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公开(公告)号：US07334992B2
公开(公告)日：2008-02-26
申请号：US11140786
申请日：2005-05-31
IPC分类号： F01D5/18
CPC分类号： F01D5/186 , F01D5/187 , F05D2250/711 , F05D2250/712 , F05D2260/201 , F05D2260/202
摘要： A turbine blade cooling system for a gas turbine engine includes a turbine blade having a trailing edge, a concave side, and a convex side. The trailing edge defines at least one set of impingement holes each having a central longitudinal axis which is closer to a nearest portion of an edge of the blade at one of the concave and convex sides relative to a nearest portion of an edge of the blade at the other of the concave and convex sides. Alternatively or in addition to the foregoing, the trailing edge can define at least one set of impingement holes each having a central longitudinal axis which is angled in a direction of a flow of cooling medium toward one of the concave and convex sides relative to the other of the concave and convex sides.
摘要翻译： 用于燃气涡轮发动机的涡轮叶片冷却系统包括具有后缘，凹侧和凸侧的涡轮叶片。 后缘限定至少一组冲击孔，每组冲击孔具有中心纵向轴线，该中心纵向轴线相对于叶片的边缘的最近部分在相对于叶片的边缘的最近部分处于相对于叶片的边缘的最靠近部分处更靠近叶片的边缘的最近部分 另一个凹凸边。 或者或除了上述之外，后缘可以限定至少一组冲击孔，每组冲击孔具有中心纵向轴线，所述中心纵向轴线在冷却介质的流动方向上相对于另一组的凹凸侧面 的凹凸边。
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公开(公告)号：US5614294A
公开(公告)日：1997-03-25
申请号：US346645
申请日：1994-11-30
申请人： James P. Downs , Eduardo Ruano
发明人： James P. Downs , Eduardo Ruano
CPC分类号： C23C28/321 , C23C14/083 , C23C14/16 , C23C28/3455 , C23C28/42 , F01D5/288 , Y10T428/24942
摘要： An article is provided, comprising a structure and a coating for minimizing thermal gradients in the structure. The coating includes a plurality of first layers of thermally conductive material, and a plurality of second layers of thermally conductive material. The first layers of thermally conductive material are less thermally conductive than the second layers at any particular temperature, and the layers are applied to the article such that the second layers of thermally conductive material are distributed amongst the first layers of thermally conductive material. Conduction of thermal energy through the layers to the structure is substantially impeded within the first layers, and substantially laterally dispersed within the second layers, thereby minimizing any thermal gradients within the structure.
摘要翻译： 提供了一种制品，其包括用于使结构中的热梯度最小化的结构和涂层。 涂层包括多个导热材料的第一层和多个第二导热材料层。 导热材料的第一层在任何特定温度下的热传导性都低于第二层，并且将这些层施加到制品上，使得第二层导热材料分布在第一层导热材料之中。 在第一层内基本上阻碍了通过层到结构的热能传导，并且基本上横向分散在第二层内，从而使结构内的任何热梯度最小化。
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公开(公告)号：US5540300A
公开(公告)日：1996-07-30
申请号：US370203
申请日：1995-01-09
CPC分类号： F16H57/0412 , F16H57/0415 , F16H57/0421 , F16H57/0457 , F16H57/0483 , F16N39/02 , F16N7/18 , Y10T74/2188 , Y10T74/2189
摘要： A drive axle assembly has a gear housing, two axle tubes extending outwardly of the gear housing, a lubricant reservoir in the gear housing and a gear assembly rotatably mounted in the gear housing that has a rotatable member that is partially disposed in lubricant in the lubricant reservoir. The drive axle assembly also has a lubricant cooling system that includes a lubricant passage in fluid communication with the lubricant reservoir via an inlet that is juxtaposed the rotatable member so that the level of lubricant in the lubricant passage is raised when the rotatable member rotates. The lubricant passage has elevated outlets that deliver lubricant to lubricant ducts disposed in the respective axle tubes when the lubricant in the lubricant passage rises above a predetermined level. The lubricant flows away from the gear housing in the lubricant ducts and returns to the reservoir along the interior of the axle tubes which cools the lubricant as it returns to the reservoir.
