Pierre Caruel
57Patents
6h-index
47Co-inventors
68Inventor score
Filing activity: Mar 28, 2008 → Sep 12, 2022
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US8840061B2 | Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut | Emerging Cross-Sectional Technologies | 9 | Active |
| US9249756B2 | Assembly for an aircraft turbojet engine comprising a thrust reversal cowl | Performing Operations; Transporting | 9 | Active |
| US9562595B2 | Double-acting linear actuator | Emerging Cross-Sectional Technologies | 8 | Active |
| US9366201B2 | Cascade-type thrust reverser with one-piece mobile cowl | Emerging Cross-Sectional Technologies | 8 | Active |
| US8584363B2 | Method for making an acoustic panel for the air intake lip of a nacelle | Emerging Cross-Sectional Technologies | 6 | Active |
| US10532820B2 | Device for de-icing the inlet of a nacelle of an aircraft engine, method for producing such a de-icing device, and aircraft engine nacelle provided with such a de-icing device | Performing Operations; Transporting | 6 | Active |
| US10294822B2 | Turbine engine nacelle fitted with a heat exchanger | Emerging Cross-Sectional Technologies | 5 | Active |
| US9074554B2 | Reverse thrust device | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US9390704B2 | Method of manufacturing a sound absorbing panel | Emerging Cross-Sectional Technologies | 5 | Active |
| US9677502B2 | Nacelle thrust reverser and nacelle equipped with at least one reverser | Mechanical Engineering; Lighting; Heating | 5 | Active |
| US8448896B2 | Guiding system for aircraft nacelle maintenance | Performing Operations; Transporting | 4 | Active |
| US8430203B2 | Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11614052B2 | Active toggle lock for a thrust reverser of an aircraft nacelle | Fixed Constructions | 2 | Active |
| US9969499B2 | Nacelle for an aircraft turbojet engine with an extended front lip | Emerging Cross-Sectional Technologies | 2 | Active |
| US9476383B2 | Aircraft turbojet engine thrust reverser with a reduced number of latches | Emerging Cross-Sectional Technologies | 2 | Active |
| US9587583B2 | Turbojet engine nacelle having a variable nozzle | Emerging Cross-Sectional Technologies | 2 | Active |
| US8800262B2 | Thrust reverser for a turbofan engine nacelle | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US11549462B2 | Turbojet engine nacelle including a single movable frame of a cascade thrust reverser and passages of ancillaries | Emerging Cross-Sectional Technologies | 1 | Active |
| US8985508B2 | Suspension assembly for an aircraft turbojet engine | Emerging Cross-Sectional Technologies | 1 | Active |
| US9169805B2 | Thrust inverter with translatable cascade vanes having detachable front frame | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10190538B2 | Thrust reverser device | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US10125683B2 | De-icing and conditioning device for an aircraft | Emerging Cross-Sectional Technologies | 1 | Active |
| US9003770B2 | Nacelle rear assembly for turbojet engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9777598B2 | Flattened nacelle of a turbojet engine | Mechanical Engineering; Lighting; Heating | 1 | Active |
| US9410500B2 | Movable cascade turbojet thrust reverser having translatable reverser cowl causing variation in jet nozzle | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.