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.
Type:
Grant
Filed:
September 29, 1994
Date of Patent:
June 18, 1996
Assignee:
Aerospatiale Societe Nationale Industrielle