Patents

 

As of 2014, Michel Aguilar filed 10 patents on the Xplorair and the thermoreactor: FR application 2906222, Aguilar, Michel, “Vehicle e.g. helicopter, for transporting passengers, has turbine generating air stream on front wing upper surface, and rear wing with upper surface on which flue gas stream is applied to produce air lift force to allow takeoff and landing”, published 2008-03-28, assigned to Aguilar, Michel.

FR application 2910056, Aguilar, Michel, “Rotary wing-less vertical take-off and landing vehicle for transporting passengers by air, has rear wing whose variable incidence is set to generate lift force in take-off mode, and added to forces developed on front wings in cruise mode”, published 2008-06-20, assigned to Aguilar, Michel.

EP patent 2066564, Aguilar, Michel, “Vertical take-off and landing vehicle which does not have a rotary wing”, issued 2010-09-15, assigned to Aguilar, Michel.

FR application 2941496, Aguilar, Michel, “Turbomachine i.e. thermoreactor, has air-fuel injector for injecting pressurized air-fuel mixture into combustion chamber, where injected air-fuel mixture realizes constant volume combustion and combustion gas release”, published 2010-07-30, assigned to Aguilar, Michel.

WO application 2012113523, Aguilar, Michel, “Jet engine, in particular a jet engine for an aircraft”, published 2012-08-30, assigned to Aguilar, Michel.

FR application 2960259, Aguilar, Michel, “Turbocharger for use in e.g. turbojet engine of aircraft, has combustion chamber supplied with compressed air by opening that allows introduction of air in chamber, and compressor whose air outlets are opened in inner volume of reservoir”, published 2011-11-25, assigned to EADS EUROP AERONAUTIC.

 

DEFENCE

FR application 2983906, Aguilar, Michel, “Method for thermal ignition of a pulsed combustion engine, and thermoreactor with thermal ignition”, published 2013-06-14, assigned to Aguilar, Michel.

WO application 2012113523, Aguilar, Michel, “Jet engine, in particular for an aircraft”, published 2012-08-30, assigned to Aguilar, Michel.

FR application 2971553, Aguilar, Michel, “Method for reducing noise of propulsion jet reactor of aircraft, involves ejecting shear flows at trailing edge of nacelles of reactor with ejection velocity in range between velocities of flows at inner and outer sides of nacelles”, published 2012-08-17, assigned to EADS EUROP AERONAUTIC DEFENCE FR application 2991721, Aguilar, Michel, “Method and thermal reactor for single-valve propulsion with multiple injections and combustions per rotation cycle”, published 201312-13, assigned to Aguilar, Michel.