPONENTS INCLUDING AFT END EXHAUST CONDUITS AND AFT...

HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING...

TURBINE SHROUD INCLUDING COOLING PASSAGES IN COMMUNICATION WITH COL...

SYSTEM AND METHOD FOR SHROUD COOLING IN A GAS TURBINE ENGINE

TURBINE SHROUD INCLUDING PLURALITY OF COOLING PASSAGES

CURVED SEAL FOR ADJACENT GAS TURBINE COMPONENTS

INTEGRATED COMBUSTOR NOZZLES WITH CONTINUOUSLY CURVED LINER SEGMENTS

GAS TURBINE SEALS

HOT GAS PATH COMPONENT WITH METERING STRUCTURE INCLUDING CONVERGING...

ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT

Transition Manifolds for Cooling Channel Connections in Cooled Stru...

TURBOMACHINE AND TURBINE NOZZLE THEREFOR

ARTICLE AND MANIFOLD FOR THERMAL ADJUSTMENT OF A TURBINE COMPONENT

TURBOMACHINE INCLUDING A COMPONENT HAVING A TRENCH

SHROUD BLOCK SEGMENT FOR A GAS TURBINE

SEALING ARRANGEMENT FOR A TURBINE SYSTEM AND METHOD OF SEALING BETW...

HOT GAS PATH COMPONENT COOLING FILM HOLE PLATEAU

SOLID SEAL WITH COOLING PATHWAYS

NOZZLE MOUNTING AND SEALING ASSEMBLY FOR A GAS TURBINE SYSTEM AND M...