Inventor · disambiguated record
Michael T. Barton
Also filed as: BARTON MICHAEL · BARTON MICHAEL T · BARTON MICHAEL T TODD · BARTON MICHAEL TODD
16 granted patents·2 pending applications·202 citations·filing 2003–2024
93Inventor score
Top patents by PatentIndex Score
18 records- 0194US10359051B2Impeller shroud supports having mid-impeller bleed flow passages and gas turbine engines including the sameHONEYWELL INT INC·Filed 2016·Granted Jul 23, 2019·13 cites·20 claims
- 0292US9650916B2Turbomachine cooling systemsHONEYWELL INT INC·Filed 2014·Granted May 16, 2017·14 cites·15 claims
- 0388US10330121B2Systems and methods for axial compressor with secondary flowHONEYWELL INT INC·Filed 2015·Granted Jun 25, 2019·6 cites·9 claims
- 0487US9631814B1Engine 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
- 0586US7500364B2System for coupling flow from a centrifugal compressor to an axial combustor for gas turbinesHONEYWELL INT INC·Filed 2005·Granted Mar 10, 2009·23 cites·10 claims
- 0681US11220922B1Monolithic diffuser and deswirl flow structure for gas turbine engineHONEYWELL INT INC·Filed 2020·Granted Jan 11, 2022·2 cites·20 claims
- 0778US9970452B2Forward-swept impellers and gas turbine engines employing the sameHONEYWELL INT INC·Filed 2015·Granted May 15, 2018·3 cites·10 claims
- 0878US8122724B2Compressor including an aerodynamically variable diffuserSLOVISKY JOHN A·Filed 2004·Granted Feb 28, 2012·33 cites·2 claims
- 0978US7717672B2Radial vaned diffusion system with integral service routingsHONEYWELL INT INC·Filed 2006·Granted May 18, 2010·18 cites·20 claims
- 1077US7189059B2Compressor including an enhanced vaned shroudHONEYWELL INT INC·Filed 2004·Granted Mar 13, 2007·36 cites·26 claims
- 1175US8210794B2Axial-centrifugal compressor with ported shroudNOLCHEFF NICK A·Filed 2008·Granted Jul 3, 2012·8 cites·20 claims
- 1275US7966821B2Reduced exhaust emissions gas turbine engine combustorHONEYWELL INT INC·Filed 2009·Granted Jun 28, 2011·12 cites·2 claims
- 1368US11125158B2Ported shroud system for turboprop inletsHONEYWELL INT INC·Filed 2018·Granted Sep 21, 2021·2 cites·20 claims
- 1459US7506511B2Reduced exhaust emissions gas turbine engine combustorHONEYWELL INT INC·Filed 2003·Granted Mar 24, 2009·18 cites·12 claims
- 1552US11156092B2Multistage axial-centrifugal compressor systems and methods for manufactureHONEYWELL INT INC·Filed 2019·Granted Oct 26, 2021·0 cites·6 claims
- 1648US2025012233A1Gas turbine engines comprising pitched nose splitter structures and aircraft comprising the sameHONEYWELL INT INC·Filed 2023·Application pending·0 cites
- 1746US12359584B1Acoustic engine casing for gas turbine engineHONEYWELL INT INC·Filed 2024·Granted Jul 15, 2025·0 cites·17 claims
- 1839US2013051974A1Gas turbine engines and methods for cooling components thereof with mid-impeller bleed cooling airPOON KIN·Filed 2011·Application pending·0 cites
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →