Torus turbine rotor drive for helicopters, multicopters or for turbo-fan aircraft

摘要

Drive unit for driving helicopters / multi-clusters and turbo-fan aircraft, which is fed by at least one twin-jet turbine jet engine (ZTL), in which the compressed sheath flow and / or jet exhaust stream (1) of a two-stream turbine air jet engine (ZTL) partially or completely through a pressure line connection, regulated in terms of volume and pressure, in a toroidal turbine housing (2), wherein the turbine is designed as a radial turbine or axial turbine, or a mixture of both and the gas fluid after power transmission to the turbine blades ( 3) is discharged to the outside (9), characterized in that in the interior of the turbine housing (2) the turbine blades (3) which are mounted on a running in the wall of the turbine housing freely rotating ring (5) via upstream guide vanes (4 ), wherein the ring (5) in its first function as a connecting component between the Turbinengehäuseinne Ren turbine blades (3) and lying outside the turbine housing to be driven rotor rim (6) and he serves at the same time due to its shape in a second function for mechanical and pressure-resistant stabilization of the turbine housing (2).