Aircraft propulsion unit comprising a nacelle and a turbomachine independently supported by a wing, fuselage or tail element
US12246846B2 · kind B2 · utility
0Cited by
2References
11Claims
0Family size
Assignee
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Key dates
| Filing date | Nov 2, 2021 |
| Grant date | Mar 11, 2025 |
| Priority date | — |
| Expiry date | Dec 16, 2041 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C30/00
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A propulsion unit for an aircraft, includes a support structure, a nacelle and a turbomachine. The support structure is configured to independently support, on the one hand, the turbomachine and, on the other hand, preferably by a cradle, an air inlet and/or a rear section of the nacelle.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.