PECHBUSQUE
France
36
2020-06-18
The entities that hold a legal rights for patent applications filed by inventor LAFONT Laurent:
Laurent LAFONT from PECHBUSQUE, FR has applied for patents for these inventions. The list has both pending applications and granted patents:
Propulsion assembly for an aircraft, comprising a load support
#2 | 2020-05-14Assembly for aircraft comprising a primary structure of an attachment pylon attached to a wing box using a bolted connection
#3 | 2019-08-01Assembly for aircraft comprising a primary mounting pylon structure fixed to an airfoil box using a bolted link
#4 | 2017-08-24Aircraft engine assembly, comprising an engine attachment device equipped with structural movable cowls connected to the central box
#5 | 2012-07-12Aircraft engine mounting structure, assembly comprising this structure and associated aircraft
#6 | 2012-07-05Aircraft assembly including an element for mounting an engine and associated aircraft
#7 | 2012-05-17Blade-retaining device for turbomachine propeller
#8 | 2012-05-10Assembly for an aircraft comprising a turbomachine attachment strut of which the means for attachment to the wing are arranged in a T shape
#9 | 2012-05-10Engine assembly for an aircraft the engine attachment strut of which includes a structural case forming an internal radial delimitation of the secondary flow
#10 | 2012-04-05Take-up device for thrust forces with connecting rods for aircraft engine attachment pylon, integrating three aligned ball joints
#11 | 2012-04-05Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins
#12 | 2012-03-22Propeller for an aircraft turbine engine comprising a vane retaining ring mounted about the hub
#13 | 2012-01-12Rear part of an aircraft including an engine support structure assembled so as to oscillate on the fuselage
#14 | 2011-09-29Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod
#15 | 2011-09-22Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rod
#16 | 2011-09-22Rear part of an aircraft comprising a structure for supporting engines, connected to the fuselage by at least one blocking element under compression loading
#17 | 2011-09-01Structural rod incorporating a vibration filtration mode
#18 | 2011-08-18Engine assembly for an aircraft comprising attachments for engines offset below on the fan frame
#19 | 2010-08-26Blade retaining device for turbo machine propeller
#20 | 2010-08-26Blade for turbomachine receiving part, comprising an airfoil part including a mechanical fuse
#21 | 2010-08-19Vane for aircraft turbine engine receiver, provided with two hollow cores lodged in one another
#22 | 2010-08-05Assembly for an aircraft including a wing element and a suspension pylon
#23 | 2010-07-08Engine assembly for aircraft with sliding nacelle
#24 | 2008-12-25Turbojet engine mounting structure for aircraft
#25 | 2008-12-04System for connecting a crossbar to an aircraft engine pylon
#26 | 2008-11-06Engine assembly for aircraft
#27 | 2008-11-06Strut for locking the engine of an aircraft
#28 | 2008-10-02Engine mounting structure interposed between an aircraft wing system and said engine
#29 | 2008-09-18Mounting assembly for securing an engine to an aircraft wing
#30 | 2008-09-18Method for mounting an aircraft engine on a rigid structure of a strut for locking the engine
#31 | 2008-09-11Monolithic Framework Engine Mounting Structure
#32 | 2008-09-11Assembly for aircraft comprising a wing system element as well as an attachment mast
#33 | 2008-08-21Engine mounting structure for an aircraft
#34 | 2008-08-21Engine mounting structure for an aircraft
#35 | 2007-03-29Engine assembly for aircraft
#36 | 2007-03-29Engine suspension pylon for aircraft
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