Perpendicular start end aircraft, the drive of the rotary piston force machines with a continuous firing process and thrust direction has a swivel systems

摘要

The present invention provides a vtol - aircraft, which, in addition systems and control members for level flight, as well as start - / landing in front of gears also systems and control members for buoyancy and determination of the position of the vtol - aircraft in the case of vertical flight and via gear by the flights - vertically back to the level flight and has. The vtol - aircraft engines has, as for all flight operations two horizontally fixedly arranged in the form of a base jacket air current engines (1), in each case, with a three-stage rotary piston force of a machine (2) with a continuous firing process and a convertible device for pushing the direction of pivoting, as well as a third blade factory (10) with a rotary unit (12) and a mechanical gear mechanism for the rotation of the third blade (10), all of which are mounted on a bogie beam, for vertical take-off and determination of the position of the vtol - aircraft in the case of vertically -, horizontally - and by way of gear flights.