Inventor · disambiguated record
Nick Nolcheff
Also filed as: NOLCHEFF NICK · NOLCHEFF NICK A
44 granted patents·12 pending applications·743 citations·filing 1992–2025
98Inventor score
Top patents by PatentIndex Score
56 records- 0194US11378093B2Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distributionHONEYWELL INT INC·Filed 2020·Granted Jul 5, 2022·4 cites·18 claims
- 0294US11149583B2Gas turbine engine particulate ingestion and accumulation sensor system and methodHONEYWELL INT INC·Filed 2020·Granted Oct 19, 2021·5 cites·11 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
- 0494US5607284ABaffled passage casing treatment for compressor bladesUNITED TECHNOLOGIES CORP·Filed 1994·Granted Mar 4, 1997·112 cites·3 claims
- 0594US5282718ACase treatment for compressor bladesUNITED TECHNOLOGIES CORP·Filed 1992·Granted Feb 1, 1994·111 cites·4 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
- 0793US7984614B2Plasma flow controlled diffuser systemHONEYWELL INT INC·Filed 2008·Granted Jul 26, 2011·31 cites·20 claims
- 0892US10208628B2Turbine engine designs for improved fine particle separation efficiencyHONEYWELL INT INC·Filed 2016·Granted Feb 19, 2019·10 cites·18 claims
- 0992US7547186B2Nonlinearly stacked low noise turbofan statorHONEYWELL INT INC·Filed 2005·Granted Jun 16, 2009·56 cites·15 claims
- 1091US10859094B2Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distributionHONEYWELL INT INC·Filed 2018·Granted Dec 8, 2020·5 cites·19 claims
- 1191US10648484B2Grooved shroud casing treatment for high pressure compressor in a turbine engineHONEYWELL INT INC·Filed 2017·Granted May 12, 2020·6 cites·17 claims
- 1291US5474417ACast casing treatment for compressor bladesUNITED TECHNOLOGIES CORP·Filed 1994·Granted Dec 12, 1995·133 cites·5 claims
- 1389US11421544B2Compressor 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
- 1489US9631554B2Electrostatic charge control inlet particle separator systemHONEYWELL INT INC·Filed 2014·Granted Apr 25, 2017·11 cites·13 claims
- 1588US11015465B2Compressor section of gas turbine engine including shroud with serrated casing treatmentHONEYWELL INT INC·Filed 2019·Granted May 25, 2021·5 cites·20 claims
- 1687US10670040B2Core-protecting fan modules and turbofan engines containing the sameHONEYWELL INT INC·Filed 2017·Granted Jun 2, 2020·5 cites·18 claims
- 1787US10221720B2Structural frame integrated with variable-vectoring flow control for use in turbine systemsHONEYWELL INT INC·Filed 2014·Granted Mar 5, 2019·8 cites·10 claims
- 1886US7942625B2Compressor and compressor housingHONEYWELL INT INC·Filed 2007·Granted May 17, 2011·26 cites·9 claims
- 1986US5586859AFlow aligned plenum endwall treatment for compressor bladesUNITED TECHNOLOGIES CORP·Filed 1995·Granted Dec 24, 1996·63 cites·4 claims
- 2084US10876409B2Mistuned rotors and methods for manufactureHONEYWELL INT INC·Filed 2018·Granted Dec 29, 2020·2 cites·19 claims
- 2183US11286779B2Characteristic distribution for rotor blade of booster rotorHONEYWELL INT INC·Filed 2020·Granted Mar 29, 2022·2 cites·17 claims
- 2283US11181120B2Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distributionHONEYWELL INT INC·Filed 2018·Granted Nov 23, 2021·3 cites·20 claims
- 2383US8006497B2Diffusers, diffusion systems, and methods for controlling airflow through diffusion systemsHONEYWELL INT INC·Filed 2008·Granted Aug 30, 2011·28 cites·19 claims
- 2481US11280199B2Throat distribution for a rotor and rotor blade having camber and location of local maximum thickness distributionHONEYWELL INT INC·Filed 2018·Granted Mar 22, 2022·3 cites·20 claims
