FB

Francois Robert Bellabal

SN Snecma: 7 patents #102 of 1,717Top 6%
SE Safran Aircraft Engines: 3 patents #417 of 1,821Top 25%
Overall (All Time): #506,455 of 4,157,543Top 15%
10
Patents All Time

Issued Patents All Time

Patent #TitleCo-InventorsDate
10184401 Turbojet engine suspension using a double rear support 2019-01-22
10132241 Method of producing suspension for a structure in a turbojet engine using a hyperstatic trellis with pre-stressed link elements Nicolas Marc Florent 2018-11-20
10106266 Suspension structure for suspending a turboprop having two unducted propellers from a structural element of an aircraft with rigid fastening of the air intake structure Mathieu Ange Poisson, Nicolas Marc Florent 2018-10-23
9863273 Isostatic suspension of a turbojet by rear double support Francois Gallet, Mathieu Ange Poisson 2018-01-09
9828877 Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods Thomas Gérard Daniel Riviere, Olivier Renon, Guilhem Seize 2017-11-28
9429073 Hyperstatic truss comprising connecting rods Thomas Alain Christian Vincent 2016-08-30
9366186 Lateral turbojet improved in order to limit the deformation thereof 2016-06-14
9121347 Link between the exhaust casing and a structural ring of the fan duct of a jet engine Guilhem Seize, Thomas Alain Christian Vincent 2015-09-01
9067688 Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system Guilhem Seize, Thomas Alain Christian Vincent 2015-06-30
8919723 Turbojet engine fan duct suspension using connecting rods with elastomer bushing Thomas Gérard Daniel Riviere 2014-12-30