Propulsion assembly for an aircraft, comprising a load bearer
US12344388B2 · kind B2 · utility
Assignee
Inventor
Key dates
| Filing date | Mar 8, 2023 |
| Grant date | Jul 1, 2025 |
| Priority date | — |
| Expiry date | Sep 19, 2043 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D27/12
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A propulsion assembly is disclosed including a pylon, a turbomachine having an engine and a fan surrounded by a fan casing, a nacelle surrounding the engine and the fan casing, and including a load bearer positioned at the upper part of the nacelle, a forward fan mount between a frontal zone of the fan casing and a frontal zone of the load bearer, a rear pylon mount between the pylon and the load bearer, and a positioning assembly providing positioning between the fan casing and the load bearer. The propulsion assembly is configured to control the separations between the cowls mounted in a moveable manner on the load bearer and a nose cowl.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.