Aircraft propulsion assembly comprising at least one aerodynamic panel which is supported by at least one intermediate radial support, aircraft comprising at least one such propulsion assembly
US12319420B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | May 24, 2024 |
| Grant date | Jun 3, 2025 |
| Priority date | — |
| Expiry date | May 24, 2044 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF01D25/24
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A propulsion assembly comprising a fan casing and a nacelle which comprises an air inlet which is connected to the front end of the fan casing, an intermediate portion which is positioned around the fan casing and a rear portion which cooperates with the rear end of the fan casing. The intermediate portion comprises at least one aerodynamic panel which extends from a front edge which is attached to the air inlet as far as a rear edge which is attached to the rear portion and at least one intermediate radial support comprising an internal edge which is connected to the fan casing and an external edge which is connected to the aerodynamic panel, this panel comprising a front edge which is connected to the air inlet by a first connection system. Also an aircraft with such a propulsion assembly.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.