Eric Conete
35Patents
13h-index
44Co-inventors
81Inventor score
Filing activity: Feb 10, 1993 → Dec 13, 2022
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 |
| US7234306B2 | Gas turbine combustion chamber made of CMC and supported in a metal casing by CMC linking members | Mechanical Engineering; Lighting; Heating | 44 | Expired |
| US7677026B2 | Mixer for separate-flow nozzle | Emerging Cross-Sectional Technologies | 40 | Active |
| US7237388B2 | Assembly comprising a gas turbine combustion chamber integrated with a high pressure turbine nozzle | Emerging Cross-Sectional Technologies | 31 | Expired |
| US6988369B2 | Combustion chamber sealing ring, and a combustion chamber including such a ring | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US6679062B2 | Architecture for a combustion chamber made of ceramic matrix material | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US6398483B1 | Protection device for protecting control mechanism of inlet guide-vanes of turbojet engine | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US6708495B2 | Fastening a CMC combustion chamber in a turbomachine using brazed tabs | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US6823676B2 | Mounting for a CMC combustion chamber of a turbomachine by means of flexible connecting sleeves | Mechanical Engineering; Lighting; Heating | 20 | Expired |
| US6675585B2 | Connection for a two-part CMC chamber | Mechanical Engineering; Lighting; Heating | 18 | Expired |
| US8590316B2 | CMC mixer with structural outer cowling | Emerging Cross-Sectional Technologies | 14 | Active |
| US5367874A | Integral composite gas turbine afterburner structure | 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 |
| US8919136B2 | Flexible abutment links for attaching a part made of CMC | Mechanical Engineering; Lighting; Heating | 10 | Active |
| US7237387B2 | Mounting a high pressure turbine nozzle in leaktight manner to one end of a combustion chamber in a gas turbine | Emerging Cross-Sectional Technologies | 9 | Expired |
| US9261008B2 | Exhaust with an acoustic attenuation system | Emerging Cross-Sectional Technologies | 8 | Active |
| US8640825B2 | Acoustic panel for an ejector nozzle | Emerging Cross-Sectional Technologies | 7 | Active |
| US5359849A | Afterburner assembly for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 6 | Expired |
| US8205453B2 | Method for assembling end to end two parts having different thermal expansion coefficients and assembly thus obtained | Emerging Cross-Sectional Technologies | 4 | Active |
| US11519361B2 | Exhaust cone with flexible fitting | Emerging Cross-Sectional Technologies | 3 | Active |
| US9403240B2 | Method for the brazing of parts made from a composite material, incorporating a slug in the bond | Chemistry; Metallurgy | 3 | Active |
| US7168253B1 | Monobloc flameholder arm for an afterburner device of a bypass turbojet | Mechanical Engineering; Lighting; Heating | 3 | Expired |
| US11821387B2 | Ejection cone having a flexible aerodynamic attachment | Emerging Cross-Sectional Technologies | 2 | Active |
| US9573852B2 | Method for brazing parts made from a composite material, with anchoring of the brazed joint | Chemistry; Metallurgy | 2 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.