INTEGRAL AND/OR MODULAR HIGH-SPEED AIRCRAFT Russian patent published in 2007 - IPC B64D33/02 B64D27/18 B64C30/00 B64C39/12 

FIELD: aviation.

SUBSTANCE: proposed aircraft may have rear section integrated with delta wing and fuselage narrowing backward for smooth distribution of area from front to rear section. Power plant includes engine, air intake and jet nozzle; power plant may be integrated with rear section. According to first version, inlet of air intake may be located under wing and nozzle outlet may be located on the wing or under it. S-shaped intake passage supplies air to integrated engine mounted in rear part. Aircraft may be provided with elevators mounted in rear part, elevons mounted on wing and front unit for pitch control mounted in front. Aircraft may be modular in construction for use of advantages between transonic and supersonic signs. Specification describes also method of manufacture of aircraft.

EFFECT: enhanced efficiency.

60 cl, 47 dwg