Vuillemin; Alexandre Alfred Gaston

Patent Applications and Registrations

Patent applications and USPTO patent grants for Vuillemin; Alexandre Alfred Gaston.The latest application filed is for "tail cone for a microjet rotary turbine engine".

Company Profile

0.17.19

Vuillemin; Alexandre Alfred Gaston - Moissy-Cramayle FR
Vuillemin; Alexandre Alfred Gaston - Moissy-Cramayel FR
Vuillemin; Alexandre Alfred Gaston - Marseilles FR
Vuillemin; Alexandre Alfred Gaston - Fontainebleau FR
Vuillemin; Alexandre Alfred, Gaston - Moissy-Cramayle Cedex FR
Vuillemin; Alexandre Alfred Gaston - Fontainbleau FR
Vuillemin; Alexandre Alfred Gaston - Paris FR

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Attachment pylon for a turbine engine Grant 9,938,901 - Bodard , et al. April 10, 2	2018-04-10
Tail cone for a microjet rotary turbine engine Grant 9,885,315 - Vuillemin , et al. February 6, 2	2018-02-06
Primary cowl of a turbofan comprising a rotating ring having micro-jets Grant 9,617,954 - Vuillemin , et al. April 11, 2	2017-04-11
Bypass turbojet Grant 9,611,865 - Morel , et al. April 4, 2	2017-04-04
Device for reducing the noise emitted by the jet of an aircraft propulsion engine Grant 9,422,887 - Bodard , et al. August 23, 2	2016-08-23
Method of processing acoustic waves emitted at the outlet of a turbo engine of an aircraft with a dielectric-barrier discharge device and aircraft comprising such a device Grant 9,361,876 - Vuillemin June 7, 2	2016-06-07
Tail Cone For A Microjet Rotary Turbine Engine App 20140373550 - VUILLEMIN; Alexandre Alfred Gaston ; et al.	2014-12-25
Attachment Pylon For A Turbine Engine App 20140290270 - Bodard; Guillaume ; et al.	2014-10-02
Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly Grant 8,827,199 - Aeberli , et al. September 9, 2	2014-09-09
Turbine engine with nonstreamlined impellers Grant 8,701,380 - Vuillemin April 22, 2	2014-04-22
Bypass Turbojet App 20130280046 - Morel; Cedric ; et al.	2013-10-24
Turbine Engine Having Two Unducted Propellers App 20130115083 - Vuillemin; Alexandre Alfred, Gaston	2013-05-09
Device For Reducing The Noise Emitted By The Jet Of An Aircraft Propulsion Engine App 20130055718 - Bodard; Guillaume ; et al.	2013-03-07
Method Of Processing Acoustic Waves Emitted At The Outlet Of A Turbo Engine Of An Aircraft With A Dielectric-barrier Discharge Device And Aircraft Comprising Such A Device App 20130043343 - Vuillemin; Alexandre Alfred Gaston	2013-02-21
Turboshaft Engine Supporting Pylon Covered With A Porous Material And Turboshaft Engine/pylon Assembly App 20130009002 - Aeberli; Sebastien Jean-Paul ; et al.	2013-01-10
Exhaust Nozzle For A Bypass Airplane Turbojet Having A Deployable Secondary Cover And A Retractable Central Body App 20120192543 - Aeberli; Sebastien Jean-Paul ; et al.	2012-08-02
Turbine Engine With Nonstreamlined Impellers App 20120000177 - VUILLEMIN; Alexandre Alfred Gaston	2012-01-05
Bypass turbomachine with reduction of jet noise Grant 8,037,687 - Beutin , et al. October 18, 2	2011-10-18
Variable-section flow mixer for a double-flow turbojet for a supersonic airplane Grant 7,827,802 - Dussillols , et al. November 9, 2	2010-11-09
Core exhaust mixer, having a variable area, for turbo-fan jet engines of supersonic aircraft Grant 7,810,335 - Dussillols , et al. October 12, 2	2010-10-12
Rotary motion mixer for a converging-stream nozzle of a turbomachine Grant 7,784,270 - Dussillols , et al. August 31, 2	2010-08-31
Turbomachine Nozzle Cowl Having Jet Noise Reduction Patterns App 20090084111 - AEBERLI; Sebastien Jean-Paul ; et al.	2009-04-02
Bypass Turbomachine With Reduction Of Jet Noise App 20090064658 - Beutin; Bruno Albert ; et al.	2009-03-12
Variable-section Flow Mixer For A Double-flow Turbojet For A Supersonic Airplane App 20080236167 - DUSSILLOLS; Laurent Christophe ; et al.	2008-10-02
Curved Lobe Mixer For A Converging-stream Nozzle For A Turbomachine App 20080105487 - Loheac; Pierre Philippe Marie ; et al.	2008-05-08
Rotary Motion Mixer For A Converging-stream Nozzle Of A Turbomachine App 20080105488 - DUSSILLOLS; Laurent Christophe ; et al.	2008-05-08
Core Exhaust Mixer, Having A Variable Area, For Turbo-fan Jet Engines Of Supersonic Aircraft App 20070163230 - Dussillols; Laurent ; et al.	2007-07-19

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