Jean-Philippe Joret
29Patents
4h-index
47Co-inventors
59Inventor score
Filing activity: Jun 11, 2007 → Dec 21, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9004548B2 | Device for locking an opening part of a jet engine nacelle with respect to a fixed part, and nacelle equipped with such a device | Emerging Cross-Sectional Technologies | 49 | Active |
| US9249756B2 | Assembly for an aircraft turbojet engine comprising a thrust reversal cowl | Performing Operations; Transporting | 9 | Active |
| US8448896B2 | Guiding system for aircraft nacelle maintenance | Performing Operations; Transporting | 4 | Active |
| US8464512B2 | Actuator for an aircraft nacelle mobile structure, and nacelle comprising at least one such actuator | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8869506B2 | Turbojet engine nacelle including a device for absorbing circumferential stresses | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US8739552B2 | Structural nacelle | Performing Operations; Transporting | 4 | Active |
| US9169026B2 | Turbojet engine nacelle | Emerging Cross-Sectional Technologies | 2 | Active |
| US9211956B2 | Turbojet engine nacelle with translatable upstream cowl | Performing Operations; Transporting | 2 | Active |
| US9777598B2 | Flattened nacelle of a turbojet engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11891185B2 | Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure | Emerging Cross-Sectional Technologies | 1 | Active |
| US8769926B2 | Thrust reverser having an aerodynamic coupling for a front frame | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US12037941B2 | Supersonic speed attenuator of an air intake of an aircraft propulsion assembly comprising a de-icing device and de-icing method | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US12258924B2 | Thrust reverser with door of a nacelle of a turbojet engine of an aircraft with a system for diverting fluids to the exterior | Emerging Cross-Sectional Technologies | 0 | Active |
| US12253048B2 | Fastening of an exhaust cone in a turbomachine turbine | Emerging Cross-Sectional Technologies | 0 | Active |
| US12152552B2 | Front frame and deflection grid of a thrust reverser of an aircraft nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US9834313B2 | Front frame for a cascade thrust reverser structure | Emerging Cross-Sectional Technologies | 0 | Active |
| US12116954B2 | Fastening of an exhaust cone in a turbomachine nozzle | Emerging Cross-Sectional Technologies | 0 | Active |
| US9593644B2 | Control device for a turbojet engine thrust reverser, blocking the reverser | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12000300B2 | Exhaust cone for a turbomachine | Emerging Cross-Sectional Technologies | 0 | Active |
| US12049853B2 | Thrust reverser for an aircraft bypass turbojet engine nacelle | Emerging Cross-Sectional Technologies | 0 | Active |
| US10753315B2 | Rear assembly of a turbojet engine nacelle including a fireproof sealing device | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12037940B2 | Supersonic air inlet of an aircraft propelling assembly comprising a support arm de-icing device and de-icing method | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9670878B2 | Cellular acoustic structure for a turbojet engine and turbojet engine incorporating at least one such structure | Emerging Cross-Sectional Technologies | 0 | Active |
| US11959437B2 | Fastening of an exhaust cone in a turbomachine nozzle | Emerging Cross-Sectional Technologies | 0 | Active |
| US9938897B2 | Air inlet structure for a turbojet engine nacelle of laminar type | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.