Bernard Certain
21Patents
6h-index
5Co-inventors
58Inventor score
Filing activity: Jul 15, 2002 → Nov 24, 2015
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8464980B2 | Power plant, a helicopter including such a power plant, and a method implemented by said power plant | Performing Operations; Transporting | 22 | Active |
| US8283796B2 | Hybrid engine installation and a method of controlling such an engine installation | Emerging Cross-Sectional Technologies | 17 | Active |
| US7223071B2 | Device for providing assistance to the pilot of a rotorcraft in the event of engine failure | Performing Operations; Transporting | 17 | Expired |
| US7143003B2 | Pilot indicator for predicting changes in the monitoring parameters of a gas turbine engine | Physics | 9 | Expired |
| US6698181B2 | System for regulating the output of an engine of a helicopter | Physics | 8 | Expired |
| US9353642B2 | Rotary wing aircraft having two main engines together with a less powerful secondary engine, and a corresponding method | Mechanical Engineering; Lighting; Heating | 8 | Active |
| US8977412B2 | Automatic flight control method for a rotorcraft enabling the rotorcraft to maintain a path by tracking manual flight controls | Physics | 6 | Active |
| US9533757B2 | Buoyancy system for an aircraft | Performing Operations; Transporting | 4 | Active |
| US7907066B2 | Method and a device for detecting and signaling that a rotorcraft is approaching the vortex domain | Performing Operations; Transporting | 4 | Active |
| US7149646B2 | Pilot indicator for predicting changes in the speed of rotation of the main rotor of a rotorcraft | Performing Operations; Transporting | 4 | Expired |
| US7530232B2 | Method for regulating the flow rate of fuel to a turboshaft engine in acceleration or in deceleration | Mechanical Engineering; Lighting; Heating | 4 | Expired |
| US9004400B2 | Method of controlling a buoyancy system for an aircraft, a buoyancy system implementing said method, and an aircraft | Performing Operations; Transporting | 3 | Active |
| US7941250B2 | Method and a device for obtaining a predictive vertical speed of a rotorcraft | Physics | 3 | Active |
| US10047678B2 | Method of stopping a rotorcraft engine in overspeed, and a system and a rotorcraft associated therewith | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US8162264B2 | Method of jettisoning an external load carried by an aircraft, and an associated device | Performing Operations; Transporting | 3 | Active |
| US10479494B2 | Rotorcraft tail rotor, a rotorcraft fitted with such a tail rotor, and a method of statically and/or dynamically balancing a rotorcraft tail rotor | Performing Operations; Transporting | 1 | Active |
| US9302769B2 | Ducted rotor for an aircraft and a rotorcraft | Performing Operations; Transporting | 1 | Active |
| US9383756B2 | Automatic flight control method for a rotorcraft enabling the rotorcraft to maintain a path by tracking manual flight controls | Physics | 1 | Active |
| US10150569B2 | Method of stopping a rotorcraft engine in overspeed, and a system and a rotorcraft associated therewith | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10131425B2 | Rotary wing aircraft having a non-ducted tail rotor with at least five blades | Performing Operations; Transporting | 1 | Active |
| US7992392B2 | Method for regulating the flow rate of fuel to a turboshaft engine in acceleration or in deceleration | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.