Assignee
LAFONT LAURENT
FR·11 granted patents·51 citations·filing 2006–2011
Top patents by PatentIndex Score
11 records- 0191US8845292B2Blade-retaining device for turbomachine propellerLAFONT LAURENT·Filed 2010·Granted Sep 30, 2014·11 cites·10 claims
- 0285US8613404B2Take-up device for thrust forces with connecting rods for aircraft engine attachment pylon, integrating three aligned ball jointsLAFONT LAURENT·Filed 2011·Granted Dec 24, 2013·6 cites·14 claims
- 0384US8496438B2Blade retaining device for turbo machine propellerLAFONT LAURENT·Filed 2010·Granted Jul 30, 2013·9 cites·8 claims
- 0466US8646725B2Engine assembly for an aircraft the engine attachment strut of which includes a structural case forming an internal radial delimitation of the secondary flowLAFONT LAURENT·Filed 2010·Granted Feb 11, 2014·4 cites·12 claims
- 0566US8613405B2Assembly for an aircraft comprising a turbomachine attachment strut of which the means for attachment to the wing are arranged in a T shapeLAFONT LAURENT·Filed 2010·Granted Dec 24, 2013·4 cites·9 claims
- 0662US8480025B2Rear part of an aircraft including an engine support structure assembled so as to oscillate on the fuselageLAFONT LAURENT·Filed 2010·Granted Jul 9, 2013·4 cites·10 claims
- 0758US8794568B2Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pinsLAFONT LAURENT·Filed 2011·Granted Aug 5, 2014·2 cites·9 claims
- 0857US9011098B2Propeller for an aircraft turbine engine comprising a vane retaining ring mounted about the hubLAFONT LAURENT·Filed 2010·Granted Apr 21, 2015·2 cites·18 claims
- 0957US8439300B2Rear part of an aircraft comprising a structure for supporting engines, extending through the fuselage and connected thereto by at least one connecting rodLAFONT LAURENT·Filed 2009·Granted May 14, 2013·4 cites·10 claims
- 1055US8083176B2Method for mounting an aircraft engine on a rigid structure of a strut for locking the engineLAFONT LAURENT·Filed 2006·Granted Dec 27, 2011·4 cites·12 claims
- 1150US8448897B2Rear part of an aircraft comprising a structure for supporting engines, connected to the fuselage by at least one blocking element under compression loadingLAFONT LAURENT·Filed 2009·Granted May 28, 2013·1 cites·10 claims
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