主权项 |
1. A power engine with controlled thrust vector comprising:
at least one turbine placed orthogonal to a flow; the turbine having jet-circulation control of the flow of a gaseous medium around blades, the blades are made with at least one cavity for supplying the medium flow into slotted holes, the blades are airfoil ones, each output of each slotted hole is on a surface of the blade in an area behind a point of maximum thickness of a profile of the blade; the blades are is installed on a hollow shaft the shaft being able to rotate: the blades are positioned on the shall through hollow traverses with streamlined profiles, perpendicular to the shaft, and the hollow spaces of the blades, the traverses and the shaft are connected among themselves; and a fixed hollow distribution pipeline is coaxially placed within the hollow shaft with an annular gap between the shaft and the pipeline; the pipeline is made in as wall with holes through which a hollow space of the distribution pipe is connected with the hollow space of the traverses, and the pipeline is connected to a source of continuous or pulsed supply of the gaseous medium under pressure; wherein spark plugs air-fuel mixture are installed in each hollow space of each blade the spark plugs are connected to an induction coil ignition system, and the pipeline is connected to a supply system of fuel-air mixture. |