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    Turbine blade with enhanced cooling and profile optimization
    4.
    发明授权
    Turbine blade with enhanced cooling and profile optimization 失效
    涡轮叶片具有增强的冷却和轮廓优化

    公开(公告)号：US5980209A

    公开(公告)日：1999-11-09

    申请号：US884091

    申请日：1997-06-27

    申请人： Vincent Anthony Barry ,  Brent A. Gregory ,  Nesim Abuaf

    发明人： Vincent Anthony Barry ,  Brent A. Gregory ,  Nesim Abuaf

    IPC分类号： F01D5/14 ,  F01D5/18 ,  F01D5/30

    CPC分类号： F01D5/141 ,  F01D5/187 ,  Y10S416/05

    摘要： A first-stage turbine blade includes an airfoil having a profile according to Table I. The airfoil has a plurality of cooling air passages extending linearly from the root portion to the tip portion of the airfoil. The blade includes a shank having a pair of cavities in communication through the blade dovetail with a plenum in the wheel space for supplying cooling air to the passages in the airfoil. The cooling passages in the airfoil terminate in a recess at the tip portion which has an opening adjacent the trailing edge of the airfoil and along the suction side to enable egress of cooling air into the hot gas stream on the low pressure side of the airfoil. The majority of the cooling passages are turbulated. Certain of those passages are arranged in rows lying adjacent to the pressure and suction sides of the airfoil.

    摘要翻译： 第一级涡轮机叶片包括具有根据表I的轮廓的翼型件。翼型件具有多个冷却空气通道，该冷却空气通道从翼部的根部直线延伸到翼型部分。 叶片包括具有一对空腔的柄，所述一对空腔通过叶片燕尾榫与在车轮空间中的增压室连通，用于向翼型中的通道供应冷却空气。 翼型件中的冷却通道终止在尖端部分处的凹部中，该凹部具有与翼型件的后缘相邻并且沿着吸力侧的开口，以使冷却空气能够排出到翼型的低压侧上的热气流中。 大部分冷却通道是混浊的。 这些通道中的某些通道排列成与翼型的压力和吸力侧相邻的排。

    Casting having an enhanced heat transfer, surface, and mold and pattern for forming same
    5.
    发明授权
    Casting having an enhanced heat transfer, surface, and mold and pattern for forming same 失效
    铸造具有增强的热传递，表面和模具以及用于形成它们的图案

    公开(公告)号：US06786982B2

    公开(公告)日：2004-09-07

    申请号：US10279654

    申请日：2002-10-24

    申请人： Ching Pang Lee ,  Wayne Charles Hasz ,  Nesim Abuaf ,  Robert Alan Johnson

    发明人： Ching Pang Lee ,  Wayne Charles Hasz ,  Nesim Abuaf ,  Robert Alan Johnson

    IPC分类号： C22C3800

    CPC分类号： B22C9/04 ,  B22C7/02 ,  B22C9/02 ,  B22D25/06

    摘要： A casting includes a heat transfer surface having a plurality of cavities. The plurality of cavities include a density of at least about 25 cavities per square centimeter to about 1,100 cavities per square centimeter resulting in increased surface area and therefore enhanced heat transfer capability. Also disclosed is a mold for forming a pattern for molding the casting. The mold includes a surface defining a portion of a chamber to which are attached a plurality of particles having an average particle size in a range of about 300 microns to about 2,000 microns.

    摘要翻译： 铸件包括具有多个空腔的传热表面。 多个空腔包括每平方厘米至少约25个腔体至每平方厘米约1,100个空腔的密度，导致增加的表面积并因此提高传热能力。 还公开了一种用于形成用于模制铸件的图案的模具。 模具包括限定室的一部分的表面，其中连接有平均粒度在约300微米至约2,000微米范围内的多个颗粒。

    Casting having an enhanced heat transfer, surface, and mold and pattern for forming same
    7.
    发明授权
    Casting having an enhanced heat transfer, surface, and mold and pattern for forming same 失效
    铸造具有增强的热传递，表面和模具以及用于形成它们的图案

    公开(公告)号：US06502622B2

    公开(公告)日：2003-01-07

    申请号：US10073590

    申请日：2002-02-12

    申请人： Ching Pang Lee ,  Wayne Charles Hasz ,  Nesim Abuaf ,  Robert Alan Johnson

    发明人： Ching Pang Lee ,  Wayne Charles Hasz ,  Nesim Abuaf ,  Robert Alan Johnson

    IPC分类号： B22C702

    CPC分类号： B22C9/02 ,  B22C7/02 ,  B22C9/04

    摘要： A casting includes a heat tranfer surface having a pluality of cavities. The plurality of cavities includes a density of at least about 25 cavities per square centimeter to about 1,100 cavities per square centimeter resulting in increased surface area and therefore enhanced heat transfer capability. Also disclosed is a mold for forming a pattern for molding the casting. The mold includes a surface defining a portion of a chamber to which are attached a plurality of particles having an average particle size in a range of about 300 microns to about 2,000 microns.

    摘要翻译： 铸件包括具有空腔抽吸性的热传递表面。 多个空腔包括每平方厘米至少约25个腔体至每平方厘米约1,100个空腔的密度，导致增加的表面积，从而增强了传热能力。 还公开了一种用于形成用于模制铸件的图案的模具。 模具包括限定室的一部分的表面，其中连接有平均粒度在约300微米至约2,000微米范围内的多个颗粒。

    Casting having an enhanced heat transfer, surface, and mold and pattern for forming same
    8.
    发明授权
    Casting having an enhanced heat transfer, surface, and mold and pattern for forming same 失效
    铸造具有增强的热传递，表面和模具以及用于形成它们的图案

    公开(公告)号：US06382300B2

    公开(公告)日：2002-05-07

    申请号：US09863185

    申请日：2001-05-24

    申请人： Ching Pang Lee ,  Wayne Charles Hasz ,  Nesim Abuaf ,  Robert Alan Johnson

    发明人： Ching Pang Lee ,  Wayne Charles Hasz ,  Nesim Abuaf ,  Robert Alan Johnson

    IPC分类号： B22C700

    CPC分类号： B22C9/04 ,  B22C7/02 ,  B22C9/02 ,  B22D25/06

    摘要： A casting includes a heat transfer surface having a plurality of cavities. The plurality of cavities include a density of at least about 25 cavities per square centimeter to about 1,100 cavities per square centimeter resulting in increased surface area and therefore enhanced heat transfer capability. Also disclosed is a mold for forming a pattern for molding the casting. The mold includes a surface defining a portion of a chamber to which are attached a plurality of particles having an average particle size in a range of about 300 microns to about 2,000 microns.

    摘要翻译： 铸件包括具有多个空腔的传热表面。 多个空腔包括每平方厘米至少约25个腔体至每平方厘米约1,100个空腔的密度，导致增加的表面积并因此提高传热能力。 还公开了一种用于形成用于模制铸件的图案的模具。 模具包括限定室的一部分的表面，其中连接有平均粒度在约300微米至约2,000微米范围内的多个颗粒。

    Airfoil with reduced heat load
    9.
    发明授权
    Airfoil with reduced heat load 有权
    减少热负荷的翼型

    公开(公告)号：US06183197B2

    公开(公告)日：2001-02-06

    申请号：US09253367

    申请日：1999-02-22

    申请人： Ronald Scott Bunker ,  Nesim Abuaf

    发明人： Ronald Scott Bunker ,  Nesim Abuaf

    IPC分类号： F01D508

    CPC分类号： F01D5/141 ,  F05D2260/231 ,  Y02T50/67 ,  Y02T50/673 ,  Y02T50/675 ,  Y10S415/914

    摘要： An airfoil with a reduced heat load for use in either a turbine or a compressor of a gas turbine engine comprises having at least one heat reducing dimple on the body of the airfoil or on the associated endwall of the airfoil. The body of the airfoil is comprised of a leading edge, a trailing edge, a pressure side and a suction side. The length of the heat reducing dimple in the expected direction of hot gas stream flow is at least equal to or greater than the width transverse to such direction. The heat reducing dimple is located on the airfoil or endwall so as to reduce the heat load as the hot gas stream flow passes from the leading edge to the trailing edge.

    摘要翻译： 具有用于燃气涡轮发动机的涡轮或压缩机中的具有降低的热负荷的翼型件包括在翼型体的主体或翼型的相关端壁上具有至少一个减热凹坑。 机翼的主体由前缘，后缘，压力侧和吸力侧构成。 热气流期望方向上的减热凹坑的长度至少等于或大于横向于该方向的宽度。 减热凹坑位于翼型件或端壁上，以便随着热气流从前缘到后缘流动而减少热负荷。

    Thermal spreading combustor liner
    10.
    发明授权
    Thermal spreading combustor liner 失效
    热扩散燃烧器衬套

    公开(公告)号：US5749229A

    公开(公告)日：1998-05-12

    申请号：US542982

    申请日：1995-10-13

    申请人： Nesim Abuaf ,  Steven George Goebel

    发明人： Nesim Abuaf ,  Steven George Goebel

    IPC分类号： F02K1/82 ,  F23R3/00 ,  F02C1/00

    CPC分类号： F23R3/002 ,  F02K1/82 ,  F05D2260/201 ,  F23R2900/03044 ,  Y02T50/67 ,  Y02T50/675 ,  Y10S60/909 ,  Y10T428/12611

    摘要： A combustor liner includes an inner layer for facing combustion gases, and an opposite outer layer for facing a cooling fluid. The outer layer has a greater coefficient of thermal conductivity than the inner layer for reducing temperature gradients in the liner. In a preferred embodiment, the outer layer significantly reduces temperature gradients in the liner which are caused by the varying cooling ability of impingement cooling air jets for more uniformly cooling the combustor liner and reducing the maximum temperature thereof.

    摘要翻译： 燃烧器衬套包括用于面对燃烧气体的内层和用于面对冷却流体的相对的外层。 外层具有比内层更大的导热系数，用于降低内衬中的温度梯度。 在一个优选实施例中，外层显着降低了衬套中的温度梯度，这是由冲击冷却空气射流变化的冷却能力引起的，用于更均匀地冷却燃烧器衬套并降低其最大温度。