Inventor · disambiguated record
George Chia-Chun Hsiao
Also filed as: HSIAO GEORGE C · HSIAO GEORGE CHIA-CHUN
7 granted patents·4 pending applications·264 citations·filing 2005–2010
88Inventor score
Files withGEN ELECTRIC7DUNCAN BEVERLY STEPHENSON1MANCINI ALFRED ALBERT1MONGIA HUKAM C1MYERS JR WILLIAM JOSEPH1
Top patents by PatentIndex Score
11 records- 0195US8001761B2Method 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
- 0294US7565803B2Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passagesGEN ELECTRIC·Filed 2005·Granted Jul 28, 2009·56 cites·27 claims
- 0394US7464553B2Air-assisted fuel injector for mixer assembly of a gas turbine engine combustorGEN ELECTRIC·Filed 2005·Granted Dec 16, 2008·57 cites·20 claims
- 0493US7762073B2Pilot 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
- 0592US7581396B2Mixer 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
- 0662US8555645B2Fuel nozzle centerbody and method of assembling the sameDUNCAN BEVERLY STEPHENSON·Filed 2008·Granted Oct 15, 2013·9 cites·14 claims
- 0752US8607575B2Method 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
- 0849US2007028618A1Mixer assembly for combustor of a gas turbine engine having a main mixer with improved fuel penetrationGEN ELECTRIC·Filed 2005·Application pending·0 cites
- 0940US2008271457A1Cooling Holes For Gas Turbine Combustor Having A Non-Uniform Diameter TherethroughGEN ELECTRIC·Filed 2007·Application pending·0 cites
- 1040US2010263382A1Dual orifice pilot fuel injectorMANCINI ALFRED ALBERT·Filed 2009·Application pending·0 cites
- 1137US2007028595A1High 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 →