Stephane Pierre Guillaume Blanchard
37Patents
7h-index
56Co-inventors
68Inventor score
Filing activity: May 20, 2004 → Apr 13, 2021
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8607454B2 | Method for producing a turbomachine blade made from a composite material | Emerging Cross-Sectional Technologies | 18 | Active |
| US8336317B2 | Ventilation for a turbine wheel in a turbine engine | Emerging Cross-Sectional Technologies | 11 | Active |
| US8282355B2 | Turbomachine rotor wheel having composite material blades | Emerging Cross-Sectional Technologies | 9 | Active |
| US8025483B2 | Balancing system for turbomachine rotor | Emerging Cross-Sectional Technologies | 9 | Active |
| US7866162B2 | Exhaust cone for channeling a stream of gas downstream from a turbine | Emerging Cross-Sectional Technologies | 8 | Active |
| US7117682B1 | Turbojet axisymmetric nozzle controlled hot flap shutter | Emerging Cross-Sectional Technologies | 7 | Expired |
| US9506355B2 | Turbine engine blade or vane made of composite material, turbine nozzle or compressor stator incorporating such vanes and method of fabricating same | Emerging Cross-Sectional Technologies | 7 | Active |
| US9605543B2 | Turbine engine blade made of composite material, and a method of fabricating it | Emerging Cross-Sectional Technologies | 7 | Active |
| US8757966B2 | Stationary vane assembly for a turbine engine having a reduced weight, and turbine engine comprising at least one such stationary vane assembly | Emerging Cross-Sectional Technologies | 6 | Active |
| US6964169B2 | Long life nozzle flap for aircraft turbojets | Emerging Cross-Sectional Technologies | 6 | Expired |
| US8070445B2 | Balancing system for turbomachine rotor | Emerging Cross-Sectional Technologies | 6 | Active |
| US8210498B2 | Gate valve for a system for circulating cooling air through a turbomachine | Emerging Cross-Sectional Technologies | 5 | Active |
| US8864458B2 | Fixed vane assembly for a turbine engine having a reduced weight, and turbine engine comprising at least one such fixed vane assembly | Emerging Cross-Sectional Technologies | 3 | Active |
| US8408009B2 | Cooling air bleed device in a turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US7168253B1 | Monobloc flameholder arm for an afterburner device of a bypass turbojet | Mechanical Engineering; Lighting; Heating | 3 | Expired |
| US7891073B2 | Method of assembling two parts, at least one of which is made of a composite, and insert for carrying out the assembly | Emerging Cross-Sectional Technologies | 3 | Active |
| US7886542B2 | Device for attaching a flame-arrestor arm to an afterburner casing and afterburner comprising such a device | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US7475547B2 | Convergent turbojet exhaust nozzle | Emerging Cross-Sectional Technologies | 2 | Active |
| US11299989B2 | Assembly for a turbine of a turbomachine comprising a mobile sealing ring | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US8448448B2 | Cooling air bleed device in a turbomachine | Emerging Cross-Sectional Technologies | 1 | Active |
| US8870531B2 | Turbomachine rotor having blades of composite material provided with metal labyrinth teeth | Emerging Cross-Sectional Technologies | 1 | Active |
| US9422818B2 | Gas turbine engine rotor wheel having composite material blades with blade-root to disk connection being obtained by clamping | Emerging Cross-Sectional Technologies | 1 | Active |
| US9194240B2 | Vibration damper comprising a peg between outer platforms of adjacent composite-material blades of a turbine engine rotor wheel | Emerging Cross-Sectional Technologies | 1 | Active |
| US10920609B2 | Turbine engine turbine assembly | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US8397513B2 | Device for tapping cooling air in a turbomachine | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.