Inventor · disambiguated record
Alain Porte
Also filed as: PORTE ALAIN
145 granted patents·23 pending applications·3,029 citations·filing 1988–2022
99Inventor score
Top patents by PatentIndex Score
168 records- 0198US7926261B2Turbofan provided with a pre-coolerAIRBUS FRANCE·Filed 2006·Granted Apr 19, 2011·64 cites·10 claims
- 0298US5729969ADevice for bleeding off and cooling hot air in an aircraft engineAEROSPATIALE·Filed 1996·Granted Mar 24, 1998·165 cites·15 claims
- 0395US12014714B2Cellular sound insulation structure including a diaphragm provided with a tube configured to treat different acoustic frequencies, method for manufacturing such a cellular sound insulation structure, and associated toolAIRBUS OPERATIONS SAS·Filed 2021·Granted Jun 18, 2024·5 cites·7 claims
- 0495US6698691B2Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the sameAIRBUS FRANCE·Filed 2002·Granted Mar 2, 2004·82 cites·20 claims
- 0594US6536556B2Noise reduction sandwich panel, notably for aircraft turbojet engineAIRBUS FRANCE·Filed 2001·Granted Mar 25, 2003·70 cites·12 claims
- 0694US6227485B1Opening device common to two adjacent aircraft engine nacelle coversAEROSPATIALE·Filed 1998·Granted May 8, 2001·117 cites·15 claims
- 0794US6123170ANoise reducing connection assembly for aircraft turbine housingsAEROSPATIALE·Filed 1998·Granted Sep 26, 2000·137 cites·30 claims
- 0892US11945596B2Method for producing an alveolar soundproofing structure including a diaphragm, and alveolar soundproofing structure obtainedAIRBUS OPERATIONS SAS·Filed 2021·Granted Apr 2, 2024·3 cites·11 claims
- 0992US11643967B2Nacelle air intake provided with a mixed ice protection systemAIRBUS OPERATIONS SAS·Filed 2022·Granted May 9, 2023·2 cites·14 claims
- 1092US10676203B2Air input structure for an aircraft nacelleAIRBUS OPERATIONS SAS·Filed 2017·Granted Jun 9, 2020·8 cites·6 claims
- 1192US7383679B2Air intake structure for aircraft engineAIRBUS FRANCE·Filed 2005·Granted Jun 10, 2008·31 cites·20 claims
- 1292US6328258B1Air intake structure for aircraft engineAEROSPATIAL NATRA·Filed 1999·Granted Dec 11, 2001·125 cites·13 claims
- 1391US11655045B2Anterior part of the nacelle of an aircraft propulsion assembly whose air intake lip is linked to the outer panel by nestingAIRBUS OPERATIONS SAS·Filed 2020·Granted May 23, 2023·3 cites·13 claims
- 1491US9010084B2Aircraft nacelle including an optimised acoustic processing systemCHELIN FRÉDÉRIC·Filed 2010·Granted Apr 21, 2015·19 cites·20 claims
- 1591US6615950B2Sandwich acoustic panelAIRBUS FRANCE·Filed 2001·Granted Sep 9, 2003·46 cites·10 claims
- 1691US6607625B2Process for the production of an acoustively resistive layer, resistive layer thus obtained, and wall using such layerEADS AIRBUS SA·Filed 2000·Granted Aug 19, 2003·46 cites·20 claims
- 1791US6398161B1Device for fixing an aircraft propulsion system to a strut and a strut adapted to said deviceAEROSPATIALE AIRBUS·Filed 2000·Granted Jun 4, 2002·72 cites·9 claims
- 1890US11815046B2Turbofan engine comprising a system for blocking the flow path of the bypass stream comprising veilsAIRBUS OPERATIONS SAS·Filed 2022·Granted Nov 14, 2023·2 cites·10 claims
- 1990US8733501B2Method for producing an acoustic treatment panelAIRBUS OPERATIONS SAS·Filed 2012·Granted May 27, 2014·17 cites·12 claims
- 2090US8047470B2System for deicing an air inlet cowl for a turbine engineAIRBUS OPERATIONS SAS·Filed 2007·Granted Nov 1, 2011·26 cites·8 claims
- 2190US7971684B2Acoustic panelAIRBUS OPERATIONS SAS·Filed 2008·Granted Jul 5, 2011·31 cites·10 claims
- 2290US6840349B2Multi-component acoustically resistive layer for acoustical attenuation panel and panel thus obtainedAIRBUS FRANCE·Filed 2003·Granted Jan 11, 2005·48 cites·12 claims
- 2389US11952136B2Method for manufacturing an acoustic panel having a capsular skin, and acoustic panel incorporating such a skinAIRBUS OPERATIONS SAS·Filed 2021·Granted Apr 9, 2024·2 cites·12 claims
- 2489US8250852B2Dual flow turbine engine equipped with a precoolerPORTE ALAIN·Filed 2007·Granted Aug 28, 2012·25 cites·10 claims
- 2589US6772857B2Acoustically resistive layer for an acoustical attenuation panel, panel using such a layerAIRBUS FRANCE·Filed 2002·Granted Aug 10, 2004·71 cites·14 claims
