发明名称 AN AIRFRAME LEADING EDGE
摘要 An airframe leading edge part designed to be replaceable fixed to a structural portion which during use moves through the air. The airframe leading edge part includes first and second longitudinal joint edges adapted to fit the structural portion. At least one joint is provided between the structural portion and at least one of the longitudinal joint edges. The joint is adapted to break in the event of a object strikes and deforms the airframe leading edge part during use. The joint is designed to break at beforehand determined maximum joint strength of the joint. Also a repair method for exchanging a damaged leading edge.
申请公布号 EP2922752(A4) 申请公布日期 2017.01.25
申请号 EP20120888908 申请日期 2012.11.20
申请人 SAAB AB 发明人 NORDIN, Pontus;STRINDBERG, Göte
分类号 B64C3/28;B64C1/06;B64C1/12;B64C27/473;B64D45/00;F01D5/28 主分类号 B64C3/28
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