AIRCRAFT Russian patent published in 2006 - IPC B64D17/80 

FIELD: aeronautical engineering.

SUBSTANCE: proposed aircraft has fuselage with cabin, wing, tail unit, brake and descent parachute packs, rudder and elevator control sections, electrical circuit and hydraulic line. Fuselage is made in form of two separable parts which are telescopically interconnected. Front part has cabin and insert embedded in rear end as shoulder. Rear part has insert with shoulder embedded in front end. Rudder and elevator control units are made in form of two separable sections which are engageable by means of gear train. Descent parachute pack is located on side of cabin of fuselage front part; remotely controlled charging unit is connected to rear end at level of center of insert of fuselage rear part.

EFFECT: enhanced safety of pilot.

13 dwg