AP

Alain Porte

Airbus Operations Sas: 89 patents #2 of 2,811Top 1%
AF Airbus France: 28 patents #1 of 526Top 1%
AI Aerospatiale Societe Nationale Industrielle: 19 patents #1 of 693Top 1%
AA Aerospatiale Airbus: 3 patents #1 of 8Top 15%
A( Airbus (S.A.S.): 3 patents #62 of 838Top 8%
SA Societe Nationale Industrielle Et Aerospatiale: 2 patents #34 of 400Top 9%
ES Eads Airbus Sa: 1 patents #1 of 19Top 6%
AA Aerospatiale Matra Airbus: 1 patents #2 of 21Top 10%
📍 Colomiers, FR: #1 of 241 inventorsTop 1%
Overall (All Time): #6,662 of 4,157,543Top 1%
145
Patents All Time

Issued Patents All Time

Showing 76–100 of 145 patents

Patent #TitleCo-InventorsDate
8439298 Device for shrouding an aircraft nacelle Robert Andre, Matthieu Fargues 2013-05-14
8425283 Ventilating air intake arrangement Damien Prat 2013-04-23
8413922 Acoustic processing structure particularly adapted to the air inlet of an aircraft nacelle Jacques Lalane, Fabrice Gantie, Jacques Barillot-Creuzet 2013-04-09
8398016 Air intake arrangement for an aircraft Emeric Chancerelle, Franck Alvarez, Damien Prat 2013-03-19
8366039 Fairing for a pylon via which a turbine engine is suspended from a wing of an aircraft 2013-02-05
8308110 System for defrosting the leading edge sheath of an air inlet hood for a turboengine 2012-11-13
8250852 Dual flow turbine engine equipped with a precooler Damien Prat 2012-08-28
8181900 Acoustic coating for an aircraft incorporating a frost treatment system by joule effect Gilles Chene, Fabrice Gantie 2012-05-22
8172037 Coating for acoustic treatment that integrates the function of hot-air treatment of frost Jacques Lalane 2012-05-08
8141337 Dual flow turbine engine equipped with a precooler Damien Prat 2012-03-27
8142144 Turbine engine for aircraft Frédéric Chelin, David Lambert 2012-03-27
8096105 Turbojet engine with attenuated jet noise 2012-01-17
8047470 System for deicing an air inlet cowl for a turbine engine 2011-11-01
7971684 Acoustic panel Fabrice Gantie, Bernard Duprieu, Valerie Frustie, Thomas Gilles, Jacques Lalane 2011-07-05
7931235 System for deicing the leading edge of a nose inlet cowl turbine engine Marie-Luce Zanarelli 2011-04-26
7926261 Turbofan provided with a pre-cooler 2011-04-19
7790082 Process for the production of a panel of composite material with stiffening strips and panel thus obtained Michel Buge, Eric Rambaud, Bruno Legeay 2010-09-07
7757719 Aircraft conduit Marie Jazet 2010-07-20
7621371 Method for attenuating the noise of a turbofan 2009-11-24
7506838 Air intake structure for aircraft engine 2009-03-24
7484592 Sound attenuation panel comprising a resistive layer with reinforced structural component Jacques Lalane 2009-02-03
7383679 Air intake structure for aircraft engine Robert Andre 2008-06-10
7334393 Aircraft engine in which there is a small clearance separating the fan cowls and the thrust inverter cowls 2008-02-26
7257894 Process for making a panel with a protected acoustic damping layer Michel Buge, Jean-Marc Poignonec 2007-08-21
7204458 Closing system interposed between two elements José Manuel Martin-Oquina, Philippe Fourest 2007-04-17