METHOD OF SHORT JUMP TAKE-OFF OF AIRCRAFT AND DEVICE FOR ITS REALIZATION

摘要

The invention relates to aviation, and more particularly to Stol. The aim of the invention is to reduce energy costs and artificial: for prison additional energy sources for performing hopping shortened takeoff. This is achieved by converting a portion of the kinematic energy dispersal yuschegos aircraft 1 in vertical pulse. In this case the energy of the rotating wheel perceive engages with a rotary coupling element, formed as a helical cam 4 with the friction working surface pivotally associated with the housing strut 1. The cam surface cooperates with the disc 3 is rigidly fastened to the wheel. Operating cam disc 4 contact with surface 3 is provided a turning mechanism 5. ri 2 f ly-7-yl. E che 00 to ON