Guy Lapergue
18Patents
6h-index
28Co-inventors
66Inventor score
Filing activity: Sep 3, 1986 → Oct 13, 2005
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US4730453A | Afterburner fuel injection system | Mechanical Engineering; Lighting; Heating | 13 | Expired |
| US6966189B2 | System for sealing the secondary flow at the inlet to a nozzle of a turbomachine having a post-combustion chamber | Emerging Cross-Sectional Technologies | 10 | Expired |
| US5676312A | Seal for a variable geometry nozzle | Mechanical Engineering; Lighting; Heating | 10 | Expired |
| US7322180B2 | Turbo-jet engine with fan integral with a drive shaft supported by first and second bearings | Mechanical Engineering; Lighting; Heating | 9 | Expired |
| US4724671A | Device for connecting a burner ring or flame holder to an afterburner duct of a turbojet engine | Mechanical Engineering; Lighting; Heating | 8 | Expired |
| US7213393B2 | Device for supplying cooling air to exhaust nozzle flaps | Emerging Cross-Sectional Technologies | 7 | Expired |
| US6360527B1 | Axisymmetric, converging-diverging exhaust nozzle swiveled by a guided ring | Emerging Cross-Sectional Technologies | 5 | Expired |
| US5359851A | Variable geometry exhaust nozzle for a turbojet engine | Mechanical Engineering; Lighting; Heating | 5 | Expired |
| US7296397B2 | Ventilation system for a convergent divergent exhaust nozzle | Emerging Cross-Sectional Technologies | 4 | Expired |
| US5494221A | Variable geometry turbojet engine exhaust nozzle | Emerging Cross-Sectional Technologies | 4 | Expired |
| US6327846A | Universal-joint vectoring system for a turbojet-engine exhaust nozzle | Mechanical Engineering; Lighting; Heating | 4 | Expired |
| US6993914B2 | Convergent-divergent turbojet nozzle | Emerging Cross-Sectional Technologies | 4 | Expired |
| US6375095B1 | Swiveling, converging-diverging, axisymmetric exhaust nozzle | Mechanical Engineering; Lighting; Heating | 3 | Expired |
| US7322181B2 | Turbofan engine with the fan fixed to a drive shaft supported by a first and a second bearing | Mechanical Engineering; Lighting; Heating | 3 | Expired |
| US7938230B2 | Device for lubricating a component in an assembly of parts | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US6349539B1 | Axisymmetric, converging-diverging, jet-deflecting turbojet-engine exhaust-nozzle | Mechanical Engineering; Lighting; Heating | 1 | Expired |
| US7340882B2 | Turbomachine with means for axial retention of the rotor | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US7520135B2 | Variable-section turbomachine nozzle | Mechanical Engineering; Lighting; Heating | 0 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.