LIGHT MULTIMODE AIRCRAFT

FIELD: transportation; aviation. ^ SUBSTANCE: proposed aircraft has fuselage with lift-cruise fans, a cabin, flat-topped tail assembly and a gas-filled ski undercarriage with an adaptive pneumatic shock absorber. The fuselage is in form of an aerodynamic low-aspect wing, above the tail end of which...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	VORONKOV OLEG JUR'EVICH, VORONKOV JURIJ SERGEEVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AEROPLANES AIRCRAFT AMPHIBIOUS OR LIKE VEHICLES AVIATION CONVERTIBLE VEHICLES COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING VEHICLES FOR USE BOTH ON RAIL AND ON ROAD VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	FIELD: transportation; aviation. ^ SUBSTANCE: proposed aircraft has fuselage with lift-cruise fans, a cabin, flat-topped tail assembly and a gas-filled ski undercarriage with an adaptive pneumatic shock absorber. The fuselage is in form of an aerodynamic low-aspect wing, above the tail end of which there are controlled lattice wings, bordered on the end parts by a vertical fin, between the planes of which behind the lattice wings, there are controlled turning lift-cruise ducted fans. At the lower surface of the wing there are diffuser channels with control aileron-blades for lift-cruise fans. The aircraft can be controlled manually or automatically in accordance with synergetic laws of unity of adaptation and control processes. ^ EFFECT: increased safety, reliability and control efficiency in turbulent air conditions. ^ 15 dwg