Systems, methods, and mechanical designs for inverters for EVTOL aircraft
US12122527B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Mar 29, 2024 |
| Grant date | Oct 22, 2024 |
| Priority date | — |
| Expiry date | Mar 29, 2044 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldElectrical machinery, apparatus, energy
- WIPO sectorElectrical engineering
Abstract
An electrical propulsion system for a vertical take-off and landing (VTOL) aircraft comprises an electrical motor assembly and an inverter assembly. The inverter assembly comprises a housing, a capacitor assembly, at least one printed circuit board assembly (PCBA), and a plurality of positioning pins. The capacitor assembly comprises a center hole, at least one capacitor, a capacitor housing having at least one busbar, and a plurality of through holes in the capacitor housing. The capacitor assembly and the at least one PCBA are positioned inside the housing. The plurality of positioning pins pass through the through the plurality of through holes of the capacitor housing and the at least one PCBA and are connected to the housing.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.