FIELD: aviation.
SUBSTANCE: proposed aircraft has fuselage, two half-wings, jet engine, vertical and horizontal stabilizers with rudder and elevator and landing gear. Each half-wing has Y-shaped passages inside it which are located in parallel relative to each other along span of half-wing; each passage has main passage of rectangular section mounted vertically; its inlet opening is located on lower surface of half-wing. In upper part main passage is branched-off into two blind passages of the same section.
EFFECT: possibility of forming additional lifting force on half-wings.
10 dwg
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 | RU2287454C1 | 
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| AIRCRAFT WITH PLATE-TYPE WING | 2000 | 
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| AIRCRAFT | 1999 | 
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| COMBINED CONFIGURATION AIRCRAFT WITH GAS-TURBINE ENGINE | 2000 | 
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| INCREASE-LIFT-WING AIRCRAFT | 2008 | 
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| AIRCRAFT WITH LIFTING FUSELAGE | 1999 | 
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| TRANSPORT AIRCRAFT | 2006 | 
 | RU2320518C1 | 
Authors
Dates
2006-10-10—Published
2005-04-18—Filed