winged aircraft whose maximum lift force may be altered by controllable wing components

摘要

WING AIRCRAFT WHOSE MAXIMUM LIFTING POWER CAN BE CHANGED BY CONTROLLED WING COMPONENTS The present invention relates to a winged aircraft whose maximum lift force can be altered by controllable wing components. By means of a regulator (20), which depends on flight state parameters and the actually measured load on the wings (10), wing components (11, 12) are actuated so that the maximum possible aerodynamic lift force do not exceed a desired upper limit value.