FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the designs of multi-propeller aircraft for vertical take-off and landing. Airborne vehicle of horizontal flight with vertical take-off and landing includes two and more spaced longitudinal bearing elements, two and more horizontal wings arranged along longitudinal axis of aircraft, multimotor power plant. Horizontal wing consists of parts that are cantilever mounted on outer sides of longitudinal bearing elements. Power plant consists of four and more engines with air propellers, which are installed at fixed angle to vertical plane in two and more rows relative to longitudinal axis of aircraft. Aircraft carrying platform comprises two and more spaced longitudinal bearing elements connected to rigid closed power circuit by means of two and more transverse elements, which do not have aerodynamic bearing planes.
EFFECT: ensuring stability of flight of aircraft during transition from vertical flight mode to horizontal flight and back.
2 cl, 8 dwg
Title | Year | Author | Number |
---|---|---|---|
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2015 |
|
RU2605466C1 |
MODULAR CONSTRUCTION OF AN UNMANNED AERIAL VERTICAL FOR VERTICAL TAKE-OFF AND LANDING | 2017 |
|
RU2681423C1 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2700154C1 |
UNMANNED AERIAL VEHICLE OF VERTICAL TAKE-OFF AND LANDING AND METHOD OF MANUFACTURING THEREOF | 2023 |
|
RU2819460C1 |
CONVERTIBLE VERTICAL TAKE-OFF AND LANDING AIRCRAFT (VERSIONS) | 2014 |
|
RU2550589C1 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2742496C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH HYBRID POWER PLANT | 2017 |
|
RU2724940C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2014 |
|
RU2574873C1 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 1998 |
|
RU2141432C1 |
VERTICAL TAKEOFF AND LANDING FLYING VEHICLE | 2003 |
|
RU2244661C2 |
Authors
Dates
2019-07-02—Published
2018-10-11—Filed