Gregory Albet
14Patents
3h-index
18Co-inventors
53Inventor score
Filing activity: Jun 19, 2012 → Mar 2, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8733501B2 | Method for producing an acoustic treatment panel | Emerging Cross-Sectional Technologies | 15 | Active |
| US8991054B2 | Process for the production of a panel for the acoustic treatment incorporating the frost treatment function with hot air | Emerging Cross-Sectional Technologies | 4 | Active |
| US10676203B2 | Air input structure for an aircraft nacelle | Emerging Cross-Sectional Technologies | 4 | Active |
| US9388767B2 | Panel for the acoustic treatment comprising hot air ducts and at least one stabilization chamber | Emerging Cross-Sectional Technologies | 3 | Active |
| US9353648B2 | Panel for the acoustic treatment comprising hot air ducts and at least one annular channel | Emerging Cross-Sectional Technologies | 3 | Active |
| US11293302B2 | Anterior part of a nacelle of an aircraft propulsion unit having a shock absorbing element | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10836503B2 | Air intake structure for an aircraft nacelle | Emerging Cross-Sectional Technologies | 1 | Active |
| US11643967B2 | Nacelle air intake provided with a mixed ice protection system | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11518526B2 | Aircraft engine nacelle comprising an anti-icing protection system | Emerging Cross-Sectional Technologies | 1 | Active |
| US11073081B2 | Air inlet lip of an aircraft engine comprising a de-icing system | Emerging Cross-Sectional Technologies | 0 | Active |
| US11161620B2 | Aircraft nacelle with rotary fan cowling incorporating an access hatch | Performing Operations; Transporting | 0 | Active |
| US12030659B2 | Anterior part of a nacelle for an aircraft propulsion assembly, whose front frame is connected to an outer wall without penetrating it | Performing Operations; Transporting | 0 | Active |
| US11407522B2 | Air inlet, nacelle, propulsive assembly and aircraft with grooved lip | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11643216B2 | Aircraft engine nacelle comprising a system of ice protection | Emerging Cross-Sectional Technologies | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.