Aircraft

Aircraft

The aircraft has main power units (1) and an auxiliary power unit (2) set at the rear portion of the fuselage (3), in which the auxiliary power unit is transversely set relative to the fuselage longitudinal axis, at the rear of the main power units. An independent claim is also included for an air i...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: NARISCHKIN, VITALIY JURYEVICH, EFANOV, ALEXANDER GENADIEVICH, POPOVICH, KONSTANTIN FEDOROVICH, PJATERNEV, SERGEY VLADIMIROVICH, DEMCHENKO, OLEG FEDOROVICH, AGAPOV, SERGEY STEPANOVICH, MATVEEV, ANDREY IVANOVICH, SCHKOLIN, VLADIMIR PETROVICH, KODOLA, VALERIY GRIGORIEVICH
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The aircraft has main power units (1) and an auxiliary power unit (2) set at the rear portion of the fuselage (3), in which the auxiliary power unit is transversely set relative to the fuselage longitudinal axis, at the rear of the main power units. An independent claim is also included for an air intake.