Inventor · disambiguated record
Ian L. Critchley
Also filed as: CRITCHLEY IAN · CRITCHLEY IAN L
13 granted patents·6 pending applications·201 citations·filing 2000–2020
92Inventor score
Top patents by PatentIndex Score
19 records- 0189US7942006B2Combustors and combustion systems for gas turbine enginesHONEYWELL INT INC·Filed 2007·Granted May 17, 2011·26 cites·15 claims
- 0287US9631814B1Engine assemblies and methods with diffuser vane count and fuel injection assembly count relationshipsHONEYWELL INT INC·Filed 2014·Granted Apr 25, 2017·14 cites·14 claims
- 0385US7406820B2System and method for turbine engine adaptive control for mitigation of instabilitiesHONEYWELL INT INC·Filed 2005·Granted Aug 5, 2008·33 cites·11 claims
- 0481US6327860B1Fuel injector for low emissions premixing gas turbine combustorHONEYWELL INT INC·Filed 2000·Granted Dec 11, 2001·26 cites·20 claims
- 0579US11022308B2Double wall combustors with strain isolated insertsHONEYWELL INT INC·Filed 2018·Granted Jun 1, 2021·2 cites·18 claims
- 0673US6357216B1Flashback control for a gas turbine engine combustor having an air bypass systemHONEYWELL INT INC·Filed 2000·Granted Mar 19, 2002·22 cites·18 claims
- 0770US7984615B2Combustors for use in turbine engine assembliesHONEYWELL INT INC·Filed 2007·Granted Jul 26, 2011·13 cites·15 claims
- 0865US11326781B2Liner for a combustor with strain isolated insertsHONEYWELL INT INC·Filed 2020·Granted May 10, 2022·0 cites·19 claims
- 0962US7000400B2Temperature variance reduction using variable penetration dilution jetsHONEYWELL INT INC·Filed 2004·Granted Feb 21, 2006·17 cites·33 claims
- 1061US7762072B2Combustion systems with rotary fuel slingersHONEYWELL INT INC·Filed 2007·Granted Jul 27, 2010·9 cites·17 claims
- 1160US6971241B2Dual mode power unit having a combustor bypass systemHONEYWELL INT INC·Filed 2003·Granted Dec 6, 2005·19 cites·20 claims
- 1256US8127552B2Transition scrolls for use in turbine engine assembliesSCHUMACHER JURGEN C·Filed 2008·Granted Mar 6, 2012·7 cites·18 claims
- 1352US6658856B2Hybrid lean premixing catalytic combustion system for gas turbinesVERICOR POWER SYSTEMS LLC·Filed 2002·Granted Dec 9, 2003·13 cites·29 claims
- 1445US2014190171A1Combustors with hybrid walled linersHONEYWELL INT INC·Filed 2013·Application pending·0 cites
- 1542US2011219779A1Low emission combustion systems and methods for gas turbine enginesHONEYWELL INT INC·Filed 2010·Application pending·0 cites
- 1639US2008184707A1Fuel manifold for combustion systemsHONEYWELL INT INC·Filed 2006·Application pending·0 cites
- 1738US2007234725A1Counterbalanced fuel slinger in a gas turbine engineHONEYWELL INT INC·Filed 2006·Application pending·0 cites
- 1833US2005241316A1Uniform effusion cooling method for a can combustion chamberHONEYWELL INT INC·Filed 2004·Application pending·0 cites
- 1932US2003126863A1Air staged catalytic combusion systemHONEYWELL INT INC·Filed 2002·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →