Mowill; R. Jan

Patent Applications and Registrations

Patent applications and USPTO patent grants for Mowill; R. Jan.The latest application filed is for "apparatus and method for reducing air mass flow for extended range low emissions combustion for single shaft gas turbines".

Company Profile

0.15.4

Mowill; R. Jan - Hengelo NL
Mowill; R. Jan - 7559 CX Hengelo NL
Mowill; R. Jan - 7550 AV Hengelo NL
Mowill; R. Jan - Oslo NO

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Apparatus and method for reducing air mass flow for extended range low emissions combustion for single shaft gas turbines Grant 8,596,035 - Mowill December 3, 2	2013-12-03
Apparatus And Method For Reducing Air Mass Flow For Extended Range Low Emissions Combustion For Single Shaft Gas Turbines App 20130000315 - MOWILL; R. Jan	2013-01-03
Turbine inlet nozzle guide vane mounting structure for radial gas turbine engine Grant 8,001,792 - Dvorak , et al. August 23, 2	2011-08-23
Single stage dual-entry centriafugal compressor, radial turbine gas generator Grant 7,628,018 - Mowill December 8, 2	2009-12-08
Single Stage Dual-entry Centrifugal Compressor, Radial Turbine Gas Generator App 20090232676 - Mowill; R. Jan	2009-09-17
Apparatus and method for gas turbine engine fuel/air premixer exit velocity control Grant 7,162,874 - Mowill January 16, 2	2007-01-16
Apparatus and method for gas turbine engine fuel/air premixer exit velocity control App 20060021354 - Mowill; R. Jan	2006-02-02
Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities Grant 6,925,809 - Mowill August 9, 2	2005-08-09
Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities App 20020069645 - Mowill, R. Jan	2002-06-13
Convectively cooled, single stage, fully premixed controllable fuel/air combustor Grant 6,220,034 - Mowill April 24, 2	2001-04-24
Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission Grant 5,765,363 - Mowill June 16, 1	1998-06-16
Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission Grant 5,638,674 - Mowill June 17, 1	1997-06-17
Star combustor with dilution ports in can portions Grant 5,628,182 - Mowill May 13, 1	1997-05-13
Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules Grant 5,572,862 - Mowill November 12, 1	1996-11-12
Single stage premixed constant fuel/air ratio combustor Grant 5,481,866 - Mowill January 9, 1	1996-01-09
Process for single stage premixed constant fuel/air ratio combustion Grant 5,377,483 - Mowill January 3, 1	1995-01-03
Apparatus for mounting, and for maintaining running clearance in, a double entry radial compressor Grant 4,704,861 - Mowill November 10, 1	1987-11-10
Dual entry radial turbine gas generator Grant 4,641,495 - Mowill February 10, 1	1987-02-10

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