Georges Habarou
15Patents
10h-index
29Co-inventors
72Inventor score
Filing activity: Jan 21, 1986 → Jul 26, 2011
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7249462B2 | Mounting a turbine nozzle on a combustion chamber having CMC walls in a gas turbine | Emerging Cross-Sectional Technologies | 58 | Expired |
| US8141371B1 | Gas turbine combustion chamber made of CMC material and subdivided into sectors | Mechanical Engineering; Lighting; Heating | 49 | Active |
| US8257029B2 | Turbine ring assembly for gas turbine | Emerging Cross-Sectional Technologies | 32 | Active |
| US8496431B2 | Turbine ring assembly for gas turbine | Emerging Cross-Sectional Technologies | 25 | Active |
| US6988369B2 | Combustion chamber sealing ring, and a combustion chamber including such a ring | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US8146372B2 | Gas turbine combustion chamber having inner and outer walls subdivided into sectors | Mechanical Engineering; Lighting; Heating | 17 | Active |
| US5348598A | Method of manufacturing a gun barrel provided with a lining | Mechanical Engineering; Lighting; Heating | 14 | Expired |
| US8424312B2 | Exhaust system for gas turbine | Emerging Cross-Sectional Technologies | 13 | Active |
| US6732532B2 | Resilient mount for a CMC combustion chamber of a turbomachine in a metal casing | Mechanical Engineering; Lighting; Heating | 12 | Expired |
| US9080463B2 | Turbine ring assembly | Emerging Cross-Sectional Technologies | 12 | Active |
| US4669954A | Abradable turbine rings and turbines thus obtained | Mechanical Engineering; Lighting; Heating | 10 | Expired |
| US8951017B2 | Turbomachine blade, a rotor, a low pressure turbine, and a turbomachine fitted with such a blade | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US6378294B1 | System for activating an adjustable tube by means of an elastic ring for a thrust nozzle | Emerging Cross-Sectional Technologies | 3 | Expired |
| US7168253B1 | Monobloc flameholder arm for an afterburner device of a bypass turbojet | Mechanical Engineering; Lighting; Heating | 3 | Expired |
| US6385965B1 | System for activating a steerable thrust-vectoring nozzle for a jet propulsion system using several circumferentially distributed elastic assemblies | Emerging Cross-Sectional Technologies | 2 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.