Hybrid power systems for different modes of flight
US11787537B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Jul 20, 2021 |
| Grant date | Oct 17, 2023 |
| Priority date | — |
| Expiry date | Dec 6, 2041 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T90/14
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A hybrid power system includes a first power source that includes an internal combustion engine, a second power source that includes a battery, and a power controller. The hybrid power system is included in a vertical takeoff and landing (VTOL) vehicle that flies in a transitional mode between a hovering mode and a forward flight mode. The power controller selects one or more of the first power source and the second power source to power a rotor included in the VTOL vehicle, including by: during a landing, the power controller determines when to have the second power source provide power to the rotor, in order to supplement power provided to the rotor by the first power source, based at least in part on one or more flight state variables associated with a flight computer.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.