Thierry Bourret
20Patents
6h-index
34Co-inventors
65Inventor score
Filing activity: May 17, 2004 → Jun 11, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| USD726758S1 | Aircraft cockpit display screen with graphical user interface | General | 49 | Active |
| US9280904B2 | Methods, systems and computer readable media for arming aircraft runway approach guidance modes | Physics | 14 | Active |
| US8723695B2 | Method and device for automatically determining an erroneous height value of a radioaltimeter mounted on an aircraft | Physics | 8 | Active |
| US9052198B2 | Interactive dialog device between an operator of an aircraft and a guidance system of said aircraft | Physics | 6 | Active |
| US9561868B2 | Method and device for vertically guiding an aircraft during an approach of a runway along a lateral approach trajectory | Physics | 6 | Active |
| US9008867B2 | Method and device for automatically monitoring the ability of an aircraft to follow a flight trajectory with at least one turn | Physics | 6 | Active |
| US9342988B2 | Method and device for determining a linear terrain profile along a lateral approach trajectory of an airport | Physics | 5 | Active |
| US8725322B2 | Method and device for updating a target altitude for an emergency descent of an aircraft | Physics | 5 | Active |
| US9058743B2 | Automatic landing method and device for an aircraft on a strong slope runway | Physics | 3 | Active |
| US8515598B2 | Method and device for aiding the flight management of an aircraft | Physics | 3 | Active |
| US8695921B2 | Automatic method and device for aiding the piloting of an airplane | Physics | 2 | Active |
| US10794727B2 | Method and device for verifying a guidance signal | Physics | 1 | Active |
| US7639154B2 | Process and device for regulating the luminous intensity of indicator lights of a piece of monitoring and control equipment in an airplane cockpit | Performing Operations; Transporting | 1 | Active |
| US9904291B2 | Method and system to control emergency descent of aircraft | Physics | 1 | Active |
| US9671783B2 | Automatic method and device for aiding the piloting of an airplane | Physics | 0 | Active |
| US7400949B2 | Device for adjusting at least one parameter, in particular for an aircraft automatic pilot system | Physics | 0 | Active |
| US9994303B2 | Control system and method for an aircraft | Physics | 0 | Active |
| US11747170B2 | Method and system for estimating an angular deviation from a reference guidance axis, a position and a velocity of an aircraft | Physics | 0 | Active |
| US11790796B2 | Method and system for determining a position error of an aircraft | Physics | 0 | Active |
| US9840337B2 | Method and device for activating the display of at least one stall margin indicator of an aircraft | Physics | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.