Igor Petrovich Sidko

Person

Moscow, RU

People

Patents Grantslast 30 patents

Information Patent Grant
System and method for an oxidant passageway in a gas turbine system...
- Patent number 10,788,212
- Issue date Sep 29, 2020
- General Electric Company
- Jonathan Kay Allen
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Fuel staging in a gas turbine engine
- Patent number 10,480,792
- Issue date Nov 19, 2019
- General Electric Company
- Ilya Aleksandrovich Slobodyanskiy
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Turbine system with exhaust gas recirculation, separation and extra...
- Patent number 10,316,746
- Issue date Jun 11, 2019
- General Electric Company
- Jonathan Kay Allen
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine system with exhaust gas recirculation, separation and extra...
- Patent number 10,253,690
- Issue date Apr 9, 2019
- General Electric Company
- Jonathan Kay Allen
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
System and method for a turbine combustor
- Patent number 10,221,762
- Issue date Mar 5, 2019
- General Electric Company
- Almaz Kamilevich Valeev
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Systems and methods for high volumetric oxidant flow in gas turbine...
- Patent number 10,094,566
- Issue date Oct 9, 2018
- General Electric Company
- Bradford David Borchert
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES

Patents Applicationslast 30 patents

Information Patent Application
FUEL STAGING IN A GAS TURBINE ENGINE
- Publication number 20160258629
- Publication date Sep 8, 2016
- GENERAL ELECTRIC COMPANY
- Ilya Aleksandrovich Slobodyanskiy
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE SYSTEM WITH EXHAUST GAS RECIRCULATION, SEPARATION AND EXTRA...
- Publication number 20160222884
- Publication date Aug 4, 2016
- GENERAL ELECTRIC COMPANY
- Jonathan Kay Allen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEMS AND METHODS FOR HIGH VOLUMETRIC OXIDANT FLOW IN GAS TURBINE...
- Publication number 20160223202
- Publication date Aug 4, 2016
- GENERAL ELECTRIC COMPANY
- Bradford David Borchert
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
TURBINE SYSTEM WITH EXHAUST GAS RECIRCULATION, SEPARATION AND EXTRA...
- Publication number 20160222883
- Publication date Aug 4, 2016
- GENERAL ELECTRIC COMPANY
- Jonathan Kay Allen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR AN OXIDANT PASSAGEWAY IN A GAS TURBINE SYSTEM...
- Publication number 20160201916
- Publication date Jul 14, 2016
- GENERAL ELECTRIC COMPANY
- Jonathan Kay Allen
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
SYSTEM AND METHOD FOR A TURBINE COMBUSTOR
- Publication number 20160010548
- Publication date Jan 14, 2016
- GENERAL ELECTRIC COMPANY
- Almaz Kamilevich Valeev
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Igor Petrovich Sidko

Person

Patents Grantslast 30 patents

System and method for an oxidant passageway in a gas turbine system...

Fuel staging in a gas turbine engine

Turbine system with exhaust gas recirculation, separation and extra...

Turbine system with exhaust gas recirculation, separation and extra...

System and method for a turbine combustor

Systems and methods for high volumetric oxidant flow in gas turbine...

Patents Applicationslast 30 patents

FUEL STAGING IN A GAS TURBINE ENGINE

TURBINE SYSTEM WITH EXHAUST GAS RECIRCULATION, SEPARATION AND EXTRA...

SYSTEMS AND METHODS FOR HIGH VOLUMETRIC OXIDANT FLOW IN GAS TURBINE...

TURBINE SYSTEM WITH EXHAUST GAS RECIRCULATION, SEPARATION AND EXTRA...

SYSTEM AND METHOD FOR AN OXIDANT PASSAGEWAY IN A GAS TURBINE SYSTEM...

SYSTEM AND METHOD FOR A TURBINE COMBUSTOR