Hazem Kioua
10Patents
2h-index
17Co-inventors
43Inventor score
Filing activity: Apr 11, 2013 → Dec 21, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9382814B2 | Device for connecting a thrust reverser front frame to a fan casing and nacelle incorporating such a device | Emerging Cross-Sectional Technologies | 3 | Active |
| US10087781B2 | Assembly centering device for turbojet engine nacelle | Emerging Cross-Sectional Technologies | 2 | 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 |
| US11572188B2 | Aircraft engine nacelle with asymmetric fan cowls | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12044168B2 | Air inlet of a turbomachine nacelle including a circulation conduit of a hot air flow between a movable upstream part and a fixed downstream part | Emerging Cross-Sectional Technologies | 0 | Active |
| US12214893B2 | Air inlet for an aircraft propulsion unit comprising a member for moving a movable upstream portion and method for using such an air inlet | Emerging Cross-Sectional Technologies | 0 | Active |
| US12246846B2 | Aircraft propulsion unit comprising a nacelle and a turbomachine independently supported by a wing, fuselage or tail element | Performing Operations; Transporting | 0 | Active |
| US12110120B2 | Propulsion unit for an aircraft and method for mounting same | Emerging Cross-Sectional Technologies | 0 | Active |
| US9341083B2 | Turbojet engine nacelle with downstream section | 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 |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.