Impact wing arrangement for aircraft, has oscillatory impact wing, where oscillation serves in manner such that energy content, effect direction or temporal development of effect direction or force impact are influenced by control

摘要

The arrangement has oscillatory impact wings (2) with backward and forward movement held or broken by an adjustable drive i.e. electric motor (5). A momentary position or a frequency of the wing oscillation is close to the information. The information is supplied from a sensor device, and the oscillation serves in a manner such that energy content, effect direction or temporal development of the effect direction or a force impact are influenced by a control in order to approximate the resulting amplitude or frequency of the wing oscillation to a value given by the control.