发明名称 Elastomeric transition for aircraft control surface
摘要 Elastomeric transition sections (118, 124) are mounted between the upper and lower portions of a wing (100) and a control surface (102) hinged thereto. The elastomeric transition sections include elastomeric material (126) having a plurality of holes (128) formed therethrough. Flexible rods (134, 136) are secured to either the wing or the control surface and extend through the holes (128) in the elastomeric material (126). The elastomeric transition sections provide a smooth aerodynamic transition between the wing and the control surface while permitting the control surface to pivot about the hinge axis (108) to perform the control function.
申请公布号 AU6278496(A) 申请公布日期 1996.12.30
申请号 AU19960062784 申请日期 1996.06.07
申请人 NORTHROP GRUMMAN CORPORATION 发明人 JOSEPH B. DILLER;NICHOLAS F. MILLER JR.
分类号 B64C3/48 主分类号 B64C3/48
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