- 2581US9932985B2Gas 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
- 2679US12196141B2Systems and methods with distributed bleed for gas turbine engine compressor stabilizationHONEYWELL INT INC·Filed 2023·Granted Jan 14, 2025·1 cites·19 claims
- 2779US11333171B2High performance wedge diffusers for compression systemsHONEYWELL INT INC·Filed 2020·Granted May 17, 2022·1 cites·20 claims
- 2879US9638103B2Plasma flow control inlet particle separator systemHONEYWELL INT INC·Filed 2013·Granted May 2, 2017·6 cites·16 claims
- 2978US8122724B2Compressor including an aerodynamically variable diffuserSLOVISKY JOHN A·Filed 2004·Granted Feb 28, 2012·33 cites·2 claims
- 3077US11371354B2Characteristic distribution for rotor blade of booster rotorHONEYWELL INT INC·Filed 2020·Granted Jun 28, 2022·1 cites·18 claims
- 3177US7189059B2Compressor including an enhanced vaned shroudHONEYWELL INT INC·Filed 2004·Granted Mar 13, 2007·36 cites·26 claims
- 3275US8438854B2Pre-diffuser for centrifugal compressorNOLCHEFF NICK A·Filed 2008·Granted May 14, 2013·8 cites·19 claims
- 3375US8210794B2Axial-centrifugal compressor with ported shroudNOLCHEFF NICK A·Filed 2008·Granted Jul 3, 2012·8 cites·20 claims
- 3473US10294965B2Compression system for a turbine engineHONEYWELL INT INC·Filed 2016·Granted May 21, 2019·2 cites·20 claims
- 3569US11466694B2Gas 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
- 3666US12504024B1Diffusers, gas turbine engines comprising the same, and methods for operation thereofHONEYWELL INT INC·Filed 2025·Granted Dec 23, 2025·0 cites·20 claims
- 3763US2020018180A1Gas turbine engine particulate ingestion and accumulation sensor system and methodHONEYWELL INT INC·Filed 2019·Application pending·0 cites
- 3860US10760580B2Gas 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
- 3959US10907503B2Compressors with integrated secondary air flow systemsHONEYWELL INT INC·Filed 2018·Granted Feb 2, 2021·0 cites·19 claims
- 4059US2019078466A1Structural frame integrated with variable-vectoring flow control for use in turbine systemsHONEYWELL INT INC·Filed 2018·Application pending·0 cites
- 4157US2018355791A1Axi-centrifugal compressorHONEYWELL INT INC·Filed 2018·Application pending·0 cites
- 4256US2017276070A1Axi-centrifugal compressorHONEYWELL INT INC·Filed 2016·Application pending·0 cites
- 4355US2018298778A1Gas turbine engine particulate ingestion and accumulation sensor system and methodHONEYWELL INT INC·Filed 2017·Application pending·0 cites
- 4454US10072522B2Compressors with integrated secondary air flow systemsNOLCHEFF NICK·Filed 2011·Granted Sep 11, 2018·1 cites·16 claims
- 4553US10871170B2High performance wedge diffusers for compression systemsHONEYWELL INT INC·Filed 2018·Granted Dec 22, 2020·0 cites·20 claims
- 4652US11156092B2Multistage axial-centrifugal compressor systems and methods for manufactureHONEYWELL INT INC·Filed 2019·Granted Oct 26, 2021·0 cites·6 claims
- 4750US2017058782A1Plasma actuated cascade flow vectoringHONEYWELL INT INC·Filed 2016·Application pending·0 cites
- 4847US11946474B2Gas turbine engine with compressor bleed system for combustor start assistHONEYWELL INT INC·Filed 2021·Granted Apr 2, 2024·0 cites·12 claims
- 4947US10989219B2Diffuser assemblies for compression systemsHONEYWELL INT INC·Filed 2019·Granted Apr 27, 2021·0 cites·13 claims
- 5047US2014321987A1Plasma actuated cascade flow vectoringHONEYWELL INT INC·Filed 2013·Application pending·0 cites
Showing the top 50 of 56 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →