FIELD: transport.
SUBSTANCE: invention relates to electric aircraft. The aerial vehicle consists of two pivotally connected modules with common vertical axis: elevating-cruising module with power units and lifting rotors, and equipment, control and target load module inside which vibration damping column is installed vertically and mounted in horizontal strong frame. The elevating-cruising module is equipped with vibration damping two-degree articulation joint, connected with column and can be quickly changed in field conditions for the module with their more or less quantity, proportionally to the amount and purpose of the vehicle target load.
EFFECT: invention is focused on providing more comfortable conditions for target load operation.
4 dwg
Title | Year | Author | Number |
---|---|---|---|
LIGHT MULTIMODE AIRCRAFT | 2007 |
|
RU2348568C1 |
AIRCRAFT SYSTEM OF RESCUE OPERATIONS SUPPORT | 2008 |
|
RU2381959C1 |
MULTI-SCREW UNMANNED ROTORCRAFT | 2016 |
|
RU2611480C1 |
MULTIROTOR VTOL DRONE | 2014 |
|
RU2567496C1 |
MULTIROTOR UNMANNED HIGH-SPEED HELICOPTER | 2015 |
|
RU2598105C1 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2012 |
|
RU2518143C2 |
HEAVY-DUTY MULTIROTOR CONVERTIBLE ROTORCRAFT | 2013 |
|
RU2521121C1 |
UNMANNED COMBINED HELICOPTER | 2016 |
|
RU2629482C1 |
UNMANNED ROTORCRAFT WITH CROSS-SECTION PROPELLERS | 2016 |
|
RU2627963C1 |
MULTIPURPOSE MULTI-TILTROTOR HELICOPTER-AIRCRAFT | 2010 |
|
RU2448869C1 |
Authors
Dates
2010-11-10—Published
2009-01-30—Filed