FIELD: transportation.
SUBSTANCE: airmobile comprises the housing, the engine, the vertical lift propellers, the variator, the horizontal movement propellers, the air rudders, the directional control system and the course-keeping ability control system, the landing device, the control mechanisms. Rotors identical in construction are mounted on the upper and the lower vertical driven shafts of each vertical lift propeller. Each rotor contains the upper and the lower cylindrical parts, between which the conical part is arranged. The lower cylindrical part at the lower butt portion has the cylindrical recess in which a cylindrical disc is fixed, having the fan blades at the outer butt surface. On the butt surface of the upper cylindrical rotor part a cylindrical recess is formed, and double radial series of vertical openings arranged at an equal distance from each other are drilled on its bottom. Each row of vertical openings is connected with the horizontal channel and the suction chamber of the injection pump. The pumps are fixed on the side surface of the upper cylindrical part, and their air intakes face in the direction of rotor rotation.
EFFECT: increasing the airmobile operation safety in flight and road conditions.
30 dwg
Title | Year | Author | Number |
---|---|---|---|
AEROCAR | 2019 |
|
RU2715099C1 |
AERODYNAMIC VESSEL | 2016 |
|
RU2611676C1 |
AEROMOBILE | 1999 |
|
RU2148004C1 |
AEROMOBILE | 2015 |
|
RU2609541C1 |
AIRMOBILE | 2011 |
|
RU2476353C1 |
VERTICAL LIFT PROPULSER | 2016 |
|
RU2616998C1 |
STREAMLINED SHIP | 2013 |
|
RU2538484C1 |
AERODYNAMIC CRAFT | 2005 |
|
RU2289519C1 |
AERODYNAMIC VESSEL | 2019 |
|
RU2710040C1 |
AERODYNAMIC AIRCRAFT | 2015 |
|
RU2609577C1 |
Authors
Dates
2017-04-19—Published
2016-05-04—Filed