FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed airmobile has body, engine, lift propulsors, and control mechanisms. Propulsors are arranged in body compartments on left and right sides. Every lift propulsor comprises rectangular body accommodating two identical lifting elements arranged one above the other. Every said lifting element comprises rectangular box with its open part directed upward. Some cylindrical hollow drums are fitted in bearing horizontally and in parallel. Drums of one pair are aligned. Quantity of drum pairs in one lifting element is odd. Gear is fitted on shaft of every drum while idle gear are fitted between gears to engage with two gears of two adjacent drums. Front and rear lifting propulsors are arranged to tilt in lengthwise plane when driven by hydraulic mechanism articulated with control pedals. Medium lifting propulsors of left and right sides are arranged to tilt in lengthwise plane and articulated with forward and reverse run control hydraulic mechanism.
EFFECT: expanded operating performances.
29 dwg
Title | Year | Author | Number |
---|---|---|---|
AEROMOBILE | 2015 |
|
RU2609541C1 |
AEROCAR | 2019 |
|
RU2715099C1 |
AEROMOBILE | 1999 |
|
RU2148004C1 |
STREAMLINED SHIP | 2011 |
|
RU2470808C1 |
AIRMOBILE | 2016 |
|
RU2617000C1 |
STREAMLINED SHIP | 2013 |
|
RU2538484C1 |
AERODYNAMIC AIRCRAFT | 2015 |
|
RU2609577C1 |
AERODYNAMIC VESSEL | 2019 |
|
RU2710040C1 |
AERODYNAMIC VESSEL | 1999 |
|
RU2149109C1 |
AERODYNAMIC CRAFT | 2005 |
|
RU2289519C1 |
Authors
Dates
2013-02-27—Published
2011-10-18—Filed