Inventor · disambiguated record
Ly Nguyen
Also filed as: NGUYEN LY · NGUYEN LY D · NGUYEN LY DINH
16 granted patents·3 pending applications·309 citations·filing 1994–2023
94Inventor score
Top patents by PatentIndex Score
19 records- 0189US7442006B2Integral diffuser and deswirler with continuous flow path deflected at assemblyHONEYWELL INT INC·Filed 2005·Granted Oct 28, 2008·38 cites·13 claims
- 0286US7504877B1Charge pump and voltage regulator for body bias voltageXILINX INC·Filed 2006·Granted Mar 17, 2009·26 cites·15 claims
- 0385US12306455B2Multiaxial thermal dissipation and structurally-compliant deviceRAYTHEON CO·Filed 2023·Granted May 20, 2025·2 cites·20 claims
- 0479US6638013B2Thermally isolated housing in gas turbine engineHONEYWELL INT INC·Filed 2002·Granted Oct 28, 2003·43 cites·20 claims
- 0575US7097411B2Turbomachine compressor scroll with load-carrying inlet vanesHONEYWELL INT INC·Filed 2004·Granted Aug 29, 2006·33 cites·30 claims
- 0671US6719524B2Method of forming a thermally isolated gas turbine engine housingHONEYWELL INT INC·Filed 2002·Granted Apr 13, 2004·32 cites·20 claims
- 0768US5434226AEpoxy resin toughened with a polyether sulfone and polyarylsulfidesulfoneCIBA GEIGY CORP·Filed 1994·Granted Jul 18, 1995·29 cites·15 claims
- 0866US6968697B2Integral compressor housing of gas turbine enginesHONEYWELL INT INC·Filed 2003·Granted Nov 29, 2005·25 cites·27 claims
- 0966US6912782B2Forming and assembly method for multi-axial pivoting combustor liner in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Jul 5, 2005·11 cites·23 claims
- 1065US7007480B2Multi-axial pivoting combustor liner in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Mar 7, 2006·26 cites·26 claims
- 1156US7093448B2Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Aug 22, 2006·18 cites·14 claims
- 1253US11236791B2Multi-axial energy damping and displacement controlRAYTHEON CO·Filed 2019·Granted Feb 1, 2022·0 cites·26 claims
- 1352US7094024B2Performance and durability improvement in compressor structure designHONEYWELL INT INC·Filed 2004·Granted Aug 22, 2006·15 cites·24 claims
- 1447US11447982B2Multidirectional enclosure compression locking mechanismRAYTHEON CO·Filed 2019·Granted Sep 20, 2022·0 cites·30 claims
- 1539US7007475B2Conical helical of spiral combustor scroll device in gas turbine engineHONEYWELL INT INC·Filed 2003·Granted Mar 7, 2006·7 cites·28 claims
- 1639US6962480B2Thermally stabilized turbine scroll retention ring for uniform loading applicationHONEYWELL INT INC·Filed 2003·Granted Nov 8, 2005·4 cites·19 claims
- 1734US2007144180A1Dual bayonet engagement and method of assembling a combustor liner in a gas turbine engineHONEYWELL INT INC·Filed 2005·Application pending·0 cites
- 1833US2005241316A1Uniform effusion cooling method for a can combustion chamberHONEYWELL INT INC·Filed 2004·Application pending·0 cites
- 1929US2003005705A1Industrial gas turbine multi-axial thermal isolatorHONEYWELL INT INC·Filed 2001·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →