Inventor · disambiguated record
Wesley K. Lord
Also filed as: LORD WESLEY K · LORD WESLEY KENNETH
78 granted patents·12 pending applications·1,332 citations·filing 1993–2023
99Inventor score
Top patents by PatentIndex Score
90 records- 0199US10060357B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 28, 2018·23 cites·27 claims
- 0298US10371061B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2016·Granted Aug 6, 2019·11 cites·33 claims
- 0397US10655538B2Geared gas turbine engine with reduced fan noiseUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 19, 2020·15 cites·30 claims
- 0497US10301971B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 28, 2019·13 cites·30 claims
- 0597US9932933B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2013·Granted Apr 3, 2018·33 cites·19 claims
- 0697US9850819B2Intercooled cooling air with dual pass heat exchangerUNITED TECHNOLOGIES CORP·Filed 2015·Granted Dec 26, 2017·14 cites·10 claims
- 0797US6554564B1Reduced noise fan exit guide vane configuration for turbofan enginesUNITED TECHNOLOGIES CORP·Filed 2001·Granted Apr 29, 2003·119 cites·6 claims
- 0896US9920653B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2012·Granted Mar 20, 2018·17 cites·20 claims
- 0996US9611034B1Wide fuselage aircraft with increased boundary layer ingestionUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 4, 2017·15 cites·18 claims
- 1096US7434384B2Fluid 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
- 1196US6379110B1Passively driven acoustic jet controlling boundary layersUNITED TECHNOLOGIES CORP·Filed 1999·Granted Apr 30, 2002·116 cites·26 claims
- 1295US11149650B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2018·Granted Oct 19, 2021·7 cites·30 claims
- 1395US10107191B2Geared gas turbine engine with reduced fan noiseUNITED TECHNOLOGIES CORP·Filed 2015·Granted Oct 23, 2018·36 cites·30 claims
- 1495US8844265B2Turbine section of high bypass turbofanADAMS PAUL R·Filed 2012·Granted Sep 30, 2014·28 cites·20 claims
- 1595US5638675ADouble lobed mixer with major and minor lobesUNITED TECHNOLOGIES CORP·Filed 1995·Granted Jun 17, 1997·116 cites·3 claims
- 1695US5440875AFixed geometry mixer/ejector suppression system for turbofan aircraft enginesUNITED TECHNOLOGIES CORP·Filed 1994·Granted Aug 15, 1995·114 cites·11 claims
- 1794US9932905B2Bypass duct heat exchanger with controlled fanUNITED TECHNOLOGIES CORP·Filed 2015·Granted Apr 3, 2018·8 cites·12 claims
- 1894US7607287B2Airfoil acoustic impedance controlUNITED TECHNOLOGIES CORP·Filed 2007·Granted Oct 27, 2009·46 cites·18 claims
- 1993US9297270B2Gas turbine engine driving multiple fansSUCIU GABRIEL L·Filed 2012·Granted Mar 29, 2016·15 cites·19 claims
- 2093US8708274B2Transverse mounted gas turbine engineLORD WESLEY K·Filed 2011·Granted Apr 29, 2014·22 cites·18 claims
- 2192US11480108B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2021·Granted Oct 25, 2022·2 cites·30 claims
- 2292US10267263B2Exhaust duct for turbine forward of fanUNITED TECHNOLOGIES CORP·Filed 2016·Granted Apr 23, 2019·9 cites·18 claims
- 2392US8850793B2Turbine section of high bypass turbofanUNITED TECHNOLOGIES CORP·Filed 2013·Granted Oct 7, 2014·11 cites·18 claims
- 2491US8789354B2Gas turbine engine with separate core and propulsion unitSUCIU GABRIEL L·Filed 2012·Granted Jul 29, 2014·14 cites·20 claims
- 2590US11242805B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2018·Granted Feb 8, 2022·5 cites·31 claims
