Inventor · disambiguated record
Francois Robert Bellabal
Also filed as: BELLABAL FRANCOIS · BELLABAL FRANCOIS ROBERT · BELLABAL FRANÇOIS ROBERT
10 granted patents·1 pending application·42 citations·filing 2011–2015
85Inventor score
Files withBELLABAL FRANCOIS ROBERT4SNECMA3SAFRAN AIRCRAFT ENGINES2BELLABAL FRANCOIS1RIVIERE THOMAS GÉRARD DANIEL1
Top patents by PatentIndex Score
11 records- 0189US10184401B2Turbojet engine suspension using a double rear supportSNECMA·Filed 2014·Granted Jan 22, 2019·16 cites·10 claims
- 0280US9121347B2Link between the exhaust casing and a structural ring of the fan duct of a jet engineBELLABAL FRANCOIS ROBERT·Filed 2011·Granted Sep 1, 2015·8 cites·9 claims
- 0373US9828877B2Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rodsRIVIERE THOMAS GÉRARD DANIEL·Filed 2012·Granted Nov 28, 2017·7 cites·4 claims
- 0469US10106266B2Suspension structure for suspending a turboprop having two unducted propellers from a structural element of an aircraft with rigid fastening of the air intake structureSAFRAN AIRCRAFT ENGINES·Filed 2015·Granted Oct 23, 2018·2 cites·10 claims
- 0569US9067688B2Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension systemBELLABAL FRANCOIS·Filed 2011·Granted Jun 30, 2015·7 cites·8 claims
- 0651US9863273B2Isostatic suspension of a turbojet by rear double supportSNECMA·Filed 2014·Granted Jan 9, 2018·1 cites·13 claims
- 0749US9429073B2Hyperstatic truss comprising connecting rodsBELLABAL FRANCOIS ROBERT·Filed 2011·Granted Aug 30, 2016·1 cites·11 claims
- 0844US10132241B2Method of producing suspension for a structure in a turbojet engine using a hyperstatic trellis with pre-stressed link elementsSAFRAN AIRCRAFT ENGINES·Filed 2014·Granted Nov 20, 2018·0 cites·18 claims
- 0941US2014311161A1Method for creating a connecting element positioned between two components of a structure, connecting element and bypass turbojet engine comprising such a connecting elementSNECMA·Filed 2012·Application pending·0 cites
- 1039US9366186B2Lateral turbojet improved in order to limit the deformation thereofBELLABAL FRANCOIS ROBERT·Filed 2011·Granted Jun 14, 2016·0 cites·13 claims
- 1136US8919723B2Turbojet engine fan duct suspension using connecting rods with elastomer bushingBELLABAL FRANCOIS ROBERT·Filed 2012·Granted Dec 30, 2014·0 cites·8 claims
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Identity basis: PatentsView inventor disambiguation (2025Q4-odp release). How scoring works →