发明名称 Airflow interrupting devices
摘要 <p>A flow interrupting device may cause a flow to separate from a wingtip device at a desired angle of attack. The flow interrupting device may be coupled to a leading edge of a wingtip device where a flow disruptor may be configured to alleviate a load on the wingtip device. The flow disrupter may comprise an edge that extends into a boundary layer at a threshold angle of attack that may disrupt the boundary layer and cause a flow to separate from the wingtip device. This separated flow may reduce stresses experienced by the wingtip device and wing during various flight conditions where a transverse flow is encountered. 6020350_1 (GHMatters) P98832.AU BELAG N K C) Co~</p>
申请公布号 AU2014271302(A1) 申请公布日期 2015.06.18
申请号 AU20140271302 申请日期 2014.12.04
申请人 TAMARACK AEROSPACE GROUP, INC. 发明人 GUIDA, NICHOLAS R.
分类号 B64C21/00;B64C23/00 主分类号 B64C21/00
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