Jean-Noel Mahieu
19Patents
5h-index
28Co-inventors
62Inventor score
Filing activity: Jun 19, 2006 → Aug 29, 2018
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7581932B2 | Method of manufacturing a composite turbomachine blade, and a blade obtained by the method | Mechanical Engineering; Lighting; Heating | 25 | Active |
| US9162750B2 | Aircraft propeller blade | Mechanical Engineering; Lighting; Heating | 16 | Active |
| US7926761B2 | Mechanical part and method of manufacturing such a part | Emerging Cross-Sectional Technologies | 13 | Active |
| US8685868B2 | Reinforcing fibrous structure for a composite material and a part containing said structure | Emerging Cross-Sectional Technologies | 12 | Active |
| US8529209B2 | Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mounted | Mechanical Engineering; Lighting; Heating | 7 | Active |
| US8709314B2 | Method for manufacturing a turbine engine vane | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9328737B2 | Unducted fan for turbine engine | Emerging Cross-Sectional Technologies | 4 | Active |
| US9771810B2 | Fiber preform for a turbine engine blade made of composite material and having an integrated platform, and a method of making it | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US8616853B2 | Stator vane for 3D composite blower | Emerging Cross-Sectional Technologies | 3 | Active |
| US8801384B2 | Airfoil attachment holding an airfoil root in a broach fitting | Performing Operations; Transporting | 3 | Active |
| US8845294B2 | Spacer interposed between a blade root and the bottom of a slot in the disk in which the blade is mounted | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9817923B2 | Part made from 3D woven composite material | Physics | 3 | Active |
| US9617858B2 | Fibrous reinforcement structure for composite material part having a reduced thickness portion | Emerging Cross-Sectional Technologies | 3 | Active |
| US9597841B2 | Fibrous structure having variable numbering yarns | Emerging Cross-Sectional Technologies | 2 | Active |
| US10180069B2 | Method of fabricating a composite material blade having internal channels, and a composite material turbine engine blade | Emerging Cross-Sectional Technologies | 1 | Active |
| US11015460B2 | Blade comprising a blade body made of composite material and a leading-edge shield | Emerging Cross-Sectional Technologies | 1 | Active |
| US10019549B2 | Method of designing a common preform for providing preforms for turbine engine outlet guide vanes of different geometrical profiles and made out of composite material | Performing Operations; Transporting | 0 | Active |
| US9657583B2 | Composite material reinforcing part of pi-shaped section, in particular a platform for a turbine engine fan, and its method of fabrication | Emerging Cross-Sectional Technologies | 0 | Active |
| US11230798B2 | Woven fibrous structure for forming a casing preform | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.