发明名称 SUBMERGED VORTEX GENERATOR
摘要 A vortex generator may include a depression in an aerodynamic surface, and a vortex generator leading edge located in the depression. The vortex generator leading edge may include a leading edge upper surface. The leading edge upper surface may be positioned at or below a tangent line defined at a location along the aerodynamic surface upstream of the depression relative to an oncoming local flow.
申请公布号 US2016031550(A1) 申请公布日期 2016.02.04
申请号 US201414448479 申请日期 2014.07.31
申请人 The Boeing Company 发明人 Harrison Neal A.;Dehaan Mark;Vassberg John C.;Sclafani Anthony J.
分类号 B64C23/06;B64C1/00 主分类号 B64C23/06
代理机构 代理人
主权项 1. A vortex generator, comprising: a depression in an aerodynamic surface; a vortex generator leading edge located in the depression and including a leading edge upper surface; and the leading edge upper surface positioned at or below a tangent line defined at a location along the aerodynamic surface upstream of the depression relative to an oncoming local flow.
地址 Chicago IL US