摘要翻译： 驱动桥组件具有齿轮壳体，两个轴管从齿轮壳体向外延伸，齿轮壳体中的润滑剂储存器和可旋转地安装在齿轮壳体中的齿轮组件，该齿轮组件具有部分地设置在润滑剂中的可旋转构件 水库 驱动轴组件还具有润滑剂冷却系统，该润滑剂冷却系统包括通过与可旋转构件并置的入口与润滑剂储存器流体连通的润滑剂通道，使得当可旋转构件旋转时润滑剂通道中的润滑剂水平升高。 润滑剂通道具有升高的出口，当润滑剂通道中的润滑剂上升到预定水平以上时，润滑剂将润滑剂输送到设置在相应的轴管中的润滑剂管道上。 润滑剂从润滑剂管道中的齿轮箱流出，并且沿着轴管的内部返回到储存器，该轴管在润滑剂返回到储存器时冷却润滑剂。
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34.发明申请公开(公告)号：US20160069264A1
公开(公告)日：2016-03-10
申请号：US14335916
申请日：2014-07-20
CPC分类号： F02C3/34 , F01D15/10 , F01K23/10 , F02C3/107 , F02C7/143 , F02C7/36 , F05D2220/32 , F05D2220/76 , H02K7/1823 , Y02E20/16 , Y02T50/675
摘要： A gas turbine engine, especially an industrial gas turbine engine for electrical power production, where a second compressor is used to supply a second compressed air at a higher pressure to a stage of stator vanes in the turbine section of the engine for cooling of the stage of stator vanes, and where the heated compressed air used to cool the stator vanes is then discharged into the combustor to be burned with a fuel and produce a hot gas stream that is passed through the turbine. an intercooler can be used with the second compressor to lower the temperature of the second compressed air used for cooling the stator vanes.
摘要翻译： 一种燃气涡轮发动机，特别是用于电力生产的工业燃气涡轮发动机，其中使用第二压缩机将较高压力的第二压缩空气供应到发动机的涡轮机部分中的定子叶片的一级，用于冷却级 的定子叶片，并且其中用于冷却定子叶片的加热的压缩空气然后被排放到燃烧器中以用燃料燃烧并产生通过涡轮机的热气流。 中间冷却器可以与第二压缩机一起使用，以降低用于冷却定子叶片的第二压缩空气的温度。
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公开(公告)号：US20120082563A1
公开(公告)日：2012-04-05
申请号：US12894476
申请日：2010-09-30
CPC分类号： F01D5/187 , F01D5/081 , F01D5/34 , F01D11/001 , F05D2250/80 , F05D2260/202 , F05D2260/205 , Y02T50/676
摘要： A micro gas turbine engine in which the turbine rotor blades are formed as an integral bladed rotor with cooling air passages formed within the blades and the rotor disk by an EDM process. an adjacent stator vane includes an air riding seal with an air cushion supplied through the vanes to provide cooling, and where the air cushion is then passed into the turbine blades and rotor disk to provide cooling for the turbine blades. With cooling of the turbine blades, higher turbine inlet temperatures for micro gas turbine engines can be produced.
摘要翻译： 一种微型燃气涡轮发动机，其中涡轮机转子叶片形成为整体叶片转子，其中通过EDM工艺在叶片和转子盘中形成冷却空气通道。 相邻的定子叶片包括具有通过叶片提供的气垫的空气骑行密封件以提供冷却，并且其中气垫然后进入涡轮机叶片和转子盘以为涡轮叶片提供冷却。 通过涡轮叶片的冷却，可以生产用于微型燃气涡轮发动机的更高的涡轮机入口温度。
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公开(公告)号：US07871245B2
公开(公告)日：2011-01-18
申请号：US12490705
申请日：2009-06-24
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , B22C7/06 , B22C9/10 , F05D2230/21 , F05D2230/50
摘要： Two pairs of ribs define three intermediate cooling chambers. Each rib in each pair extends parallel to the other rib in the pair. The ribs in a first pair are non-parallel to the ribs in a second pair. A first rib from the first pair is positioned spaced toward the leading edge. A first rib of the second pair is then serially positioned spaced toward the trailing edge. A second rib of the first pair is then positioned toward the trailing edge relative to the first rib in the second pair. A second rib in the second pair is then positioned toward the trailing edge relative to the second rib in the first pair.
摘要翻译： 两对肋条限定了三个中间冷却室。 每对中的每个肋平行于该对中的另一个肋延伸。 第一对中的肋与第二对中的肋不平行。 来自第一对的第一肋被定位成与前缘隔开。 然后将第二对的第一肋串联地定位成朝向后缘。 然后将第一对的第二肋相对于第二对中的第一肋定位成朝向后缘。 然后将第二对中的第二肋相对于第一对中的第二肋定位成朝向后缘。
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公开(公告)号：US07534085B2
公开(公告)日：2009-05-19
申请号：US11472104
申请日：2006-06-21
IPC分类号： F01D5/08
CPC分类号： F01D5/081 , Y02T50/676
摘要： A gas turbine engine is provided with a turbine rotor disk having a plurality of disk slots which each receive a turbine blade. Cooling air is delivered into the disk slots, and flows into cooling air passages at a radially inner surface of the turbine blades. As known, the cooling air flows through the turbine blades to cool internal and external surfaces of the turbine blade. The disk slots are formed to have a greater cross-sectional area adjacent at the inlet end than at downstream locations. In this manner, the velocity of the air at the inlet end is reduced compared to the prior art, and pressure losses are minimized compared to the prior art.
摘要翻译： 燃气涡轮发动机设置有具有多个盘槽的涡轮转子盘，每个盘槽都容纳涡轮叶片。 冷却空气被输送到盘槽中，并且在涡轮叶片的径向内表面处流入冷却空气通道。 如已知的，冷却空气流过涡轮机叶片以冷却涡轮机叶片的内部和外部表面。 盘槽形成为在入口端处具有比在下游位置处更大的横截面面积。 以这种方式，与现有技术相比，入口端的空气速度降低，与现有技术相比，压力损失最小化。
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38.发明申请FOUR PINION DIFFERENTIAL WITH CROSS PIN RETENTION UNIT AND RELATED METHOD 有权具有十字头保持单元的四个PINION和相关方法公开(公告)号：US20090088285A1
公开(公告)日：2009-04-02
申请号：US12237726
申请日：2008-09-25
CPC分类号： F16H48/08 , F16H2048/085 , Y10T29/49945 , Y10T29/49959
摘要： A differential having four pinions supported for rotation on cross pins within a differential case. The differential employs a retainer system for securing the cross pins relative to the differential case. The retainer system can include a collar and a plurality of pin members.
摘要翻译： 具有四个小齿轮的差速器，其支撑在差速器壳体内的十字销上。 差速器采用用于固定十字销相对于差速器壳体的保持器系统。 保持器系统可以包括轴环和多个销构件。
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公开(公告)号：US20080132342A1
公开(公告)日：2008-06-05
申请号：US12011598
申请日：2008-01-28
申请人： William E. Worman , James P. Downs
发明人： William E. Worman , James P. Downs
IPC分类号： F16C3/02
CPC分类号： F16D3/845 , F16D1/068 , F16D3/22 , F16D2001/103 , Y10S464/906
摘要： A propeller shaft assembly includes a substantially cylindrical hollow propeller shaft, a stub shaft and a constant velocity joint having inner race and an outer race drivingly interconnected by a plurality of balls. The stub shaft has a first end fixed to the propeller shaft and a second end drivingly coupled to the inner race. The second end includes a portion positioned adjacent to the inner race that defines an outer diameter greater than an outer diameter defined by the interface between the inner race and the plurality of balls.
摘要翻译： 传动轴组件包括大致圆柱形的中空推进器轴，短轴和具有内圈的等速接头和通过多个滚珠驱动地连接的外座圈。 短轴具有固定到传动轴的第一端和驱动地连接到内圈的第二端。 第二端包括邻近内圈定位的部分，其限定大于由内圈和多个球之间的界面限定的外径的外径。
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公开(公告)号：US07207409B2
公开(公告)日：2007-04-24
申请号：US10797717
申请日：2004-03-10
申请人： James P. Downs
发明人： James P. Downs
IPC分类号： B60K17/34
CPC分类号： B60K17/3467
摘要： A two speed drive system for an all wheel drive vehicle includes a double planetary gear front differential and a power take-off unit transferring drive torque to a front wheel set and a rear wheel set of the vehicle. A rear differential connects the power take-off unit and the rear wheel set providing the drive torque to the rear wheel set. A two speed drive unit is positioned between the power take-off unit and the rear differential. The drive unit shifts between a high range drive operation and a low range drive operation. The drive unit may be mounted directly to either the power take-off unit or the rear differential.
摘要翻译： 用于全轮驱动车辆的双速驱动系统包括双行星齿轮前差速器和将驱动扭矩传递到车辆的前轮组和后轮组的动力输出单元。 后差速器将动力输出单元和提供驱动扭矩的后轮组件连接到后轮组。 两速驱动单元位于动力输出单元和后差速器之间。 驱动单元在高范围驱动操作和低范围驱动操作之间移动。 驱动单元可以直接安装在动力输出单元或后差速器上。
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