Alexandre Forestier
22Patents
14h-index
19Co-inventors
78Inventor score
Filing activity: Jan 26, 1982 → Jun 5, 2002
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US4940386A | Multiple flow turbojet engine with an outer ring of the fan outlet shrunk onto the case | Emerging Cross-Sectional Technologies | 43 | Expired |
| US6668559B2 | Fastening a CMC combustion chamber in a turbomachine using the dilution holes | Emerging Cross-Sectional Technologies | 37 | Expired |
| US4494909A | Damping device for turbojet engine fan blades | Emerging Cross-Sectional Technologies | 31 | Expired |
| US4999996A | System for mounting a pre-vaporizing bowl to a combustion chamber | Mechanical Engineering; Lighting; Heating | 30 | Expired |
| US4451110A | Turbine bearing | Mechanical Engineering; Lighting; Heating | 27 | Expired |
| US6708495B2 | Fastening a CMC combustion chamber in a turbomachine using brazed tabs | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US6679062B2 | Architecture for a combustion chamber made of ceramic matrix material | Mechanical Engineering; Lighting; Heating | 24 | Expired |
| US4527952A | Device for locking a turbine rotor blade | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US4858721A | Acoustic panel for sound insulating linings of gas ducts | Mechanical Engineering; Lighting; Heating | 23 | Expired |
| US4820120A | Stator assembly for the fan of a multi-flow turbo-jet engine | Emerging Cross-Sectional Technologies | 20 | 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 |
| US4449607A | Soundproofing for a gas pipe, in particular for the fan jet of a turbojet, and equipment for its fabrication | Emerging Cross-Sectional Technologies | 17 | Expired |
| US5159807A | Control system for oxidizer intake diaphragms | Mechanical Engineering; Lighting; Heating | 15 | Expired |
| US6647729B2 | Combustion chamber provided with a system for fixing the chamber end wall | Mechanical Engineering; Lighting; Heating | 13 | Expired |
| US5172545A | Apparatus for attaching a pre-atomization bowl to a gas turbine engine combustion chamber | Emerging Cross-Sectional Technologies | 13 | Expired |
| US4453891A | Vibration damping device, especially for a blade of a turbojet engine | Emerging Cross-Sectional Technologies | 12 | Expired |
| US6732532B2 | Resilient mount for a CMC combustion chamber of a turbomachine in a metal casing | Mechanical Engineering; Lighting; Heating | 12 | Expired |
| US5230212A | Oxidizer supply control system for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 5 | Expired |
| US6155055A | Separator for a two-head combustor chamber | Mechanical Engineering; Lighting; Heating | 5 | Expired |
| US5996333A | Oxidizer control device for a gas turbine engine | Mechanical Engineering; Lighting; Heating | 4 | Expired |
| US4525135A | Apparatus for molding and perforating a FRP sheet | Emerging Cross-Sectional Technologies | 1 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.