发明名称 FLAP ROLLER ARRANGEMENT, FLAP ASSEMBLY, AND METHOD FOR REMOVING A ROLLER ASSEMBLY FROM A FLAP FITTING
摘要 A flap roller arrangement for supporting a flap on a wing of an aircraft is disclosed herein. The flap roller arrangement includes, but is not limited to, a roller assembly that is configured for rolling engagement with a flap track of the wing and for engagement with a flap fitting. The flap roller arrangement further includes a retaining member that is removably coupled to the roller assembly. The roller assembly is configured to egress through an opening in the flap fitting in a direction away from the flap track. The retaining member is configured to obstruct egress of the roller assembly through the opening when the retaining member is coupled to the roller assembly. The roller assembly is enabled to egress through the opening when the retaining member is removed from the roller assembly.
申请公布号 CA2852969(C) 申请公布日期 2016.05.17
申请号 CA20122852969 申请日期 2012.10.22
申请人 GULFSTREAM AEROSPACE CORPORATION 发明人 GRIECO, JAMES R.;PAKHLEVANYAN, GARY
分类号 B64C3/58;B23P19/00;B64C3/50 主分类号 B64C3/58
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