发明名称 |
Low Noise Wing Slat System With Deployable Wing Leading Edge Elements |
摘要 |
Concepts and technologies described herein provide for a low noise aircraft wing slat system. According to one aspect of the disclosure provided herein, a cove-filled wing slat is used in conjunction with a moveable leading edge element of an aircraft wing to provide a high lift system. The moveable leading edge element may include a one-piece or two-piece panel that retracts within the aircraft wing to accommodate the cove-filled slat in the stowed position. Upon deployment of the cove-filled slat, the moveable leading edge element deploys outward to create a continuous outer mold line shape with the wing.
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申请公布号 |
US2011240803(A1) |
申请公布日期 |
2011.10.06 |
申请号 |
US20100751419 |
申请日期 |
2010.03.31 |
申请人 |
SHMILOVICH ARVIN;YADLIN YORAM |
发明人 |
SHMILOVICH ARVIN;YADLIN YORAM |
分类号 |
B64C3/50 |
主分类号 |
B64C3/50 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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