Christophe Scholtes
11Patents
2h-index
13Co-inventors
43Inventor score
Filing activity: Nov 12, 2014 → Oct 1, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US10598191B2 | Vane for turbomachinery, such as an aircraft turbojet or turbofan engine or an aircraft turboprop engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US10738650B2 | Device for deicing a splitter nose and inlet guide vanes of an aviation turbine engine | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10138745B2 | Sealing system with two rows of complementary sealing elements | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10273967B2 | Compressor shroud comprising a sealing element provided with a structure for entraining and diverting discharge air | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11585230B2 | Assembly for a turbomachine | Emerging Cross-Sectional Technologies | 1 | Active |
| US11566538B2 | Internal turbomachine casing having improved thermal insulation | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11859502B2 | Variable-pitch stator vane comprising aerodynamic fins | Emerging Cross-Sectional Technologies | 0 | Active |
| US11105262B2 | Turbomachine comprising an air collection circuit | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11248486B2 | Aircraft turbine-engine module casing, comprising a heat pipe associated with a sealing ring surrounding a movable impeller of the module | Emerging Cross-Sectional Technologies | 0 | Active |
| US10975716B2 | Assembly forming a labyrinth seal for a turbomachine comprising an abradable material and inclined fins | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10683805B2 | Anti-icing system for a turbine engine vane | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.