Francois Robert Bellabal
10Patents
3h-index
7Co-inventors
42Inventor score
Filing activity: Feb 9, 2011 → Jan 7, 2015
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10184401B2 | Turbojet engine suspension using a double rear support | Emerging Cross-Sectional Technologies | 13 | Active |
| US9121347B2 | Link between the exhaust casing and a structural ring of the fan duct of a jet engine | Emerging Cross-Sectional Technologies | 7 | Active |
| US9067688B2 | Turboshaft engine attached to a pylon of the fuselage of an aircraft by a failsafe suspension system | Performing Operations; Transporting | 6 | Active |
| US9828877B2 | Turbojet engine cold stream flow path suspended from the exhaust case by radial crevice mounts and link rods | Emerging Cross-Sectional Technologies | 2 | Active |
| US9429073B2 | Hyperstatic truss comprising connecting rods | Emerging Cross-Sectional Technologies | 1 | Active |
| US8919723B2 | Turbojet engine fan duct suspension using connecting rods with elastomer bushing | Emerging Cross-Sectional Technologies | 0 | Active |
| US9863273B2 | Isostatic suspension of a turbojet by rear double support | Emerging Cross-Sectional Technologies | 0 | Active |
| US10106266B2 | 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 | Emerging Cross-Sectional Technologies | 0 | Active |
| US9366186B2 | Lateral turbojet improved in order to limit the deformation thereof | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10132241B2 | Method of producing suspension for a structure in a turbojet engine using a hyperstatic trellis with pre-stressed link elements | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.