Hybrid aircraft and landing launch/recovery system
US12304624B2 · kind B2 · utility
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0References
8Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jul 10, 2023 |
| Grant date | May 20, 2025 |
| Priority date | — |
| Expiry date | Oct 4, 2043 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64U70/93
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft includes a fuselage extending along a first x-axis and a wing assembly including a first wing an a second wing. A first power assembly of the aircraft includes a first propulsion element and a first electric motor while a second power assembly includes a second propulsion element and a second electric motor. The aircraft further includes a third power assembly positioned aft of the first power assembly and the second power assembly. The third power assembly includes a third propulsion element and an internal combustion engine.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.