Inventor · disambiguated record
Steven H. Zysman
Also filed as: ZYSMAN STEVEN H · ZYSMAN STEVEN HENRY
37 granted patents·6 pending applications·777 citations·filing 1994–2024
97Inventor score
Top patents by PatentIndex Score
43 records- 0196US7434384B2Fluid mixer with an integral fluid capture ducts forming auxiliary secondary chutes at the discharge end of said ductsUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 14, 2008·103 cites·8 claims
- 0295US5638675ADouble lobed mixer with major and minor lobesUNITED TECHNOLOGIES CORP·Filed 1995·Granted Jun 17, 1997·116 cites·3 claims
- 0395US5440875AFixed geometry mixer/ejector suppression system for turbofan aircraft enginesUNITED TECHNOLOGIES CORP·Filed 1994·Granted Aug 15, 1995·114 cites·11 claims
- 0494US9506353B2Lightweight shrouded fan bladeUNITED TECHNOLOGIES CORP·Filed 2012·Granted Nov 29, 2016·13 cites·20 claims
- 0592US9108737B2Nacelle scoop inletZYSMAN STEVEN H·Filed 2012·Granted Aug 18, 2015·16 cites·13 claims
- 0690US11549434B2Engine bleed air ducting into heat exchangerRAYTHEON TECH CORP·Filed 2021·Granted Jan 10, 2023·4 cites·20 claims
- 0789US12109793B2Composite skins having variable hole sizes and shapes formed using photomachiningUNITED TECHNOLOGIES CORP·Filed 2019·Granted Oct 8, 2024·2 cites·14 claims
- 0887US11236701B2Convergent divergent exit nozzle for a gas turbine engineRAYTHEON TECH CORP·Filed 2018·Granted Feb 1, 2022·3 cites·8 claims
- 0987US10487744B2Fence for duct tone mitigationUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 26, 2019·8 cites·16 claims
- 1087US8844553B2Passive boundary layer bleed system for nacelle inlet airflow controlZYSMAN STEVEN H·Filed 2006·Granted Sep 30, 2014·16 cites·22 claims
- 1187US8490382B2Modulating flow through gas turbine engine cooling systemZYSMAN STEVEN H·Filed 2006·Granted Jul 23, 2013·23 cites·21 claims
- 1286US11078837B2Engine bleed air ducting into heat exchangerUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 3, 2021·5 cites·1 claims
- 1385US6487848B2Gas turbine engine jet noise suppressorUNITED TECHNOLOGIES CORP·Filed 1998·Granted Dec 3, 2002·75 cites·22 claims
- 1483US6106229AHeat exchanger system for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 1997·Granted Aug 22, 2000·90 cites·21 claims
- 1583US6058696AInlet and outlet module for a heat exchanger for a flowpath for working medium gasesUNITED TECHNOLOGIES CORP·Filed 1997·Granted May 9, 2000·58 cites·9 claims
- 1683US2024416640A1Composite skins having variable hole sizes and shapes formed using photomachiningRTX CORP·Filed 2024·Application pending·0 cites
- 1782US10371092B2Convergent divergent exit nozzle for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2015·Granted Aug 6, 2019·3 cites·13 claims
- 1881US5775095AMethod of noise suppression for a turbine engineUNITED TECHNOLOGIES CORP·Filed 1996·Granted Jul 7, 1998·39 cites·2 claims
- 1980US6565313B2Bleed deflector for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2001·Granted May 20, 2003·39 cites·14 claims
- 2079US10557416B2Flow modulating airfoil apparatusUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 11, 2020·2 cites·20 claims
- 2173US11046445B2NacelleUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jun 29, 2021·2 cites·18 claims
- 2273US7658060B2Lubricant cooling exchanger dual intake ductUNITED TECHNOLOGIES CORP·Filed 2006·Granted Feb 9, 2010·14 cites·10 claims
- 2372US7455498B2Slotted bleed deflector for a gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2006·Granted Nov 25, 2008·12 cites·20 claims
- 2470US8839805B2Passive boundary layer bleed system for nacelle inlet airflow controlZYSMAN STEVEN H·Filed 2009·Granted Sep 23, 2014·12 cites·25 claims
- 2567US9644535B2Passive boundary layer bleed system for nacelle inlet airflow controlUNITED TECHNOLOGIES CORP·Filed 2014·Granted May 9, 2017·2 cites·18 claims
- 2666US11408369B2NacelleRAYTHEON TECH CORP·Filed 2020·Granted Aug 9, 2022·0 cites·4 claims
- 2765US11548652B2NacelleRAYTHEON TECH CORP·Filed 2021·Granted Jan 10, 2023·0 cites·4 claims
- 2865US10060390B2Bypass duct with angled drag linksZYSMAN STEVEN H·Filed 2012·Granted Aug 28, 2018·2 cites·22 claims
- 2964US9644537B2Free stream intake with particle separator for reverse core engineUNITED TECHNOLOGIES CORP·Filed 2013·Granted May 9, 2017·3 cites·11 claims
- 3062US10479519B2Nacelle short inlet for fan blade removalUNITED TECHNOLOGIES CORP·Filed 2016·Granted Nov 19, 2019·1 cites·19 claims
- 3160US12264623B1System for electric machine associated with gas turbine engineHONEYWELL INT INC·Filed 2024·Granted Apr 1, 2025·0 cites·19 claims
- 3256US10730635B1Engine wingUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 4, 2020·0 cites·16 claims
- 3353US11402304B2Environmental sampling system and methodUNITED TECHNOLOGIES CORP·Filed 2019·Granted Aug 2, 2022·0 cites·14 claims
- 3451US10767596B2NacelleUNITED TECHNOLOGIES CORP·Filed 2017·Granted Sep 8, 2020·0 cites·19 claims
- 3550US11585294B2High bypass ratio engine bypass duct nozzle with controlled nozzle areaRAYTHEON TECH CORP·Filed 2020·Granted Feb 21, 2023·0 cites·16 claims
- 3647US10570852B2Moveable exhaust plug linerUNITED TECHNOLOGIES CORP·Filed 2017·Granted Feb 25, 2020·0 cites·20 claims
- 3747US10450898B2Track fairing assembly for a turbine engine nacelleUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 22, 2019·0 cites·16 claims
- 3845US10934938B2Boundary layer cooling air for embedded engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Mar 2, 2021·0 cites·4 claims
- 3945US2020024982A1Boundary layer ingesting fanUNITED TECHNOLOGIES CORP·Filed 2018·Application pending·0 cites
- 4041US2017175626A1Gas turbine engine with minimized inlet distortionUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 4140US2016153363A1Liquid separating air inletsUNITED TECHNOLOGIES CORP·Filed 2015·Application pending·0 cites
- 4239US2009133376A1Combined gearbox breather and drain mast for jet aircraft engineZYSMAN STEVEN H·Filed 2007·Application pending·0 cites
- 4335US2018355821A1Moveable exhaust plugUNITED TECHNOLOGIES CORP·Filed 2017·Application pending·0 cites
Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →