公开(公告)号：US20060275108A1

公开(公告)日：2006-12-07

申请号：US11146801

申请日：2005-06-07

申请人： Robert Memmen ,  Gary Bash

发明人： Robert Memmen ,  Gary Bash

IPC分类号： F03B11/00

CPC分类号： F01D11/001 ,  F01D5/081 ,  F05D2250/283 ,  F05D2250/70

摘要： Disclosed are assemblies and articles for restricting leakage of a pressurized fluid from a cavity flanked by a vane support and a bladed rotor assembly. In accordance with an embodiment of the invention, the vane support defines a circumferential channel, and a interrupted rim region of the bladed rotor assembly defines a segmented ring. The segmented ring protrudes outward from the bladed rotor assembly, spans across the cavity and into the channel to define a seal.

摘要翻译： 公开了用于限制加压流体从由叶片支撑件和叶片转子组件侧面的空腔泄漏的组件和制品。 根据本发明的实施例，叶片支撑件限定圆周通道，并且叶片转子组件的中断的边缘区域限定分段环。 分段环从叶片转子组件向外突出，跨越空腔并进入通道以限定密封。

公开(公告)号：US06761536B1

公开(公告)日：2004-07-13

申请号：US10355883

申请日：2003-01-31

申请人： Gary Bash ,  J. Page Strohl

发明人： Gary Bash ,  J. Page Strohl

IPC分类号： F01D518

CPC分类号： F01D5/18 ,  F01D5/30

摘要： A gas turbine blade having an airfoil to platform interface configured to minimize thermal and vibratory stresses is disclosed. This configuration minimizes exposure to the conditions that are known to cause high cycle fatigue and low cycle fatigue cracks. The turbine blade incorporates a channel in the platform trailing edge that extends from the platform concave face to the platform convex face and has a portion having a constant radius. The channel extends a sufficient distance into a stress field created by the aerodynamic loading of the turbine blade airfoil in order to redirect the mechanical stresses away from the blade trailing edge while allowing the platform trailing edge region to be more responsive to thermal fluctuations.

摘要翻译： 公开了一种具有构造成使热和振动应力最小化的翼型到平台接口的燃气轮机叶片。 这种构造使得暴露于已知导致高循环疲劳和低循环疲劳裂纹的条件下。 涡轮机叶片包括平台后缘中的从平台凹面延伸到平台凸面的通道，并且具有恒定半径的部分。 通道延伸到由涡轮叶片翼型件的空气动力学负载产生的应力场中的足够的距离，以便将机械应力从叶片后缘重定向，同时允许平台后缘区域对热波动更加响应。

公开(公告)号：US07101150B2

公开(公告)日：2006-09-05

申请号：US10842976

申请日：2004-05-11

申请人： Gary Bash ,  J. Page Strohl

发明人： Gary Bash ,  J. Page Strohl

IPC分类号： F01D1/02 ,  F01D9/00

CPC分类号： F01D9/042 ,  F05D2230/642 ,  F05D2240/80 ,  F05D2260/30

摘要： A vane assembly for a gas turbine is described wherein the vane assembly comprises a first vane and a second vane connected together by a plurality of flanges, at least one fastener, and at least one spring plate. The fastener and hole diameters in the respective flanges are sized such that the first vane and second vane are essentially pinned together along their inner flanges and allowed to adjust due to thermal growth along their outer flanges, while maintaining a constant seal along both inner and outer platform edges. The thermal growth along the outer flanges is made possible by oversized flange holes relative to the diameter of the fastener.

摘要翻译： 描述了一种用于燃气轮机的叶片组件，其中叶片组件包括通过多个凸缘，至少一个紧固件和至少一个弹簧板连接在一起的第一叶片和第二叶片。 相应凸缘中的紧固件和孔直径的尺寸使得第一叶片和第二叶片沿着其内凸缘基本上被固定在一起，并且由于沿着它们的外凸缘的热生长而允许调节，同时沿着内外两者保持恒定的密封 平台边缘。 通过相对于紧固件的直径的超大的凸缘孔，沿着外凸缘的热生长成为可能。

公开(公告)号：US20050254944A1

公开(公告)日：2005-11-17

申请号：US10842976

申请日：2004-05-11

申请人： Gary Bash ,  J. Strohl

发明人： Gary Bash ,  J. Strohl

IPC分类号： F01D1/02 ,  F01D9/04

CPC分类号： F01D9/042 ,  F05D2230/642 ,  F05D2240/80 ,  F05D2260/30

摘要： A vane assembly for a gas turbine is described wherein the vane assembly comprises a first vane and a second vane connected together by a plurality of flanges, at least one fastener, and at least one spring plate. The fastener and hole diameters in the respective flanges are sized such that the first vane and second vane are essentially pinned together along their inner flanges and allowed to adjust due to thermal growth along their outer flanges, while maintaining a constant seal along both inner and outer platform edges. The thermal growth along the outer flanges is made possible by oversized flange holes relative to the diameter of the fastener.

摘要翻译： 描述了一种用于燃气轮机的叶片组件，其中叶片组件包括通过多个凸缘，至少一个紧固件和至少一个弹簧板连接在一起的第一叶片和第二叶片。 相应凸缘中的紧固件和孔直径的尺寸使得第一叶片和第二叶片沿着其内凸缘基本上被固定在一起，并且由于沿着它们的外凸缘的热生长而允许调节，同时沿着内外两者保持恒定的密封 平台边缘。 通过相对于紧固件的直径的超大的凸缘孔，沿着外凸缘的热生长成为可能。

公开(公告)号：US08142137B2

公开(公告)日：2012-03-27

申请号：US12323736

申请日：2008-11-26

申请人： Chris Johnston ,  Gary Bash ,  Tim teRiele ,  David Parker ,  James Page Strohl

发明人： Chris Johnston ,  Gary Bash ,  Tim teRiele ,  David Parker ,  James Page Strohl

IPC分类号： F03B11/00 ,  F01D5/14

CPC分类号： F01D5/188 ,  F01D9/041 ,  F02C7/12 ,  F05D2240/81 ,  F05D2260/202 ,  Y10S416/50

摘要： A gas turbine vane to improve vane performance by addressing known failure mechanisms. A cooling circuit to the trailing edge of a vane airfoil is fed from the outer diameter platform, which prevents failure due to an oxidized and eroded airfoil trailing edge. The gas turbine includes an outer diameter platform, a hollow airfoil and an inner diameter platform with a plurality of cooling tubes extending radially through the airfoil. The cooling tubes are open at the outer diameter end and closed with covers at the inner diameter end. The inner diameter platform is also cooled and includes a meterplate for a portion of the cooling passageway and includes an undercut to improve thermal deflections of the inner diameter platform.

摘要翻译： 一种燃气轮机叶片，通过解决已知的故障机制来改善叶片性能。 从外径平台供给到叶片翼型的后缘的冷却回路，这防止由于氧化和侵蚀的翼型后缘造成的故障。 燃气轮机包括外径平台，中空翼型件和具有径向延伸穿过翼型件的多个冷却管的内径平台。 冷却管在外径端开口，在内径端用盖封闭。 内径平台也被冷却，并且包括用于冷却通道的一部分的仪表板，并且包括底切以改善内径平台的热偏转。

公开(公告)号：US20100129196A1

公开(公告)日：2010-05-27

申请号：US12323736

申请日：2008-11-26

申请人： Chris Johnston ,  Gary Bash ,  Tim teRiele ,  David Parker ,  James Page Strohl

发明人： Chris Johnston ,  Gary Bash ,  Tim teRiele ,  David Parker ,  James Page Strohl

IPC分类号： F02C7/12

CPC分类号： F01D5/188 ,  F01D9/041 ,  F02C7/12 ,  F05D2240/81 ,  F05D2260/202 ,  Y10S416/50

摘要： A gas turbine vane to improve vane performance by addressing known failure mechanisms. A cooling circuit to the trailing edge of a vane airfoil is fed from the outer diameter platform, which prevents failure due to an oxidized and eroded airfoil trailing edge. The gas turbine includes an outer diameter platform, a hollow airfoil and an inner diameter platform with a plurality of cooling tubes extending radially through the airfoil. The cooling tubes are open at the outer diameter end and closed with covers at the inner diameter end. The inner diameter platform is also cooled and includes a meterplate for a portion of the cooling passageway and includes an undercut to improve thermal deflections of the inner diameter platform.

摘要翻译： 一种燃气轮机叶片，通过解决已知的故障机制来改善叶片性能。 从外径平台供给到叶片翼型的后缘的冷却回路，这防止由于氧化和侵蚀的翼型后缘造成的故障。 燃气轮机包括外径平台，中空翼型件和具有径向延伸穿过翼型件的多个冷却管的内径平台。 冷却管在外径端开口，在内径端用盖封闭。 内径平台也被冷却，并且包括用于冷却通道的一部分的仪表板，并且包括底切以改善内径平台的热偏转。