Electrical flight control system for an airplane, with attitude protection on takeoff
US5527002A · kind A · utility
15Cited by
5References
8Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Sep 29, 1994 |
| Grant date | Jun 18, 1996 |
| Priority date | — |
| Expiry date | Sep 29, 2014 |
Classification
- Technology area (CPC G)Physics
- CPC primaryG05D1/0661
- WIPO fieldControl
- WIPO sectorInstruments
Abstract
According to the invention, attenuator means (8) are provided, making it possible to limit the rate of rotation of the airplane on takeoff, so as to avoid the tail of the airplane striking the ground and to reduce the dispersion of the rotation rates.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.