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Improvements in and relating to solid boundary surfaces for fluid streams

机译:流体流的固体边界表面及其相关方面的改进

摘要

610,622. Reducing surface friction; boundary layer control. PRESTON, J. H., and THWAITES, B. April 11, 1946, No. 11197. [Class 4] Separation of the boundary layer of a fluid stream moving over a solid surface is prevented by forming the surface of porous material, the linear size and spacing of whose pores are small compared with the thickness of the fluid boundary layer, means being provided for applying suction to the fluid through the pores of the material. The pore size and spacing are of the order of one-hundredth of the boundary layer thickness and do not exceed onefiftieth thereof. The invention may be applied to aerofoils, propeller blades, blading for fans, compressors or turbines, aircraft bodies, engine nacelles, submarine hulls, or ducts or channels in which fluid flow is confined, such as diffusers for compressors and pumps, or the walls of wind tunnels. Suitable surface materials are sintered metal sheet or fine metal gauze bent to the desired shape, or a mould of the desired form may be sprayed to produce a porous metal layer. Fig. 1 shows a thick-section symmetrical aerofoil in which the upper and lower surfaces 5 of the rearward quarter-chord are of finely porous material, a space 6 being formed below the porous covering by an internal partition 7, the space being connected to a suction pump P by ducts D. In the embodiment according to Fig. 3, the porous surface layer 12 extends between the points 10 and 11 at the leading edge of a thin symmetrical aerofoil. In order to preserve laminar flow, the porous areas of the surfaces of the aerofoils may be more extensive than illustrated, and an aerofoil may even be provided with a porous surface throughout. Fig. 5 shows a symmetrical rectangular-section channel or duct in which the portions S of the walls W over which the velocity gradient is steeply negative are of porous material, to which suction is applied. Variation of the applied suction head may be obtained by partitioning the space below the porous area and applying different heads to the several compartments, or the degree of porosity of the surface material may be varied appropriately. Specification 479,598 is referred to, and the Provisional Specification refers to Specification 578,763.
机译:610,622。减少表面摩擦;边界层控制。 J. PRESTON和B. THWAITES,B。1946年4月11日,第11197号。[类别4]通过形成多孔材料的表面,线性尺寸和线形,可以防止在固体表面上流动的流体边界层分离。与流体边界层的厚度相比,其孔的间距较小,提供了用于通过材料的孔向流体施加吸力的装置。孔的尺寸和间距为边界层厚度的一百分之一,并且不超过边界层厚度的五十分之一。本发明可以应用于翼型,螺旋桨叶片,风扇,压缩机或涡轮的叶片,飞机主体,发动机机舱,潜艇船体,或流体被限制在其中的管道或通道,例如压缩机和泵的扩散器或墙壁。风洞。合适的表面材料是弯曲成所需形状的烧结金属板或细金属丝网,或者可以喷涂所需形式的模具以产生多孔金属层。图1示出了厚截面的对称翼型,其中后四分之一弦的上表面和下表面5由细微的多孔材料制成,在多孔覆盖物下方通过内部隔板7形成空间6,该空间连接至在根据图3的实施例中,多孔表面层12在薄的对称翼型的前缘的点10和11之间延伸。为了保持层流,机翼的表面的多孔区域可以比图示的更大,并且机翼甚至可以始终具有多孔的表面。图5示出了对称的矩形截面的通道或管道,其中壁W的速度梯度陡峭为负的部分S是多孔材料,对其施加了抽吸。可以通过在多孔区域下方分隔空间并将不同的吸头施加到多个隔室来获得施加的吸头的变化,或者可以适当地改变表面材料的孔隙度。请参考规范479,598,临时规范指的是规范578,763。

著录项

  • 公开/公告号GB610622A

    专利类型

  • 公开/公告日1948-10-19

    原文格式PDF

  • 申请/专利权人 JOSEPH HENRY PRESTON;BRYAN THWAITES;

    申请/专利号GB19460011197

  • 发明设计人

    申请日1946-04-11

  • 分类号B64C21/06;

  • 国家 GB

  • 入库时间 2022-08-24 02:37:34

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