- 2689US11118507B2Geared gas turbine engine with reduced fan noiseRAYTHEON TECH CORP·Filed 2020·Granted Sep 14, 2021·2 cites·30 claims
- 2789US10723470B2Aft fan counter-rotating turbine engineUNITED TECHNOLOGIES CORP·Filed 2017·Granted Jul 28, 2020·4 cites·17 claims
- 2889US10711631B2Turbine engine with guide vanes forward of its fan bladesUNITED TECHNOLOGIES CORP·Filed 2015·Granted Jul 14, 2020·5 cites·14 claims
- 2987US9010085B2Turbine section of high bypass turbofanADAMS PAUL R·Filed 2012·Granted Apr 21, 2015·8 cites·23 claims
- 3087US8844553B2Passive boundary layer bleed system for nacelle inlet airflow controlZYSMAN STEVEN H·Filed 2006·Granted Sep 30, 2014·16 cites·22 claims
- 3186US11286811B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2019·Granted Mar 29, 2022·2 cites·26 claims
- 3286US6203269B1Centrifugal air flow controlUNITED TECHNOLOGIES CORP·Filed 1999·Granted Mar 20, 2001·95 cites·16 claims
- 3385US6487848B2Gas turbine engine jet noise suppressorUNITED TECHNOLOGIES CORP·Filed 1998·Granted Dec 3, 2002·75 cites·22 claims
- 3484US11346289B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2020·Granted May 31, 2022·2 cites·14 claims
- 3584US10724541B2Nacelle short inletUNITED TECHNOLOGIES CORP·Filed 2016·Granted Jul 28, 2020·5 cites·17 claims
- 3682US11486311B2Turbine section of high bypass turbofanRAYTHEON TECH CORP·Filed 2021·Granted Nov 1, 2022·1 cites·30 claims
- 3782US7942632B2Variable-shape variable-stagger inlet guide vane flapUNITED TECHNOLOGIES CORP·Filed 2007·Granted May 17, 2011·20 cites·15 claims
- 3881US5775095AMethod of noise suppression for a turbine engineUNITED TECHNOLOGIES CORP·Filed 1996·Granted Jul 7, 1998·39 cites·2 claims
- 3980US11015550B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeUNITED TECHNOLOGIES CORP·Filed 2018·Granted May 25, 2021·2 cites·18 claims
- 4079US7114323B2Jet exhaust noise reduction system and methodUNITED TECHNOLOGIES CORP·Filed 2004·Granted Oct 3, 2006·32 cites·26 claims
- 4177US10421553B2Pusher fan engine with in wing configurationUNITED TECHNOLOGIES CORP·Filed 2015·Granted Sep 24, 2019·3 cites·18 claims
- 4277US10196930B2System and method for controlling an environmental condition of an engine electronic componentUNITED TECHNOLOGIES CORP·Filed 2015·Granted Feb 5, 2019·2 cites·20 claims
- 4376US10563585B2Heat exchanger for gas turbine engineUNITED TECHNOLOGIES CORP·Filed 2016·Granted Feb 18, 2020·3 cites·27 claims
- 4476US10302014B2Modifying a gas turbine engine to use a high pressure compressor as a low pressure compressorUNITED TECHNOLOGIES CORP·Filed 2015·Granted May 28, 2019·2 cites·4 claims
- 4575US7018172B2Airfoil surface impedance modification for noise reduction in turbofan enginesUNITED TECHNOLOGIES CORP·Filed 2003·Granted Mar 28, 2006·31 cites·21 claims
- 4674US10633090B2Cross flow fan with exit guide vanesUNITED TECHNOLOGIES CORP·Filed 2016·Granted Apr 28, 2020·2 cites·18 claims
- 4773US11614036B2Turbine section of gas turbine engineRAYTHEON TECH CORP·Filed 2021·Granted Mar 28, 2023·0 cites·30 claims
- 4872US11781447B2Low pressure ratio fan engine having a dimensional relationship between inlet and fan sizeRAYTHEON TECH CORP·Filed 2021·Granted Oct 10, 2023·0 cites·30 claims
- 4972US10830129B2Transverse-mounted power turbine drive systemUNITED TECHNOLOGIES CORP·Filed 2014·Granted Nov 10, 2020·3 cites·19 claims
- 5071US11512631B2Geared gas turbine engine with reduced fan noiseRAYTHEON TECH CORP·Filed 2021·Granted Nov 29, 2022·0 cites·30 claims
Showing the top 50 of 90 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →