System for controlling an aircraft thrust reversal means
US12065986B2 · kind B2 · utility
Assignees
Inventors
Key dates
| Filing date | Dec 23, 2020 |
| Grant date | Aug 20, 2024 |
| Priority date | — |
| Expiry date | Dec 23, 2040 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG05D1/654
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
This system (36) for controlling an aircraft thrust reversal means comprises a reverse idle control means (38), a first detection means (31) configured to detect, when the reverse idle control is active, a condition for activation of the thrust reversal means, and an actuation means (52) configured to activate the thrust reversal means when the first detection means (31) detects a condition for activation of the thrust reversal means.It further comprises a second detection means (42, 44, 46, 48, 49) configured to detect a condition for activation of the reverse idle control, the control means (38) being configured to activate the reverse idle control when the second detection means (42, 44, 46, 48, 49) detects a condition for activating the reverse idle control.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.