![Fluid flow control device for an aerofoil](/abs-image/US/2011/10/27/US20110260008A1/abs.jpg.150x150.jpg)
基本信息:
- 专利标题: Fluid flow control device for an aerofoil
- 专利标题(中):机翼流体流量控制装置
- 申请号:US13066736 申请日:2011-04-22
- 公开(公告)号:US20110260008A1 公开(公告)日:2011-10-27
- 发明人: John Jaycott Smith
- 申请人: John Jaycott Smith
- 专利权人: AERODYNAMIC RESEARCH INNOVATIONS HOLDINGS, LTD.
- 当前专利权人: AERODYNAMIC RESEARCH INNOVATIONS HOLDINGS, LTD.
- 优先权: GBGB1006979.7 20100427
- 主分类号: B64C23/06
- IPC分类号: B64C23/06 ; B64C3/58 ; F01D5/18
摘要:
A fluid flow control device for an aerofoil comprises an aerofoil-tip body of aerofoil shape, coupling apparatus adapted to couple one end of the body to an aerofoil, and a passive tip blowing assembly. The passive tip blowing assembly is provided at the other end of the aerofoil-tip and comprises a housing defining a fluid chamber and a vane of aerofoil shape. The fluid chamber extends along part of the chord-length of the body and has a fluid inlet and a fluid outlet. The vane is arranged along the chord of the aerofoil-tip, with its leading edge at the inlet and its trailing edge at the outlet. The aerofoil section of the aerofoil-tip has a higher camber than that of the aerofoil, which turns fluid flow across the low pressure side of the aerofoil towards the aerofoil-tip, so that the fluid flow mirrors the fluid flow across the high pressure side of the aerofoil.
摘要(中):
用于机翼的流体流动控制装置包括机翼形状的机翼尖端主体,适于将身体的一端连接到机翼的联接装置和被动尖端吹风组件。 被动顶吹组件设置在机翼尖端的另一端,并且包括限定流体室和机翼形叶片的壳体。 流体室沿主体的弦长的一部分延伸并且具有流体入口和流体出口。 翼片沿着机翼尖端的弦线布置,其前缘在入口处,其后缘处在出口处。 机翼尖翼的机翼部分具有比机翼更高的弯度,这使得流体流过机翼的低压侧朝向机翼尖端流动,使得流体流反映流过高压侧的流体流 的机翼。
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64C | 飞机;直升飞机 |
------B64C23/00 | 其他类目不包含的影响流经飞机表面的空气流 |
--------B64C23/06 | .通过产生旋涡 |