AEROPLANO

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...

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Hauptverfasser: NARISCHKIN VITALIY JURYEVICH, EFANOV ALEXANDER GENADIEVICH, MATVEEV ANDREY IVANOVICH, SCHKOLIN VLADIMIR PETROVICH, KODOLA VALERIY GRIGORIEVICH, DEMCHENKO OLEG FEDOROVICH, PJATERNEV SERGEY VLADIMIROVICH, POPOVICH KONSTANTIN FEDOROVICH, AGAPOV SERGEY STEPANOVICH
Format: Patent
Sprache:ita
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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.