Hakim Maalioune
25Patents
3h-index
36Co-inventors
59Inventor score
Filing activity: Feb 1, 2008 → Nov 23, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8692489B2 | System for controlling an electrical device of a nacelle | Emerging Cross-Sectional Technologies | 22 | Active |
| US9448557B2 | Method and system for controlling at least one actuator of the cowlings of a turbojet engine thrust inverter | Emerging Cross-Sectional Technologies | 5 | Active |
| US8955306B2 | Method for synchronizing the actuators of a movable thrust reverser cowl | Mechanical Engineering; Lighting; Heating | 4 | Active |
| US9109538B2 | Aircraft control system | Emerging Cross-Sectional Technologies | 3 | Active |
| US8975911B2 | System for controlling at least one actuator of the cowlings of a turbojet engine thrust reverser | Emerging Cross-Sectional Technologies | 3 | Active |
| US9850776B2 | Variable-section nozzle, and aircraft turbojet engine nacelle equipped with such a nozzle | Emerging Cross-Sectional Technologies | 2 | Active |
| US9482183B2 | Thrust reverser control system | Emerging Cross-Sectional Technologies | 2 | Active |
| US8650855B2 | System for controlling at least one actuator of the cowlings of a turbojet engine thrust reverser | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US9051898B2 | Thrust reversal device | Electricity | 1 | Active |
| US8955305B2 | Self-calibration method for the electric jacks of a turbojet nacelle | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8777155B2 | Electric power supply circuit for a turbojet engine nacelle | Performing Operations; Transporting | 1 | Active |
| US8285467B2 | Method and system for controlling at least one actuator for actuating the cowlings of a thrust inverter in a turbojet engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11492128B2 | Method for supplying electric power to an ultrasonic nacelle de-icing and anti-icing | Performing Operations; Transporting | 1 | Active |
| US9057342B2 | Control system for a turboreactor nacelle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12208915B2 | Aircraft assembly fitted with at least one hydrogen-powered thrust reverser actuation system | Emerging Cross-Sectional Technologies | 0 | Active |
| US10266162B2 | Method and system for controlling the braking of an aircraft equipped with a thrust-reversal system | Emerging Cross-Sectional Technologies | 0 | Active |
| US8991151B2 | Actuator system for a mobile panel of a nacelle of a turbojet | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9587584B2 | Thrust-reversal device for an aircraft including at least two thrust reversers | Emerging Cross-Sectional Technologies | 0 | Active |
| US11946436B2 | Aircraft control architecture, of at least one actuator of a nacelle movable cowl | Emerging Cross-Sectional Technologies | 0 | Active |
| US11313916B2 | Testability method for an electronic power chain associated with an electric motor | Electricity | 0 | Active |
| US12065986B2 | System for controlling an aircraft thrust reversal means | Physics | 0 | Active |
| US12404013B2 | System for managing the deceleration of an aircraft on a runway on the ground and associated method | Emerging Cross-Sectional Technologies | 0 | Active |
| US12054278B2 | High availability electrical switcher: monitoring of a simplex actuation chain by a redundant control | Physics | 0 | Active |
| US11168645B2 | Device for actuating a thrust reverser with an anti-deployment member | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US8831900B2 | System for controlling at least one actuator for thrust reverser cowlings on a turbojet engine and method for testing said system | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.