- 2689US6761245B2Tubular acoustic attenuation piece for an aircraft jet engine air intakeAIRBUS FRANCE·Filed 2002·Granted Jul 13, 2004·55 cites·13 claims
- 2788US11325717B2Aircraft nacelle including a link between a conduit of an air inlet and a conduit of an engineAIRBUS OPERATIONS SAS·Filed 2017·Granted May 10, 2022·5 cites·8 claims
- 2888US8757547B2Aircraft nacelle air intake incorporating optimized ice-treatment hot air injection meansPORTE ALAIN·Filed 2010·Granted Jun 24, 2014·16 cites·9 claims
- 2988US8181900B2Acoustic coating for an aircraft incorporating a frost treatment system by joule effectCHENE GILLES·Filed 2007·Granted May 22, 2012·29 cites·13 claims
- 3087US8413922B2Acoustic processing structure particularly adapted to the air inlet of an aircraft nacellePORTE ALAIN·Filed 2008·Granted Apr 9, 2013·26 cites·18 claims
- 3187US7484592B2Sound attenuation panel comprising a resistive layer with reinforced structural componentAIRBUS FRANCE·Filed 2002·Granted Feb 3, 2009·34 cites·9 claims
- 3287US6334730B1Telescopic rod for opening a mobile cowl, in particular of an aircraft engine bayAEROSPATIALE·Filed 1998·Granted Jan 1, 2002·56 cites·7 claims
- 3386US9719422B2Process for the production of an acoustic treatment panel that integrates channels juxtaposed with an alveolar structurePORTE ALAIN·Filed 2012·Granted Aug 1, 2017·5 cites·11 claims
- 3486US7790082B2Process for the production of a panel of composite material with stiffening strips and panel thus obtainedAIRBUS FRANCE·Filed 2004·Granted Sep 7, 2010·27 cites·13 claims
- 3586US6755280B2Method for producing a panel comprising an adapted acoustically resistive layer and panel so obtainedAIRBUS FRANCE·Filed 2002·Granted Jun 29, 2004·54 cites·20 claims
- 3686US6347765B1Device for attaching an aircraft engine to a strutAEROSPATIALE AIRBUS·Filed 2000·Granted Feb 19, 2002·54 cites·15 claims
- 3786US5782077ADevice for bleeding off and cooling hot air in an aircraft engineAEROSPATIALE·Filed 1996·Granted Jul 21, 1998·90 cites·13 claims
- 3885US8851416B2Aircraft nacelle including at least one radial partition between two conductsPORTE ALAIN·Filed 2011·Granted Oct 7, 2014·9 cites·20 claims
- 3985US6443395B1Air inlet cowl for a jet engine equipped with de-icing meansAIRBUS FRANCE·Filed 2001·Granted Sep 3, 2002·53 cites·9 claims
- 4084US11027817B2Acoustic treatment panel comprising a porous acoustically resistive structure comprising connecting canalsAIRBUS OPERATIONS SAS·Filed 2018·Granted Jun 8, 2021·4 cites·9 claims
- 4184US8448901B2Aircraft nacelle including hot air discharge meansPORTE ALAIN·Filed 2008·Granted May 28, 2013·17 cites·14 claims
- 4284US5011193ADevice for the tight, dismantlable coupling of two tubes, particularly for a fuel transfer installationAEROSPATIALE·Filed 1989·Granted Apr 30, 1991·51 cites·4 claims
- 4383US9567905B2Aircraft nacelle comprising a reinforced connection between an air intake and a powerplantAIRBUS OPERATIONS SAS·Filed 2013·Granted Feb 14, 2017·9 cites·13 claims
- 4483US9352844B2Nacelle incorporating an element for connecting a lip and an acoustic attenuation panel togetherPORTE ALAIN·Filed 2010·Granted May 31, 2016·10 cites·4 claims
- 4583US6896099B2Aircraft engine pod with acoustic attenuationAIRBUS FRANCE·Filed 2002·Granted May 24, 2005·43 cites·10 claims
- 4682US6857669B2Device for connecting two tubular pieces of an aircraft turbine engineAIRBUS FRANCE·Filed 2003·Granted Feb 22, 2005·41 cites·11 claims
- 4781US6079670AHot air diffuser for a jet engine air inlet cowl with de-icing circuitAEROSPATIALE·Filed 1998·Granted Jun 27, 2000·67 cites·16 claims
- 4880US8794572B2Air intake of an aircraft nacelle that incorporates a reinforced lip with a defrost system by joule-effectPORTE ALAIN·Filed 2012·Granted Aug 5, 2014·8 cites·18 claims
- 4980US6334588B1Aircraft propulsion unit fan cowls equipped with maintaining and positioning safety elementsAERISPATIALE SOC NAT IND·Filed 1998·Granted Jan 1, 2002·68 cites·13 claims
- 5080US6131855ADevice for removing hot air for a jet engine air inlet cowl with a de-icing circuitAEROSPATIALE·Filed 1998·Granted Oct 17, 2000·62 cites·11 claims
Showing the top 50 of 168 patent records by PatentIndex Score.
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →