Inventor · disambiguated record
Hukam Chand Mongia
Also filed as: MONGIA HUKAM C · MONGIA HUKAM CHAND
33 granted patents·4 pending applications·2,235 citations·filing 1982–2013
98Inventor score
Files withGEN ELECTRIC23GARRETT CORP4GEN MOTORS CORP4MANCINI ALFRED ALBERT2DUNCAN BEVERLY STEPHENSON1
Top patents by PatentIndex Score
37 records- 0198US6865889B2Method and apparatus to decrease combustor emissionsGEN ELECTRIC·Filed 2002·Granted Mar 15, 2005·95 cites·14 claims
- 0298US6453660B1Combustor mixer having plasma generating nozzleGEN ELECTRIC·Filed 2001·Granted Sep 24, 2002·160 cites·19 claims
- 0398US6389815B1Fuel nozzle assembly for reduced exhaust emissionsGEN ELECTRIC·Filed 2000·Granted May 21, 2002·211 cites·19 claims
- 0497US7878000B2Pilot fuel injector for mixer assembly of a high pressure gas turbine engineGEN ELECTRIC·Filed 2005·Granted Feb 1, 2011·54 cites·17 claims
- 0597US6418726B1Method and apparatus for controlling combustor emissionsGEN ELECTRIC·Filed 2001·Granted Jul 16, 2002·175 cites·20 claims
- 0697US6381964B1Multiple annular combustion chamber swirler having atomizing pilotGEN ELECTRIC·Filed 2000·Granted May 7, 2002·170 cites·14 claims
- 0797US6363726B1Mixer having multiple swirlersGEN ELECTRIC·Filed 2000·Granted Apr 2, 2002·157 cites·14 claims
- 0896US8171735B2Mixer assembly for gas turbine engine combustorMANCINI ALFRED ALBERT·Filed 2010·Granted May 8, 2012·37 cites·11 claims
- 0996US6286298B1Apparatus and method for rich-quench-lean (RQL) concept in a gas turbine engine combustor having trapped vortex cavityGEN ELECTRIC·Filed 1998·Granted Sep 11, 2001·117 cites·14 claims
- 1095US8001761B2Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustorGEN ELECTRIC·Filed 2006·Granted Aug 23, 2011·54 cites·35 claims
- 1195US6481209B1Methods and apparatus for decreasing combustor emissions with swirl stabilized mixerGEN ELECTRIC·Filed 2000·Granted Nov 19, 2002·94 cites·14 claims
- 1294US7565803B2Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passagesGEN ELECTRIC·Filed 2005·Granted Jul 28, 2009·56 cites·27 claims
- 1394US7464553B2Air-assisted fuel injector for mixer assembly of a gas turbine engine combustorGEN ELECTRIC·Filed 2005·Granted Dec 16, 2008·57 cites·20 claims
- 1494US6367262B1Multiple annular swirlerGEN ELECTRIC·Filed 2000·Granted Apr 9, 2002·174 cites·17 claims
- 1593US7762073B2Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection portsGEN ELECTRIC·Filed 2006·Granted Jul 27, 2010·45 cites·27 claims
- 1692US7581396B2Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlersGEN ELECTRIC·Filed 2005·Granted Sep 1, 2009·42 cites·13 claims
- 1792US6484489B1Method and apparatus for mixing fuel to decrease combustor emissionsGEN ELECTRIC·Filed 2001·Granted Nov 26, 2002·87 cites·17 claims
- 1891US5255506ASolid fuel combustion system for gas turbine engineGEN MOTORS CORP·Filed 1991·Granted Oct 26, 1993·93 cites·4 claims
- 1989US6405523B1Method and apparatus for decreasing combustor emissionsGEN ELECTRIC·Filed 2000·Granted Jun 18, 2002·76 cites·20 claims
- 2089US5289686ALow nox gas turbine combustor liner with elliptical apertures for air swirlingGEN MOTORS CORP·Filed 1992·Granted Mar 1, 1994·65 cites·3 claims
- 2183US7010923B2Method and apparatus to decrease combustor emissionsGEN ELECTRIC·Filed 2004·Granted Mar 14, 2006·22 cites·5 claims
- 2275US4545196AVariable geometry combustor apparatusGARRETT CORP·Filed 1982·Granted Oct 8, 1985·25 cites·5 claims
- 2372US10408454B2Gas turbine engine flow regulatingWOODWARD INC·Filed 2013·Granted Sep 10, 2019·5 cites·22 claims
- 2471US6609377B2Multiple injector combustorGEN ELECTRIC·Filed 2002·Granted Aug 26, 2003·22 cites·16 claims
- 2570US4532762AGas turbine engine variable geometry combustor apparatusGARRETT CORP·Filed 1982·Granted Aug 6, 1985·24 cites·14 claims
- 2665US4594848AGas turbine combustor operating methodGARRETT CORP·Filed 1984·Granted Jun 17, 1986·20 cites·3 claims
- 2764US6497103B2Methods for decreasing combustor emissionsGEN ELECTRIC·Filed 2002·Granted Dec 24, 2002·21 cites·6 claims
- 2862US8555645B2Fuel nozzle centerbody and method of assembling the sameDUNCAN BEVERLY STEPHENSON·Filed 2008·Granted Oct 15, 2013·9 cites·14 claims
- 2962US4567724AVariable geometry combustor apparatus and associated methodsGARRETT CORP·Filed 1984·Granted Feb 4, 1986·15 cites·7 claims
- 3060US4768446ACoal combustion systemGEN MOTORS CORP·Filed 1987·Granted Sep 6, 1988·19 cites·4 claims
- 3159US6474071B1Multiple injector combustorGEN ELECTRIC·Filed 2000·Granted Nov 5, 2002·18 cites·17 claims
- 3254US4958488ACombustion systemGEN MOTORS CORP·Filed 1989·Granted Sep 25, 1990·15 cites·2 claims
- 3352US8607575B2Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustorMYERS JR WILLIAM JOSEPH·Filed 2010·Granted Dec 17, 2013·1 cites·29 claims
- 3449US2007028618A1Mixer assembly for combustor of a gas turbine engine having a main mixer with improved fuel penetrationGEN ELECTRIC·Filed 2005·Application pending·0 cites
- 3540US2008271457A1Cooling Holes For Gas Turbine Combustor Having A Non-Uniform Diameter TherethroughGEN ELECTRIC·Filed 2007·Application pending·0 cites
- 3638US2010251719A1Centerbody for mixer assembly of a gas turbine engine combustorMANCINI ALFRED ALBERT·Filed 2006·Application pending·0 cites
- 3737US2007028595A1High pressure gas turbine engine having reduced emissionsMONGIA HUKAM C·Filed 2005·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →