Patrick Boileau
40Patents
2h-index
42Co-inventors
57Inventor score
Filing activity: Nov 29, 1990 → Sep 8, 2023
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US5094480A | Pipe coupling with leakage draining means | Mechanical Engineering; Lighting; Heating | 12 | Expired |
| US11428190B2 | Grid-type thrust reverser for turbojet engine | Emerging Cross-Sectional Technologies | 2 | Active |
| US9587583B2 | Turbojet engine nacelle having a variable nozzle | Emerging Cross-Sectional Technologies | 2 | Active |
| US11840352B2 | Nacelle air intake and nacelle comprising such an air intake | Emerging Cross-Sectional Technologies | 1 | Active |
| US9151225B2 | Air intake structure for turbojet engine nacelle | Performing Operations; Transporting | 1 | Active |
| US12092026B2 | Nacelle air intake and nacelle comprising such an air intake | Emerging Cross-Sectional Technologies | 1 | Active |
| US10190538B2 | Thrust reverser device | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US11891185B2 | Nacelle for a propulsion assembly with a very high bypass ratio, comprising a removable and structural front internal structure | Emerging Cross-Sectional Technologies | 1 | Active |
| US11313323B2 | Propulsion unit for aircraft comprising an assembly box-type structure in the six o'clock position | Emerging Cross-Sectional Technologies | 1 | Active |
| US12103694B2 | Nacelle air intake and nacelle comprising such an air intake | Emerging Cross-Sectional Technologies | 1 | Active |
| US10458362B2 | Turbojet nacelle provided with a thrust reverser, including cut-outs to avoid the movable slat of an aircraft wing | Emerging Cross-Sectional Technologies | 0 | Active |
| US12110843B2 | Thrust reverser comprising movable grids and cowls assembled by recessing | Emerging Cross-Sectional Technologies | 0 | Active |
| US11834187B2 | Drive unit for an aircraft having lifting points, and carriages for supporting such a unit | Emerging Cross-Sectional Technologies | 0 | Active |
| US9995246B2 | Thrust reverser for nacelle of aircraft turbofan | Emerging Cross-Sectional Technologies | 0 | Active |
| US12258925B2 | Thrust reverser comprising pivoting half-assemblies and a connecting beam for the half-assemblies at the six o'clock position | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9856826B2 | Nacelle rear assembly for a turbojet engine comprising a suspension cradle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11542026B2 | Aircraft propulsion unit and method for ventilating an engine enclosure | Emerging Cross-Sectional Technologies | 0 | Active |
| US12221941B2 | Reverser with movable cascades for an aircraft propulsion assembly, comprising a system for limiting the buckling of an actuator of the reverser | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11512641B2 | Upper axial retention for a cascade-type thrust reverser with sliding vanes of D-shaped structure | Emerging Cross-Sectional Technologies | 0 | Active |
| US10633103B2 | Propulsion unit for an aircraft and method for opening a movable cowl of said propulsion unit | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US10309340B2 | Thrust reverser of a turbojet engine nacelle, comprising control cylinders of movable cowls and a variable secondary nozzle | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US11952963B2 | Thrust reverser with anti-buckling actuating system | Emerging Cross-Sectional Technologies | 0 | Active |
| US10641206B2 | Nacelle rear assembly for a turbojet engine comprising a cradle for a core-type mast | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US12378929B2 | Thrust reverser comprising fixed cascades and a sealing membrane | Mechanical Engineering; Lighting; Heating | 0 | Active |
| US9957056B2 | Propulsion unit for an aircraft | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.