FIELD: transport.
SUBSTANCE: set of invention relates to aircraft engineering. Proposed method consists in using lifting-bearing turbofans with gas drive from turbojet engines, while horizontal flight is performed by turbojet or piston engines with longitudinal thrust vector with respect to aircraft. Aircraft flight is controlled by elevation and vertical rudders. High-speed aircraft-turbocraft comprises airframe, turbojet engines, lifting-bearing turbofans with gas drive from turbojet engines arranged along aircraft sides or above airframe. High-speed increased load-lifting capacity aircraft comprises combined flight complex consisting of aerodynamic control surface, lifting-bearing variable thrust vector turbofans, turbojet or piston engines, and has-jet rudders. Turbofan engines can be used as gas generators.
EFFECT: reduced drag and take-off-and landing run time.
6 cl, 4 dwg
