the soaring ribs met for dimension wing or stabilizer aircraft

摘要

the application describes a node soaring ribs met for torsion wing or stabilizer of an aircraft.the invention includes a central hub element extending between the front and rear u043bu043eu043du0436u0435u0440u043eu043du043eu043c u043bu043eu043du0436u0435u0440u043eu043du043eu043c torsion, a set of vertical u043fu043eu0434u043au0440u0435 u043fu043bu044fu044eu0449u0438u0445 elementslocated in the range between the upper and lower u043eu0431u0448u0438u0432u043au043eu0439 u043eu0431u0448u0438u0432u043au043eu0439 torsion.the supporting element has a first side (in the direction of the front u043bu043eu043du0436u0435u0440u043eu043du0430, and second side shelf, running in the direction of the u0434u043du0435u0433u043e u043bu043eu043du0436u0435u0440u043eu043du0430.the side shelves extend from opposite sides of the vertical body and are attached to the central element of their soaring ribs met, u043fu0440u0438u043bu0435u0433u0430u044f lateral sides to his u043fu043bu043eu0441u043a guests.