Inventor · disambiguated record
Bruce David Reynolds
Also filed as: REYNOLDS BRUCE · REYNOLDS BRUCE D · REYNOLDS BRUCE DAVID
27 granted patents·5 pending applications·117 citations·filing 1996–2024
95Inventor score
Top patents by PatentIndex Score
32 records- 0196US11473438B2Grooved rotor casing system using additive manufacturing methodHONEYWELL INT INC·Filed 2019·Granted Oct 18, 2022·14 cites·16 claims
- 0295US10495108B2Variable vane devices containing rotationally-driven translating vane structures and methods for the production thereofHONEYWELL INT INC·Filed 2017·Granted Dec 3, 2019·11 cites·15 claims
- 0394US10876423B2Compressor section of gas turbine engine including hybrid shroud with casing treatment and abradable sectionHONEYWELL INT INC·Filed 2018·Granted Dec 29, 2020·7 cites·20 claims
- 0494US10527060B2Variable stator vane assemblies and variable stator vanes thereof having a locally swept leading edge and methods for minimizing endwall leakage therewithHONEYWELL INT INC·Filed 2017·Granted Jan 7, 2020·9 cites·14 claims
- 0594US10359051B2Impeller 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
- 0693US11098731B2Grooved shroud casing treatment for high pressure compressor in a turbine engineHONEYWELL INT INC·Filed 2020·Granted Aug 24, 2021·6 cites·11 claims
- 0791US10648484B2Grooved shroud casing treatment for high pressure compressor in a turbine engineHONEYWELL INT INC·Filed 2017·Granted May 12, 2020·6 cites·17 claims
- 0889US11421544B2Compressor section of gas turbine engine including hybrid shroud with casing treatment and abradable sectionHONEYWELL INT INC·Filed 2020·Granted Aug 23, 2022·2 cites·15 claims
- 0988US11015465B2Compressor section of gas turbine engine including shroud with serrated casing treatmentHONEYWELL INT INC·Filed 2019·Granted May 25, 2021·5 cites·20 claims
- 1088US10330121B2Systems and methods for axial compressor with secondary flowHONEYWELL INT INC·Filed 2015·Granted Jun 25, 2019·6 cites·9 claims
- 1186US10046424B2Rotors with stall margin and efficiency optimization and methods for improving gas turbine engine performance therewithHONEYWELL INT INC·Filed 2014·Granted Aug 14, 2018·7 cites·17 claims
- 1283US11608744B2System and method for air injection passageway integration and optimization in turbomachineryHONEYWELL INT INC·Filed 2020·Granted Mar 21, 2023·2 cites·20 claims
- 1383US11286779B2Characteristic distribution for rotor blade of booster rotorHONEYWELL INT INC·Filed 2020·Granted Mar 29, 2022·2 cites·17 claims
- 1482US10295436B2Structured light measuring apparatus and methodsHONEYWELL INT INC·Filed 2016·Granted May 21, 2019·4 cites·7 claims
- 1581US9932985B2Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereofHONEYWELL INT INC·Filed 2015·Granted Apr 3, 2018·2 cites·15 claims
- 1679US12196141B2Systems and methods with distributed bleed for gas turbine engine compressor stabilizationHONEYWELL INT INC·Filed 2023·Granted Jan 14, 2025·1 cites·19 claims
- 1778US12286896B2System and method for turbomachine with local vortex generator arrayHONEYWELL INT INC·Filed 2024·Granted Apr 29, 2025·0 cites·20 claims
- 1878US9784285B2Variable stator vane assemblies and variable stator vanes thereof having a locally swept leading edge and methods for minimizing endwall leakage therewithHONEYWELL INT INC·Filed 2014·Granted Oct 10, 2017·3 cites·15 claims
- 1977US11371354B2Characteristic distribution for rotor blade of booster rotorHONEYWELL INT INC·Filed 2020·Granted Jun 28, 2022·1 cites·18 claims
- 2069US11885234B2System and method for turbomachine with local vortex generator arrayHONEYWELL INT INC·Filed 2021·Granted Jan 30, 2024·0 cites·18 claims
- 2169US11466694B2Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereofHONEYWELL INT INC·Filed 2020·Granted Oct 11, 2022·0 cites·13 claims
- 2268US10718214B2High-pressure compressor rotor with leading edge having indent segmentHONEYWELL INT INC·Filed 2017·Granted Jul 21, 2020·1 cites·15 claims
- 2366US11015614B2Variable vane devices containing rotationally-driven translating vane structures and methods for the production thereofHONEYWELL INT INC·Filed 2019·Granted May 25, 2021·0 cites·10 claims
- 2461US2020240435A1Variable stator vane assemblies and variable stator vanes thereof having a locally swept leading edge and methods for minimizing endwall leakage therewithHONEYWELL INT INC·Filed 2019·Application pending·0 cites
- 2560US10760580B2Gas turbine engine compressors having optimized stall enhancement feature configurations and methods for the production thereofHONEYWELL INT INC·Filed 2018·Granted Sep 1, 2020·0 cites·16 claims
- 2657US2018355791A1Axi-centrifugal compressorHONEYWELL INT INC·Filed 2018·Application pending·0 cites
- 2756US2017276070A1Axi-centrifugal compressorHONEYWELL INT INC·Filed 2016·Application pending·0 cites
- 2852US11156092B2Multistage axial-centrifugal compressor systems and methods for manufactureHONEYWELL INT INC·Filed 2019·Granted Oct 26, 2021·0 cites·6 claims
- 2947US11946474B2Gas turbine engine with compressor bleed system for combustor start assistHONEYWELL INT INC·Filed 2021·Granted Apr 2, 2024·0 cites·12 claims
- 3047US2021381385A1Characteristic distribution for rotor blade of booster rotorHONEYWELL INT INC·Filed 2020·Application pending·0 cites
- 3146US2022048145A1Turbine airfoil designHONEYWELL INT INC·Filed 2020·Application pending·0 cites
- 3237US5722813ASegmented composite compressor deswirlALLIED SIGNAL INC·Filed 1996·Granted Mar 3, 1998·15 cites·17 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →