Turbojet engine nacelle including a single movable frame of a cascade thrust reverser and passages of ancillaries
US11549462B2 · kind B2 · utility
Assignees
Inventors
Key dates
| Filing date | May 27, 2020 |
| Grant date | Jan 10, 2023 |
| Priority date | — |
| Expiry date | May 27, 2040 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A turbojet engine nacelle having a cascade-type thrust reverser includes a movable frame surrounding a cold air flow path, guided axially by longitudinal rails fixed to an intermediate casing surrounding the cold air flow path and supporting cascades of thrust-reversal guide vanes and mobile rear cowls. The nacelle has a passage of ancillaries opening radially towards the outside of the movable frame, in a zone with no bearing structure passing radially across the cold air flow path. The movable frame is cut in an axial plane at the passage for the passage of ancillaries, and each edge of the cut of the movable frame is connected to the intermediate casing by a slide rail fitted on a longitudinal rail arranged each on one side of this passage.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.