FIELD: transportation.
SUBSTANCE: winged surface effect vehicle of "airplane" pattern comprises fuselage, on which small extension wing is installed with rectangular shape in plan. In tail part there are two vertical tails are installed with stabiliser and engines joined at ends of vertical tails. Center of winged surface effect vehicle located in front of center of pressure of small extension wing is located in zone of value of parametres 
and 
which provide stability for winged surface effect vehicle at all altitudes of flight above surface and at a distance from surface. Inside fuselage an additional engine may be installed for creation of static air cushion and drive of hydrojet device mechanism.
EFFECT: invention makes it possible to reduce weight of structure, to increase aerodynamic quality and to improved longitudinal balancing and course-keeping ability.
2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SELF-STABILISING WINGED SURFACE EFFECT VEHICLE | 2007 |
|
RU2368522C2 |
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| SELF-STABILIZING WINS-IN-GROUND-EFFECT CRAFT | 2003 |
|
RU2224671C1 |
| METHOD OF COMPLEX IMPROVEMENT OF AERODYNAMIC AND TRANSPORT CHARACTERISTICS, RAM WING MACHINE FOR IMPLEMENTATION OF NAMED METHOD (VERSIONS) AND FLIGHT METHOD | 2010 |
|
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| HOVERCARFT | 2012 |
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|
RU2543431C1 |
| SELF-STABILISING HOVERCRAFT | 2008 |
|
RU2424137C2 |
| METHOD OF STABILIZATION OF WING-IN-GROUND EFFECT CRAFT AND WING-IN-GROUND EFFECT CRAFT FOR REALIZATION OF THIS METHOD | 1995 |
|
RU2097269C1 |
