Jérôme Colmagro
30Patents
4h-index
42Co-inventors
59Inventor score
Filing activity: Jan 11, 2012 → May 25, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9656742B2 | Air ejection device comprising an aerodynamic profile provided with a slot obturating flexible tongue | Emerging Cross-Sectional Technologies | 10 | Active |
| US10556699B2 | Aircraft engine assembly comprising a pylon leading edge incorporated with an annular row of unfaired after-guide vanes | Emerging Cross-Sectional Technologies | 10 | Active |
| US8770518B2 | Connection of a fuselage to an aircraft wing | Emerging Cross-Sectional Technologies | 9 | Active |
| US9199719B2 | Keel beam of an aircraft | Performing Operations; Transporting | 4 | Active |
| US9656736B2 | Method for assembling an aircraft aft portion | Performing Operations; Transporting | 4 | Active |
| US8746621B2 | Connector for stiffening frames between an aircraft fuselage and a wing box | Performing Operations; Transporting | 3 | Active |
| US10647440B2 | Assembly for an aircraft comprising an engine of the “open rotor puller” type and means for attaching the latter to the rigid structure of an attachment pylon | Physics | 3 | Active |
| US11319079B2 | Assembly for an aircraft comprising a primary structure for an attachment pylon secured to a wing box by means of fittings that are more compact in the leading edge region | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10519899B2 | Thrust reverser system limiting aerodynamic perturbation in an inactive configuration | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10144500B2 | Aircraft nacelle comprising at least one fan cowl door which is mounted so as to be able to rotate about the longitudinal axis of the nacelle | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10336458B2 | Aircraft assembly comprising a mounting strut built into the nacelle and arranged at the rear section of the fuselage | Performing Operations; Transporting | 2 | Active |
| US11840347B2 | Assembly comprising a translationally and rotationally immobile link axis, engine attachment or aircraft comprising such an assembly | Emerging Cross-Sectional Technologies | 1 | Active |
| US10994380B2 | Device for manipulating a hollow shaft intended to create a pivot link between a first element and a second element | Performing Operations; Transporting | 1 | Active |
| US10730634B2 | Primary support strut structure for an aircraft | Performing Operations; Transporting | 1 | Active |
| US10814994B2 | Primary support structure for an aircraft power plant support pylon | Performing Operations; Transporting | 1 | Active |
| US10232930B2 | Nacelle for an aircraft engine assembly comprising at least one jointed nacelle cowling at its front end | Emerging Cross-Sectional Technologies | 1 | Active |
| US11840348B2 | Braced-pylon architecture for mounting an engine to an aircraft | Emerging Cross-Sectional Technologies | 0 | Active |
| US11987029B2 | Method for manufacturing a cellular structure obtained from bent strips of material, and cellular structure thus obtained | Performing Operations; Transporting | 0 | Active |
| US11027852B2 | Assembly for aircraft comprising a primary mounting pylon structure fixed to an airfoil box using a bolted link | Performing Operations; Transporting | 0 | Active |
| US11104445B2 | Assembly of parts assembled by a through-shaft that can be fitted if the parts are in approximate alignment | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11897622B2 | Propeller propulsion unit comprising a heat engine and an electric motor and aircraft comprising such a propeller propulsion unit | Emerging Cross-Sectional Technologies | 0 | Active |
| US11485512B2 | Closed circuit for cooling the engine of an aircraft propulsion plant | Emerging Cross-Sectional Technologies | 0 | Active |
| US11421548B2 | Aircraft engine assembly with boundary layer ingestion including an electric motor and a cooling system partially arranged in the exhaust cone | Emerging Cross-Sectional Technologies | 0 | Active |
| US11332255B2 | Primary structure of a strut for bearing an aircraft power plant, the rear part of which is formed by a set of connecting rods | Performing Operations; Transporting | 0 | Active |
| US10640198B2 | Propeller for an aircraft turbo engine, including safety means for controlling blade angle of attack | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.