FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to hybrid aircraft design. Proposed vehicle comprises sealed airframe 1 of the main module, power frame 3 secured over main airframe perimeter and equipped with built-in propulsors 4 with vertical thrust axes and the system of thrust deflection, wing 5 arranged on propulsor outer side. Sealed airframe 1 has top and bottom horizontal surfaces. Cargo attachment equipment is arranged at said top surface 8 while propulsors 9 with horizontal thrust axis are arranged at rear part in symmetry about horizontal tie 7. Sealed airframe centre has through vertical channels 11 wherein propulsors with vertical thrust vector closed by grates are installed. At bottom surface, on both sides of airframe horizontal axis 7, propulsors 6 with horizontal thrust axes and thrust deflection system are arranged. Proposed vehicle can comprises two aircraft integrated by common platform 25 and structural elements 26.
EFFECT: increased range, higher safety.
14 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
HYBRID AIRCRAFT | 2008 |
|
RU2385257C1 |
SEARCH-AND-RESCUE AIRCRAFT | 2007 |
|
RU2337855C1 |
HIGH-CAPACITY UNIVERSAL VEHICLE (VERSIONS) | 2015 |
|
RU2585380C1 |
AERO-SPACE TRANSPORT SYSTEM | 1994 |
|
RU2111147C1 |
METHOD OF FLIGHT AND AIRCRAFT TO THIS END | 2009 |
|
RU2410284C1 |
LENS-SHAPE HYBRID AIRSHIP | 2012 |
|
RU2546027C2 |
METHOD OF CREATING SYSTEM OF FORCES OF AIRCRAFT OF AEROPLANE CONFIGURATION AND GROUND-AIR AMPHIBIOUS VEHICLE FOR IMPLEMENTING THIS METHOD | 1998 |
|
RU2127202C1 |
AEROSTATIC AIRBORNE VEHICLE (VERSIONS) | 2011 |
|
RU2511500C2 |
GROUND-AIR AMPHIBIOUS VEHICLE | 1990 |
|
RU2068345C1 |
HIGH-ALTITUDE GUIDED AEROSTATIC FLYING VEHICLE | 1994 |
|
RU2111146C1 |
Authors
Dates
2015-03-10—Published
2012-09-06—Filed