发明名称 КРЫЛО ДОЗВУКОВОГО САМОЛЕТА
摘要 FIELD: aviation. ^ SUBSTANCE: straight or swept wing consists of center-wing section, outer wing panels, slats, flaps and flight control units. Vertical corrugations made on wing skin and front part of flaps, 15 mm in height are used for forming smooth profiled narrowing passages at ratio of inlet and outlet sections of 2:1. When flaps are in retracted position, said passages are closed; in flight and landing position of flaps, axes of outlet sections of passages coincide with direction of main flow on upper surface of wing. ^ EFFECT: improved characteristics of wing at large angles of attack. ^ 5 dwg
申请公布号 RU2004110694(A) 申请公布日期 2005.10.20
申请号 RU20040110694 申请日期 2004.04.09
申请人 ОАО "ЦК ФПГ "Российский авиационный консорциум" (RU) 发明人 Гапеев Даниил Иванович (RU);Гущин Андрей Александрович (RU);Климов Валентин Тихон ович (RU);Коробейников Виктор Васильевич (RU);Юдин Геннадий В чеславович (RU)
分类号 B64C9/16 主分类号 B64C9/16
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