FIELD: air transport; manufacture of aeromobiles. SUBSTANCE: aeromobile has body, engine, propulsors for vertical take- off and control mechanisms. Propulsors are located on port starboard in compartment of body. Each propulsor has cylindrical housing with bearing journals on the outside. Reduction gear is mounted inside propulsor housing in its center portion. Drive shaft of reduction gear is received by hole of one of journals. Driven shaft of reduction hear is mounted vertically in bearings of propulsor housing. Secured separately on driven shaft are upper and lower groups of disks. Each disk may have smooth upper surface. Lower surface of disk may be provided with blind passages of round or square section. These passages may be located over concentric circles in even number in each of them. Front and rear vertical take-off propulsors are mounted for probable inclination in transversal plane by means of hydraulic mechanism kinematically linked with control pedals. Center port and starboard vertical take-off propulsors are mounted for probable inclination in longitudinal plane; they are kinematically linked with hydraulic control mechanism. EFFECT: improved service characteristics. 3 cl, 22 dwg
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Authors
Dates
2000-04-27—Published
1999-02-16—Filed