Systems and methods for deicing aircraft
US12391389B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Oct 7, 2022 |
| Grant date | Aug 19, 2025 |
| Priority date | — |
| Expiry date | Jan 19, 2043 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64D15/12
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
An aircraft includes external structures, and one or more thermal emitters integrated with one or more of the external structures. The one or more thermal emitters are configured to generate heat to deice the one or more external structures. The one or more thermal emitters are configured to receive electrical power from one or more of an auxiliary power unit of the aircraft, a power distribution system of the aircraft, one or more engines of the aircraft, or an external power cart that is separate and distinct from the aircraft.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.