发明名称 VENT STRINGER AND AIRCRAFT MAIN WING
摘要 A vent stringer 20 is formed by a pair of ribs 21 rising in the direction perpendicular to an inner surface 11a of a wing panel 11, and a cover 22 provided in the tip end portions of the ribs 21. With rivets 23 unexposed to an outer surface 1 lb of the wing panel 11, a spark is prevented from occurring in a fuel tank 30, which is provided in a main wing 10, through the rivet 23 at the time of a lightning strike. Formed by being machined integrally with the wing panel 11, the rib 21 is formed with high accuracy so as to match the curved shape of the wing panel 11. The cover 22 has only to be formed by curving a strap member so as to match the shapes of the wing panel 11 and the ribs 21.
申请公布号 US2012187246(A1) 申请公布日期 2012.07.26
申请号 US201213353703 申请日期 2012.01.19
申请人 MOTOHASHI HIDETO;HOSOKAWA YOSHIFUMI;FUJII TOSHINARI;FUKUOKA TOSHIYASU;MITSUBISHI AIRCRAFT CORPORATION 发明人 MOTOHASHI HIDETO;HOSOKAWA YOSHIFUMI;FUJII TOSHINARI;FUKUOKA TOSHIYASU
分类号 B64C3/18;B64D37/04;B64D37/06;B64D45/02 主分类号 B64C3/18
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