AIRCRAFT (VERSIONS) Russian patent published in 2013 - IPC B64C30/00 B64C7/02 

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering, particularly, to supersonic airliner air intakes. In compliance with first version, aircraft comprises wing, fuselage, at least one turbojet engine arranged at fuselage tail. Turbojet air intake has two channels, one arranged atop the fuselage and another located at fuselage tail bottom. In compliance with second version, aircraft comprises two turbojets arranged at fuselage tail, one above the other in aircraft mirror plane. Top turbojet air intake is located on fuselage hose top while bottom air intake is arranged at fuselage nose bottom. Generator of compression shocks in said air intakes represents fuselage nose section compose of horizontal multistage wedge. In compliance with third version, aircraft incorporates, at least, one turbojet arranged in nacelle located under the wing. Aircraft fuselage is secured to its wing by said nacelle. Turbojet engines are provided with air intakes incorporating generator of compression shocks representing common vertical wedge.

EFFECT: possibility to make versatile supersonic airliners.

9 cl, 16 dwg