发明名称 KRUEGER FLAP ASSEMBLY SYSTEMS AND METHODS
摘要 Systems and methods according to one or more embodiments are provided for a Krueger flap (104) assembly with dual Krueger seal assemblies (310,312). In certain embodiments, the dual Krueger seal assemblies (310,312) may seal a space between a Krueger flap main body (104) and an aircraft engine (108). Further seals may be provided to seal any gaps between the dual Krueger seal assemblies (310,312). In certain embodiments, one or both of the dual Krueger seal assemblies (310,312) may include centrally grounded springs (418a,418b,420a,420b). The dual Krueger seal assemblies may include a plurality of springs supporting each Krueger seal assembly.
申请公布号 EP3112259(A1) 申请公布日期 2017.01.04
申请号 EP20160169854 申请日期 2016.05.17
申请人 The Boeing Company 发明人 SALMON, Huw James;GOMEZ, Roberto J.
分类号 B64C3/50;B64C7/02;B64C9/24 主分类号 B64C3/50
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