Electric aircraft and method of cooling a battery pack
US11728532B1 · kind B1 · utility
4Cited by
5References
10Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | May 27, 2022 |
| Grant date | Aug 15, 2023 |
| Priority date | — |
| Expiry date | May 27, 2042 |
Classification
- Technology area (CPC H)Electricity
- CPC primaryH01M2220/20
- WIPO fieldElectrical machinery, apparatus, energy
- WIPO sectorElectrical engineering
Abstract
In an aspect an electric aircraft is presented. An electric aircraft includes a consumable coolant reservoir housed within the electric aircraft. A consumable coolant reservoir is configured to contain a coolant. An electric aircraft includes a battery pack temperature control system including at least a thermal pathway. A thermal pathway is in thermal communication with a consumable coolant reservoir and at least a battery pack of an electric aircraft. A thermal pathway is configured to transport a thermal energy away from at least a battery pack.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.