Inventor · disambiguated record
Michael John Layland
Also filed as: LAYLAND MICHAEL · LAYLAND MICHAEL J · LAYLAND MICHAEL JOHN
24 granted patents·2 pending applications·534 citations·filing 1989–2015
97Inventor score
Top patents by PatentIndex Score
26 records- 0196US8197191B2Inlet section of an aircraft engine nacelleBINKS ALAN·Filed 2009·Granted Jun 12, 2012·51 cites·38 claims
- 0296US7921966B2Linear acoustic linerROHR INC·Filed 2008·Granted Apr 12, 2011·55 cites·19 claims
- 0396US7923668B2Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed thereinROHR INC·Filed 2007·Granted Apr 12, 2011·85 cites·25 claims
- 0496US5083426AIntegrated engine shroud for gas turbine enginesROHR INDUSTRIES INC·Filed 1989·Granted Jan 28, 1992·84 cites·12 claims
- 0595US7469862B2Aircraft engine nacelle inlet having access opening for electrical ice protection systemGOODRICH CORP·Filed 2005·Granted Dec 30, 2008·34 cites·14 claims
- 0694US7798285B2Acoustic barrel for aircraft engine nacelle including crack and delamination stoppersROHR INC·Filed 2008·Granted Sep 21, 2010·40 cites·13 claims
- 0793US9403599B2Inlet section of an aircraft engine nacelleBINKS ALAN·Filed 2012·Granted Aug 2, 2016·19 cites·13 claims
- 0891US7513458B2Aircraft engine nacelle inlet having electrical ice protection systemROHR INC·Filed 2005·Granted Apr 7, 2009·29 cites·30 claims
- 0990US8267642B2Inlet section of an aircraft engine nacelleBINKS ALAN·Filed 2011·Granted Sep 18, 2012·13 cites·20 claims
- 1089US8402765B2Translating variable area fan nozzle providing an upstream bypass flow exitAMKRAUT DANIEL M·Filed 2009·Granted Mar 26, 2013·24 cites·5 claims
- 1186US9016042B2Reinforcement members for aircraft propulsion system components configured to address delamination of the inner fixed structureCHIOU SONG·Filed 2012·Granted Apr 28, 2015·10 cites·11 claims
- 1285US8025499B2Multi-segment tool and method for composite formationROHR INC·Filed 2008·Granted Sep 27, 2011·7 cites·16 claims
- 1384US8196704B2Linear acoustic linerCHIOU SONG·Filed 2011·Granted Jun 12, 2012·11 cites·12 claims
- 1483US9567089B2Hybrid hinge and latch beamROHR INC·Filed 2013·Granted Feb 14, 2017·10 cites·6 claims
- 1581US7631838B2Aircraft engine nacelle inlet having access opening for electrical ice protection systemROHR INC·Filed 2008·Granted Dec 15, 2009·12 cites·4 claims
- 1680US7837150B2Ice protection system for a multi-segment aircraft componentROHR INC·Filed 2007·Granted Nov 23, 2010·22 cites·21 claims
- 1776US9233757B2NacelleJAMES NORMAN JOHN·Filed 2011·Granted Jan 12, 2016·6 cites·10 claims
- 1875US9759087B2Translating variable area fan nozzle providing an upstream bypass flow exitROHR INC·Filed 2013·Granted Sep 12, 2017·5 cites·14 claims
- 1975US8394315B2Multi-segment tool and method for composite formationHUBERT CLAUDE MARC·Filed 2011·Granted Mar 12, 2013·3 cites·19 claims
- 2071US7681838B2Aircraft engine nacelle inlet having access opening for electrical ice protection systemROHR INC·Filed 2008·Granted Mar 23, 2010·7 cites·14 claims
- 2168US9897007B2Thrust reverser-integrated track beam and inner fixed structureROHR INC·Filed 2013·Granted Feb 20, 2018·3 cites·22 claims
- 2267US9551298B2Variable area fan nozzle with one or more integrated blocker doorsROHR INC·Filed 2013·Granted Jan 24, 2017·3 cites·18 claims
- 2364USRE46321EMulti-segment tool and method for composite formationROHR INC·Filed 2015·Granted Feb 28, 2017·1 cites·19 claims
- 2447US2013129483A1Crack and delamination stoppers for aircraft propulsion system componentsROHR INC·Filed 2012·Application pending·0 cites
- 2547US2016083102A1NacelleROHR INC·Filed 2015·Application pending·0 cites
- 2644US10184398B2Acoustic structural panel with slanted coreROHR INC·Filed 2013·Granted Jan 22, 2019·0 cites·15 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →