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公开(公告)号：US20160319668A1
公开(公告)日：2016-11-03
申请号：US14698334
申请日：2015-04-28
申请人： The Boeing Company
CPC分类号： F01D5/141 , B63B1/06 , B63B1/36 , B63H25/38 , B64C3/26 , B64C2230/22 , F05D2220/323 , F05D2220/36 , F05D2240/30 , F05D2250/63 , F15D1/005 , Y02T70/121
摘要： A surface area of a structure is fabricated with a textured surface that reduces the surface wear rate or erosion caused by a high speed flow of fluid containing abrasive particles over the surface area. More particularly, a leading edge surface such as a rotor leading edge surface, an aircraft airfoil leading edge surface, a propeller leading edge surface, etc. is fabricated with a textured surface comprised of a plurality of grooves that alter or break up a high speed flow of fluid containing abrasive particles over the textured surface. The grooves are contacted by the high speed flow of fluid containing the abrasive particles and alter or break up the flow of fluid and abrasive particles and thereby reduce surface wear rate or erosion of the structure leading edge.
摘要翻译： 结构的表面区域被制造成具有纹理表面，其减小由表面积上含有磨料颗粒的流体的高速流动引起的表面磨损率或侵蚀。 更具体地，制造具有由多个凹槽组成的前缘表面，例如转子前缘表面，飞行器翼型件前缘表面，螺旋桨前缘表面等，其纹理表面改变或破坏高速 在磨砂表面上含有磨料颗粒的流体流。 凹槽通过含有磨料颗粒的流体的高速流动而接触，并改变或分解流体和磨料颗粒的流动，从而降低结构前缘的表面磨损率或腐蚀。
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公开(公告)号：US08997846B2
公开(公告)日：2015-04-07
申请号：US12254530
申请日：2008-10-20
申请人： Yan R. Kucherov , Graham Hubler
发明人： Yan R. Kucherov , Graham Hubler
CPC分类号： F28F13/12 , F15D1/005 , F15D1/009 , F28F3/04 , F28F13/02 , F28F13/185 , H05K7/20009 , Y10T137/2087 , Y10T137/2093
摘要： A heat dissipation system that includes a structure having a surface with a cavity recessed on the surface. A wing or channel causes a vortex to occur in the cavity. Destabilizers, such as projections or recesses are disposed on the sidewall of the cavity to disrupt the local surface boundary layer that forms in the cavity. Alternatively, a plurality of freely moving bead elements are disposed in the cavity to disrupt the local surface boundary layer. A cover can be included that prevents the bead elements from exiting the cavity.
摘要翻译： 一种散热系统，其包括具有凹陷在表面上的腔的表面的结构。 翼或通道导致在空腔中发生涡流。 诸如突起或凹陷之类的不稳定剂设置在空腔的侧壁上以破坏在空腔中形成的局部表面边界层。 或者，多个自由移动的胎圈元件设置在空腔中以破坏局部表面边界层。 可以包括防止胎圈元件离开空腔的盖子。
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3.发明申请公开(公告)号：US20070163757A1
公开(公告)日：2007-07-19
申请号：US10575129
申请日：2004-10-07
IPC分类号： F28F13/12
CPC分类号： F28F1/40 , B21C37/158 , F15D1/005 , F15D1/065 , F28F19/006
摘要： The invention relates in general to surfaces along which media, such as gases, liquids or multi-phase mixtures are flowing, especially to a device for transportation of a flowing medium and/or for heat exchange between a flowing medium and the device, and methods of producing and using such devices. Disclosed is a surface or layer having dimples, the edges of which are rounded, thereby forming a central dimple area and at least one curvature area for each dimple which continuously connects the dimple to the surrounding surface for reducing particle deposition and ice formation on a surface along which a medium flows.
摘要翻译： 本发明一般涉及诸如气体，液体或多相混合物流动的介质，尤其涉及用于运输流动介质和/或在流动介质和设备之间进行热交换的装置的表面，以及方法 生产和使用这些设备。 公开了具有凹坑的表面或层，其边缘是圆形的，从而形成中心凹坑区域和每个凹坑的至少一个曲率区域，其将凹坑连续地连接到周围表面，以减少表面上的颗粒沉积和冰层 中间流动。
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公开(公告)号：US06880476B2
公开(公告)日：2005-04-19
申请号：US10470514
申请日：2002-02-01
申请人： Fred Olsen , Hans Oigarden
发明人： Fred Olsen , Hans Oigarden
CPC分类号： B64C21/10 , B63B1/34 , B64C2230/26 , F15D1/005 , F15D1/12 , Y02T50/166 , Y02T70/121
摘要： Formations on the surface of bodies for reducing the drag relative to a medium which the body is located in or close to. The formations comprise a plurality of cavities (1,20,40,60). The surface in which the cavities are formed is closed. The cavity has a disruption edge (5,25,44,66) adjacent to the cavity, with the disruption edge located upstream of the cavity, so as to set the flowing medium most proximal to the surface into turbulence upon passing the disruption edge. The cavity has a maximum depth from the surface of at least approximately 2 mm.
摘要翻译： 用于减少相对于身体位于或靠近的介质的阻力的身体表面上的组合。 所述结构包括多个空腔（1,20,40,60）。 形成空腔的表面是封闭的。 空腔具有与空腔相邻的破裂边缘（5,25,46,66），其中破坏边缘位于空腔的上游，以便在通过破裂边缘时将最接近表面的流动介质设置成湍流。 空腔具有至少约2mm的表面的最大深度。
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公开(公告)号：US06006823A
公开(公告)日：1999-12-28
申请号：US59724
申请日：1998-03-13
申请人： Gennady Iraklievich Kiknadze , Ivan Alexandrovich Gachechiladze , Valery Grigorievich Oleinikov
发明人： Gennady Iraklievich Kiknadze , Ivan Alexandrovich Gachechiladze , Valery Grigorievich Oleinikov
摘要： The invention relates to hydroaerodynamics and to thermal physics and concerns devices to control the boundary and near wall layers in the flows of continuos media such as gases, liquids, their two-phase or multicomponent mixtures and the like, moving along ducts under no pressure or under pressure.
摘要翻译： 本发明涉及流体动力学和热物理学，并涉及控制连续介质流中诸如气体，液体，它们的两相或多组分混合物等的边界和近壁层的装置，在无压力下沿管道移动， 在压力之下。
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公开(公告)号：US09404370B2
公开(公告)日：2016-08-02
申请号：US13816975
申请日：2011-08-18
申请人： Timo Scheuermann , Stefan Ebert
发明人： Timo Scheuermann , Stefan Ebert
CPC分类号： F01D5/147 , F01D9/026 , F05D2220/40 , F05D2250/28 , F15D1/005 , F15D1/065
摘要： An exhaust-gas turbocharger component (10) having at least one flow-conducting component surface (11) and having a discontinuity structure (12) which is formed on the component surface (11). The discontinuity structure (12) has a multiplicity of punctiform depressions (13) which are arranged separately from one another on at least one part of the component surface (11).
摘要翻译： 具有形成在所述部件表面（11）上的至少一个导流部件表面（11）并且具有不连续结构（12）的废气涡轮增压器部件（10）。 不连续结构（12）具有多个点状凹陷（13），它们在部件表面（11）的至少一部分上彼此分开布置。
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7.发明授权Heat dissipation system with surface located cavities for boundary layer disruption 有权散热系统具有表面定位的空腔，用于边界层破坏公开(公告)号：US09080821B1
公开(公告)日：2015-07-14
申请号：US14663080
申请日：2015-03-19
发明人： Yan R. Kucherov , Graham K. Hubler
CPC分类号： F28F13/12 , F15D1/005 , F15D1/009 , F28F3/04 , F28F13/02 , F28F13/185 , H05K7/20009 , Y10T137/2087 , Y10T137/2093
摘要： A heat dissipation system that includes a structure having a surface with a cavity recessed on the surface. A wing or channel causes a vortex to occur in the cavity. Destabilizers, such as projections or recesses are disposed on the sidewall of the cavity to disrupt the local surface boundary layer that forms in the cavity. Alternatively, a plurality of freely moving bead elements are disposed in the cavity to disrupt the local surface boundary layer. A cover can be included that prevents the bead elements from exiting the cavity.
摘要翻译： 一种散热系统，其包括具有凹陷在表面上的腔的表面的结构。 翼或通道导致在空腔中发生涡流。 诸如突起或凹陷之类的不稳定剂设置在空腔的侧壁上以破坏在空腔中形成的局部表面边界层。 或者，多个自由移动的胎圈元件设置在空腔中以破坏局部表面边界层。 可以包括防止胎圈元件离开空腔的盖子。
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公开(公告)号：US20150082895A1
公开(公告)日：2015-03-26
申请号：US14037893
申请日：2013-09-26
发明人： Stephen Arthur Ifft
CPC分类号： G01L19/147 , F15D1/0005 , F15D1/005 , G01F1/46 , G01F15/00
摘要： A retractable flow conditioner that includes a body adapted for insertion into a fluid in a confined conduit upstream of a differential pressure measuring probe. The body has at least one flow conditioning element. The retractable flow conditioner also includes a mounting assembly attached to the body. The mounting assembly is configured to retractably mount the body into the confined conduit.
摘要翻译： 一种可伸缩流动调节器，其包括适于插入压差测量探头上游的限制导管内的流体的主体。 身体至少有一个流动调节元件。 可伸缩流动调节器还包括安装在主体上的安装组件。 安装组件被构造成将主体可收缩地安装到密闭导管中。
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公开(公告)号：US20120227853A1
公开(公告)日：2012-09-13
申请号：US13408650
申请日：2012-02-29
申请人： Andreas BAUER
发明人： Andreas BAUER
摘要： Fluid line and method of forming the fluid line. The fluid line includes a cylindrical inner surface having uniformly distributed recesses in the form of spherical sectors formed in the inner surface.
摘要翻译： 流体管线和形成流体管线的方法。 流体管线包括圆柱形内表面，其具有形成在内表面中的球形形状的均匀分布的凹部。
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10.发明授权公开(公告)号：US07628569B2
公开(公告)日：2009-12-08
申请号：US11995514
申请日：2005-07-12
申请人： Robi Bonilla Gris
发明人： Robi Bonilla Gris
IPC分类号： E02D5/60
CPC分类号： E02B17/0017 , B63B1/34 , B63B2021/504 , F15D1/005 , F15D1/12 , F16L1/123 , Y02T70/121
摘要： Sheath (20, 21) with specially designed artificial rugosity (18, 19), to be put on structures and objects (10) submerged in a flow (12) and leaning on a scourable bottom, such as piers and abutments of bridges, pipelines, and others. The rugosity diminishes the intensity of the secondary flow that occurs in the border of attack of the structure and also reduces the turbulent wake; as a result, there is a decrease in the local scour that can put the mentioned structures at risk. The sheath also reduces the drag force due to the relative movement of the structure (10) in relation to the liquid medium, so it can be applied to moving objects in a liquid medium at rest. The sheath may have an efficient streamlined profile that produces an additional decrease of the scour and the drag force; it may also include a mechanism to turn the sheath automatically, if the flow has variable direction.
摘要翻译： 护套（20,21）具有特别设计的人造粗糙度（18,19），被放置在淹没在流动（12）中的结构和物体（10）上，并倾斜在可冲洗的底部，例如桥墩和桥基，管道 ， 和别的。 粗糙度降低了在结构攻击边界发生的二次流的强度，并且还减少了湍流尾迹; 因此，可能会使上述结构处于危险中的地方冲刷减少。 由于结构（10）相对于液体介质的相对运动，护套还减小了阻力，所以可以将其施加到静止的液体介质中的移动物体上。 护套可以具有有效的流线型轮廓，其产生冲刷和牵引力的额外减少; 它还可以包括如果流动具有可变方向，则自动转动护套的机构。
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