Vorrichtung zur Einstellung der Schieberollmoment-Daempfung von Flugzeugen

摘要

1281753 Adjusting dihedral effect MITSUBISHI JUKOGYO KK 1 July 1969 [1 July 1968] 33261/69 Heading B7W A surface 4 has a fixed location on and protrudes from a pod 3 mounted on the tip of an aircraft wing 2, and, at least in part, is located forward of the trailing edge of the wing 2. Depending on its position on the pod the surface 4 increases or decreases the dihedral effect. The surface 4 may be integral with the pod 3, hinged to the pod, or retractable into the pod and may be controlled from the cockpit of an associated aircraft.