Bruno Jacques Gerard Dambrine
51Patents
9h-index
54Co-inventors
81Inventor score
Filing activity: Nov 5, 1997 → Jan 19, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US7241112B2 | Turbomachine blade, in particular a fan blade, and its method of manufacture | Emerging Cross-Sectional Technologies | 39 | Active |
| US7101154B2 | Turbomachine blade, in particular a fan blade, and its method of manufacture | Emerging Cross-Sectional Technologies | 36 | Expired |
| US7581932B2 | Method of manufacturing a composite turbomachine blade, and a blade obtained by the method | Mechanical Engineering; Lighting; Heating | 25 | Active |
| US8322971B2 | Method of manufacturing a gas turbine casing out of composite material, and a casing as obtained thereby | Emerging Cross-Sectional Technologies | 18 | 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 |
| US8505588B2 | Production of a fibrous structure with variable thickness by 3D weaving | Textiles; Paper | 10 | Active |
| US6174570A | Method for metal coating of fibres by liquid process | Emerging Cross-Sectional Technologies | 9 | Expired |
| US9321100B2 | Method for producing a metal reinforcement for a turbomachine blade | Emerging Cross-Sectional Technologies | 7 | Active |
| US10145039B2 | Fiber blank woven as a single piece by three-dimensional weaving to make a closed box-structure platform out of composite material for a turbine engine fan | Emerging Cross-Sectional Technologies | 6 | Active |
| US9364887B2 | Process for manufacturing a metal part, such as turbine engine blade reinforcement | Emerging Cross-Sectional Technologies | 5 | Active |
| US7334999B2 | Turbomachine rotor including at least one disk reinforced by a composite ring | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9669570B2 | Process for injection moulding a composite part | Performing Operations; Transporting | 5 | Active |
| US9200385B2 | Jacquard loom having optimized warp yarn density | Textiles; Paper | 4 | Active |
| US9617858B2 | Fibrous reinforcement structure for composite material part having a reduced thickness portion | Emerging Cross-Sectional Technologies | 3 | 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 |
| US11285638B2 | Method of fabricating a composite material part by injecting a filled slurry into a fiber texture | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US8980031B2 | Method of fabricating a turbine engine blade out of composite material | Emerging Cross-Sectional Technologies | 3 | Active |
| US8448837B2 | Method for manufacturing a one-piece annular metal part having a reinforcing insert of composite material | Emerging Cross-Sectional Technologies | 3 | Active |
| US5941688A | Fibre-reinforced rotor stage for a turbomachine | Emerging Cross-Sectional Technologies | 3 | Expired |
| US10724159B2 | Fiber blank woven as a single piece by three-dimensional weaving to make a closed box-structure platform out of composite material for a turbine engine fan | Emerging Cross-Sectional Technologies | 3 | Active |
| US9802869B2 | Method for manufacturing an oxide/oxide composite material turbomachine blade provided with internal channels | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US9150948B2 | Method for manufacturing an integral rotationally symmetrical metal part including a reinforcement consisting of ceramic fibers | Emerging Cross-Sectional Technologies | 2 | Active |
| US10328604B2 | Method for manufacturing a refractory part made of composite material | Mechanical Engineering; Lighting; Heating | 2 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.