Thrust reverser comprising a single actuator for controlling a mobile cowling
US12018629B2 · kind B2 · utility
0Cited by
7References
8Claims
0Family size
Assignee
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Key dates
| Filing date | Sep 2, 2020 |
| Grant date | Jun 25, 2024 |
| Priority date | — |
| Expiry date | Sep 2, 2040 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A thrust reverser for an aircraft propulsion assembly, this reverser including a mobile annular external structure, a single actuator for controlling the position of this mobile external structure and a device for guiding the mobile external structure when changing its position. The actuator and the guiding device are housed in a fairing of a pylon of the propulsion assembly to a wing or fuselage of the aircraft.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.