Device and method for assisting in the management of an engine failure on an aircraft
US8155803B2 · kind B2 · utility
3Cited by
18References
9Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Feb 5, 2008 |
| Grant date | Apr 10, 2012 |
| Priority date | — |
| Expiry date | Feb 10, 2031 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG05D1/0072
- WIPO fieldMeasurement
- WIPO sectorInstruments
Abstract
A device and method for assisting in the management of an engine failure on an aircraft. The device automatically determines when an engine failure is detected, vectoring settings including speed, thrust and altitude settings designed to be implemented on the aircraft in such a manner as to allow it to fly to a particular airport.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.