Philippe Pabion
22Patents
9h-index
31Co-inventors
71Inventor score
Filing activity: Jul 16, 1992 → Jan 9, 2009
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8162593B2 | Inter-turbine casing with cooling circuit, and turbofan comprising it | Mechanical Engineering; Lighting; Heating | 36 | Active |
| US7687021B2 | Method of fabricating a casing for turbine stator | Emerging Cross-Sectional Technologies | 23 | Active |
| US7377749B2 | Device for balancing a rotating part, in particular a turbojet rotor | Emerging Cross-Sectional Technologies | 22 | Active |
| US7234920B2 | Turbine casing having refractory hooks and obtained by a powder metallurgy method | Emerging Cross-Sectional Technologies | 21 | Expired |
| US5421704A | Inter-blade platform for a bladed disc of a turbomachine rotor | Emerging Cross-Sectional Technologies | 17 | Expired |
| US6699011B2 | Linking arrangement of a turbine stator ring to a support strut | Mechanical Engineering; Lighting; Heating | 17 | Expired |
| US5193982A | Separate inter-blade platform for a bladed rotor disk | Emerging Cross-Sectional Technologies | 17 | Expired |
| US7290982B2 | Arrangement for the attachment of distributor sectors supporting vanes around an arc of a circle | Mechanical Engineering; Lighting; Heating | 13 | Expired |
| US7972107B2 | Device for cooling a turbomachine turbine casing | Emerging Cross-Sectional Technologies | 11 | Active |
| US6050522A | Thrust reverser for a high bypass turbofan engine | Emerging Cross-Sectional Technologies | 9 | Expired |
| US7527470B2 | Stator turbine vane with improved cooling | Emerging Cross-Sectional Technologies | 9 | Active |
| US5520514A | Sealing lining between vanes and intermediate platforms | Mechanical Engineering; Lighting; Heating | 8 | Expired |
| US7025562B2 | Device for cooling turbine disks | Mechanical Engineering; Lighting; Heating | 7 | Expired |
| US7004721B2 | Annular platform for a nozzle of a low-pressure turbine of a turbomachine | Emerging Cross-Sectional Technologies | 6 | Expired |
| US8221061B2 | Gas turbine engine with valve for establishing communication between two enclosures | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US7794203B2 | Joining device for joining two assemblies, for example for a stator of a turbomachine | Emerging Cross-Sectional Technologies | 4 | Active |
| US8162594B2 | Cooled blade for a turbomachine | Emerging Cross-Sectional Technologies | 4 | Active |
| US8011879B2 | Transition channel between two turbine stages | Emerging Cross-Sectional Technologies | 4 | Active |
| US7137783B2 | Cooled gas turbine blades | Emerging Cross-Sectional Technologies | 2 | Expired |
| US7351030B2 | Connection device for making a connection between a turbomachine nozzle and a feed enclosure for feeding cooling fluid to injectors | Emerging Cross-Sectional Technologies | 2 | Expired |
| US8128375B2 | Turbomachine blade that is cast with a local fattening of the section of the airfoil | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US7210901B2 | Assembly of sectors of a dispensing unit in a gas turbine | Mechanical Engineering; Lighting; Heating | 0 | Expired |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.