Inventor · disambiguated record
R. Jan Mowill
Also filed as: MOWILL R JAN
18 granted patents·772 citations·filing 1985–2011
96Inventor score
Files withKONGSBERG VAPENFAB AS2MOWILL ROLF JAN2HIJA HOLDING B V1MOWILL R JAN1OPRA TECHNOLOGIES B V1
Top patents by PatentIndex Score
18 records- 0196US5628182AStar combustor with dilution ports in can portionsFiled 1995·Granted May 13, 1997·125 cites·15 claims
- 0296US5572862AConvectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modulesMOWILL ROLF JAN·Filed 1994·Granted Nov 12, 1996·112 cites·19 claims
- 0390US5765363AConvectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admissionFiled 1997·Granted Jun 16, 1998·92 cites·5 claims
- 0489US5481866ASingle stage premixed constant fuel/air ratio combustorFiled 1994·Granted Jan 9, 1996·52 cites·16 claims
- 0588US8596035B2Apparatus and method for reducing air mass flow for extended range low emissions combustion for single shaft gas turbinesMOWILL ROLF JAN·Filed 2011·Granted Dec 3, 2013·8 cites·20 claims
- 0686US6925809B2Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocitiesFiled 2001·Granted Aug 9, 2005·63 cites·25 claims
- 0786US4641495ADual entry radial turbine gas generatorKONGSBERG VAPENFAB AS·Filed 1985·Granted Feb 10, 1987·46 cites·26 claims
- 0885US5377483AProcess for single stage premixed constant fuel/air ratio combustionFiled 1994·Granted Jan 3, 1995·40 cites·4 claims
- 0981US8001792B1Turbine inlet nozzle guide vane mounting structure for radial gas turbine engineOPRA TECHNOLOGIES B V·Filed 2010·Granted Aug 23, 2011·14 cites·16 claims
- 1080US7628018B2Single stage dual-entry centriafugal compressor, radial turbine gas generatorMOWILL R JAN·Filed 2008·Granted Dec 8, 2009·13 cites·20 claims
- 1180US6220034B1Convectively cooled, single stage, fully premixed controllable fuel/air combustorFiled 1998·Granted Apr 24, 2001·40 cites·49 claims
- 1275US5477671ASingle stage premixed constant fuel/air ratio combustorFiled 1994·Granted Dec 26, 1995·26 cites·15 claims
- 1367US5613357AStar-shaped single stage low emission combustor systemFiled 1996·Granted Mar 25, 1997·26 cites·35 claims
- 1463US5638674AConvectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admissionFiled 1994·Granted Jun 17, 1997·27 cites·19 claims
- 1562US5924276APremixer with dilution air bypass valve assemblyFiled 1997·Granted Jul 20, 1999·38 cites·17 claims
- 1660US4704861AApparatus for mounting, and for maintaining running clearance in, a double entry radial compressorKONGSBERG VAPENFAB AS·Filed 1986·Granted Nov 10, 1987·21 cites·20 claims
- 1753US7162874B2Apparatus and method for gas turbine engine fuel/air premixer exit velocity controlHIJA HOLDING B V·Filed 2004·Granted Jan 16, 2007·9 cites·20 claims
- 1845US5988589AAir valve assembly including split-shaft and seal arrangementFiled 1997·Granted Nov 23, 1999·20 cites·8 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →