R. Jan Mowill

Person

Hengelo, NL

People

Patents Grantslast 30 patents

Information Patent Grant
Apparatus and method for reducing air mass flow for extended range...
- Patent number 8,596,035
- Issue date Dec 3, 2013
- Opra Technologies B.V.
- R. Jan Mowill
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Turbine inlet nozzle guide vane mounting structure for radial gas t...
- Patent number 8,001,792
- Issue date Aug 23, 2011
- Opra Technologies B.V.
- Marek Dvorak
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...
Information Patent Grant
Single stage dual-entry centriafugal compressor, radial turbine gas...
- Patent number 7,628,018
- Issue date Dec 8, 2009
- R. Jan Mowill
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Grant
Apparatus and method for gas turbine engine fuel/air premixer exit...
- Patent number 7,162,874
- Issue date Jan 16, 2007
- HIJA Holding B.V.
- R. Jan Mowill
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Gas turbine engine fuel/air premixers with variable geometry exit a...
- Patent number 6,925,809
- Issue date Aug 9, 2005
- R. Jan Mowill
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Grant
Convectively cooled, single stage, fully premixed controllable fuel...
- Patent number 6,220,034
- Issue date Apr 24, 2001
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Air valve assembly including split-shaft and seal arrangement
- Patent number 5,988,589
- Issue date Nov 23, 1999
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Premixer with dilution air bypass valve assembly
- Patent number 5,924,276
- Issue date Jul 20, 1999
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convectively cooled, single stage, fully premixed controllable fuel...
- Patent number 5,765,363
- Issue date Jun 16, 1998
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convectively cooled, single stage, fully premixed controllable fuel...
- Patent number 5,638,674
- Issue date Jun 17, 1997
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Star combustor with dilution ports in can portions
- Patent number 5,628,182
- Issue date May 13, 1997
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Star-shaped single stage low emission combustor system
- Patent number 5,613,357
- Issue date Mar 25, 1997
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Convectively cooled, single stage, fully premixed fuel/air combusto...
- Patent number 5,572,862
- Issue date Nov 12, 1996
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Single stage premixed constant fuel/air ratio combustor
- Patent number 5,481,866
- Issue date Jan 9, 1996
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Single stage premixed constant fuel/air ratio combustor
- Patent number 5,477,671
- Issue date Dec 26, 1995
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Process for single stage premixed constant fuel/air ratio combustion
- Patent number 5,377,483
- Issue date Jan 3, 1995
- R. Jan Mowill
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Patents Applicationslast 30 patents

Information Patent Application
APPARATUS AND METHOD FOR REDUCING AIR MASS FLOW FOR EXTENDED RANGE...
- Publication number 20130000315
- Publication date Jan 3, 2013
- R. Jan MOWILL
- F04 - POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC...
Information Patent Application
SINGLE STAGE DUAL-ENTRY CENTRIFUGAL COMPRESSOR, RADIAL TURBINE GAS...
- Publication number 20090232676
- Publication date Sep 17, 2009
- R. Jan Mowill
- F01 - MACHINES OR ENGINES IN GENERAL ENGINE PLANTS IN GENERAL STEAM ENGINES
Information Patent Application
Apparatus and method for gas turbine engine fuel/air premixer exit...
- Publication number 20060021354
- Publication date Feb 2, 2006
- R. Jan Mowill
- F23 - COMBUSTION APPARATUS COMBUSTION PROCESSES
Information Patent Application
Gas turbine engine fuel/air premixers with variable geometry exit a...
- Publication number 20020069645
- Publication date Jun 13, 2002
- R. Jan Mowill
- Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMA...

R. Jan Mowill

Person

Patents Grantslast 30 patents

Apparatus and method for reducing air mass flow for extended range...

Turbine inlet nozzle guide vane mounting structure for radial gas t...

Single stage dual-entry centriafugal compressor, radial turbine gas...

Apparatus and method for gas turbine engine fuel/air premixer exit...

Gas turbine engine fuel/air premixers with variable geometry exit a...

Convectively cooled, single stage, fully premixed controllable fuel...

Air valve assembly including split-shaft and seal arrangement

Premixer with dilution air bypass valve assembly

Convectively cooled, single stage, fully premixed controllable fuel...

Convectively cooled, single stage, fully premixed controllable fuel...

Star combustor with dilution ports in can portions

Star-shaped single stage low emission combustor system

Convectively cooled, single stage, fully premixed fuel/air combusto...

Single stage premixed constant fuel/air ratio combustor

Single stage premixed constant fuel/air ratio combustor

Process for single stage premixed constant fuel/air ratio combustion

Patents Applicationslast 30 patents

APPARATUS AND METHOD FOR REDUCING AIR MASS FLOW FOR EXTENDED RANGE...

SINGLE STAGE DUAL-ENTRY CENTRIFUGAL COMPRESSOR, RADIAL TURBINE GAS...

Apparatus and method for gas turbine engine fuel/air premixer exit...

Gas turbine engine fuel/air premixers with variable geometry exit a...