Inventor · disambiguated record
Xiaolan Hu
Also filed as: HU XIAOLAN
25 granted patents·10 pending applications·192 citations·filing 2000–2023
94Inventor score
Top patents by PatentIndex Score
35 records- 0194US10208624B2Lubrication of journal bearing during clockwise and counter-clockwise rotationUNITED TECHNOLOGIES CORP·Filed 2013·Granted Feb 19, 2019·25 cites·10 claims
- 0293US6627019B2Process for making ceramic matrix composite parts with cooling channelsFiled 2000·Granted Sep 30, 2003·86 cites·27 claims
- 0392US9121302B2Radial compressor blade clearance control systemDUONG LOC QUANG·Filed 2012·Granted Sep 1, 2015·17 cites·20 claims
- 0489US9856751B2Nonlinear rolling bearing radial support stiffnessUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jan 2, 2018·7 cites·13 claims
- 0588US10415391B2Rotor and gas turbine engine including a rotorUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 17, 2019·6 cites·17 claims
- 0681US8936439B2Radial turbine backface curvature stress reductionDUONG LOC QUANG·Filed 2011·Granted Jan 20, 2015·8 cites·21 claims
- 0779US9963974B2Reduction of equally spaced turbine nozzle vane excitationUNITED TECHNOLOGIES CORP·Filed 2012·Granted May 8, 2018·6 cites·10 claims
- 0878US10233758B2Detuning trailing edge compound lean contourUNITED TECHNOLOGIES CORP·Filed 2014·Granted Mar 19, 2019·6 cites·23 claims
- 0975US8172510B2Radial compressor of asymmetric cyclic sector with coupled blades tuned at anti-nodesDUONG LOC Q·Filed 2009·Granted May 8, 2012·15 cites·20 claims
- 1072US8172511B2Radial compressor with blades decoupled and tuned at anti-nodesDUONG LOC Q·Filed 2009·Granted May 8, 2012·7 cites·24 claims
- 1167US10087762B2Scallop curvature for radial turbine wheelDUONG LOC QUANG·Filed 2011·Granted Oct 2, 2018·3 cites·28 claims
- 1260US8876484B2Turbine blade pocket pin stress reliefDUONG LOC QUANG·Filed 2011·Granted Nov 4, 2014·1 cites·16 claims
- 1356US12377990B2Lip skin with hydrophobic and hydrophlic surfaces for an aircraft aerostructureROHR INC·Filed 2023·Granted Aug 5, 2025·0 cites·16 claims
- 1454US2023145026A1Silicon-controlled rectifier water-cooling heat dissipation deviceSHANGHAI KOHLER ELECTRONICS·Filed 2022·Application pending·0 cites
- 1553US11873781B1Thrust reverser cascade with one or more flow stabilizersROHR INC·Filed 2022·Granted Jan 16, 2024·0 cites·19 claims
- 1653US8534990B2Inlet guide vane drive system with spring preload on mechanical linkageDUONG LOC QUANG·Filed 2009·Granted Sep 17, 2013·4 cites·4 claims
- 1752US12270356B2Thrust reverser cascade with one or more flow disruptersROHR INC·Filed 2022·Granted Apr 8, 2025·0 cites·19 claims
- 1850US11167855B2Method and apparatus for aircraft anti-icingROHR INC·Filed 2019·Granted Nov 9, 2021·0 cites·20 claims
- 1950US2011064340A1Method and apparatus for stabilizing a squeeze film damper for a rotating machineDUONG LOC QUANG·Filed 2009·Application pending·0 cites
- 2049US9957825B2Non-linearly deflecting brush seal landUNITED TECHNOLOGIES CORP·Filed 2016·Granted May 1, 2018·0 cites·14 claims
- 2148US10309256B2Non-linear bumper bearingsUNITED TECHNOLOGIES CORP·Filed 2014·Granted Jun 4, 2019·0 cites·20 claims
- 2247US8926289B2Blade pocket designDUONG LOC QUANG·Filed 2012·Granted Jan 6, 2015·0 cites·14 claims
- 2347US8915088B2Fuel control method for starting a gas turbine engineAJAMI ANDRE M·Filed 2010·Granted Dec 23, 2014·1 cites·18 claims
- 2446US8864471B2Gas turbine rotor with purge bladesDUONG LOC QUANG·Filed 2011·Granted Oct 21, 2014·0 cites·15 claims
- 2544US2009077973A1Gas Turbine Fuel System for High Altitude Starting and OperationHAMILTON SUNDSTRAND CORP·Filed 2007·Application pending·0 cites
- 2644US2014174098A1Turbine disc with reduced neck stress concentrationUNITED TECHNOLOGIES CORP·Filed 2012·Application pending·0 cites
- 2743US8694285B2Turbine blade base load balancingDUONG LOC QUANG·Filed 2011·Granted Apr 8, 2014·0 cites·18 claims
- 2842US2015354459A1Fuel injector for high altitude starting and operation of a gas turbine engineHAMILTON SUNDSTRAND CORP·Filed 2014·Application pending·0 cites
- 2942US2011072823A1Gas turbine engine fuel injectorCHEN DAIH-YEOU·Filed 2009·Application pending·0 cites
- 3042US2012288373A1Rotor with asymmetric blade spacingDUONG LOC QUANG·Filed 2011·Application pending·0 cites
- 3141US12435682B2Thrust reverser cascade with offset vane leading edgesROHR INC·Filed 2022·Granted Oct 7, 2025·0 cites·20 claims
- 3241US2013236325A1Blade tip profileDUONG LOC QUANG·Filed 2012·Application pending·0 cites
- 3341US2011274537A1Blade excitation reduction method and arrangementDUONG LOC QUANG·Filed 2010·Application pending·0 cites
- 3434US9874275B2Two-speed planetary transmissionChangfeng group co ltd·Filed 2016·Granted Jan 23, 2018·0 cites·18 claims
- 3534US2016208688A1Inflow radial turbine with reduced bore stress concentrationUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →