Inventor · disambiguated record
Kin-Leung Cheung
Also filed as: CHEUNG KIN-LEUNG
14 granted patents·6 pending applications·149 citations·filing 2004–2020
92Inventor score
Top patents by PatentIndex Score
20 records- 0196US10369593B2Method of applying a nanocrystalline coating to a gas turbine engine componentPRATT & WHITNEY CANADA·Filed 2014·Granted Aug 6, 2019·16 cites·15 claims
- 0296US8871297B2Method of applying a nanocrystalline coating to a gas turbine engine componentBARNETT BARRY·Filed 2011·Granted Oct 28, 2014·26 cites·8 claims
- 0391US11391297B2Composite fan case with nanoparticlesPRATT & WHITNEY CANADA·Filed 2018·Granted Jul 19, 2022·7 cites·17 claims
- 0489US9970824B2Sensor probe with anti-icingPRATT & WHITNEY CANADA·Filed 2015·Granted May 15, 2018·17 cites·18 claims
- 0586US7025356B1Air-oil sealPRATT & WHITNEY CANADA·Filed 2004·Granted Apr 11, 2006·37 cites·8 claims
- 0683US9427835B2Nano-metal coated vane component for gas turbine engines and method of manufacturing sameCHEUNG KIN-LEUNG·Filed 2012·Granted Aug 30, 2016·11 cites·15 claims
- 0783US8182213B2Vane assembly with removable vanesCHEUNG KIN-LEUNG·Filed 2009·Granted May 22, 2012·13 cites·20 claims
- 0882US11466622B2Composite aerospace componentPRATT & WHITNEY CANADA·Filed 2018·Granted Oct 11, 2022·1 cites·16 claims
- 0981US8545167B2Composite casing for rotating bladesCHEUNG KIN-LEUNG·Filed 2009·Granted Oct 1, 2013·15 cites·16 claims
- 1065US9804058B2Method of facilitating visual detection of a crack in a component of a gas turbine enginePRATT & WHITNEY CANADA·Filed 2014·Granted Oct 31, 2017·2 cites·9 claims
- 1161US9909501B2Acoustic structure for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2014·Granted Mar 6, 2018·2 cites·19 claims
- 1256US9919500B2Inner bypass ductPRATT & WHITNEY CANADA·Filed 2014·Granted Mar 20, 2018·2 cites·19 claims
- 1355US2018045608A1Method of facilitating visual detection of a crack in a component of a gas turbine enginePRATT & WHITNEY CANADA·Filed 2017·Application pending·0 cites
- 1454US2015239010A1Method of forming an abradable coating for a gas turbine enginePRATT & WHITNEY CANADA·Filed 2014·Application pending·0 cites
- 1554US2008286459A1Method for applying abradable coatingPRATT & WHITNEY CANADA·Filed 2007·Application pending·0 cites
- 1649US2016045926A1Abradable coatings for gas turbine engine componentsPRATT & WHITNEY CANADA·Filed 2014·Application pending·0 cites
- 1748US2022106885A1Hybrid vanes for gas turbine enginesPRATT & WHITNEY CANADA·Filed 2020·Application pending·0 cites
- 1845US10718350B2Fan blade with galvanic separatorPRATT & WHITNEY CANADA·Filed 2016·Granted Jul 21, 2020·0 cites·20 claims
- 1944US10711625B2Wall construction for gaspath traversing componentPRATT & WHITNEY CANADA·Filed 2013·Granted Jul 14, 2020·0 cites·20 claims
- 2038US2013251500A1Gas turbine engine case with heating layer and methodCHEUNG KIN-LEUNG·Filed 2012·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →