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Wing comprising a leading edge slat and having means for preventing the transition to a turbulent boundary layer

机译:包括前缘板的翼,具有用于防止过渡到湍流边界层的装置

摘要

A wing comprising a fixed main part and a leading edge slat with upper and lower surface rear edges. The wing main part has an upper surface wall, which extends downstream and in alignment with the upper surface rear edge, and a lower surface wall, which extends downstream and in alignment with the lower surface rear edge. The wing has an upper surface gap between the end of the upper surface rear edge and the end of the upper surface wall and a lower surface gap between the end of the lower surface rear edge and the end of the lower surface wall. The wing has an upper surface channel downstream of the upper surface gap and a lower surface channel downstream of the lower surface gap. The wing comprises a suction system connected to each channel and arranged to suck the air contained in the channel.
机译:一种机翼,包括固定的主要部分和具有上表面和下表面后边缘的前缘板条。翼主部分具有上表面壁,其延伸下游并与上表面后边缘和下表面壁延伸,该下表面壁延伸,延伸下游并与下表面后边缘对齐。机翼在上表面后边缘的端部和上表面壁的端部之间具有上表面间隙和下表面后边缘的端部与下表面壁的端部之间的下表面间隙。该机翼具有上表面间隙下游的上表面通道和下表面间隙下游的下表面通道。该机翼包括连接到每个通道的抽吸系统,并且布置成吸入通道中的空气。

著录项

  • 公开/公告号US11027820B2

    专利类型

  • 公开/公告日2021-06-08

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS SAS;

    申请/专利号US201816180194

  • 发明设计人 MATHIAS FAROUZ-FOUQUET;

    申请日2018-11-05

  • 分类号B64C9/24;B64C21/06;B64C3/14;B64C3/28;

  • 国家 US

  • 入库时间 2022-08-24 19:06:00

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