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公开(公告)号：US09284851B2
公开(公告)日：2016-03-15
申请号：US13610136
申请日：2012-09-11
CPC分类号： F01D17/00 , F01D17/162 , F04D29/563
摘要： In a variable vane drive device of an axial-flow fluid machine, a ring support unit supporting a movable ring includes: a first roller; a first support part supporting the first rollers so as to be relatively immovable with respect to a vane holding ring in a radial direction and in an axial direction; a second roller; a second support part supporting the second roller so as to be relatively movable with respect to the vane holding ring in the radial direction and pressing the second roller in the radial direction; a third roller allowing relative movement of the movable ring in the radial direction and restricting relative movement of the movable ring in the axial direction; and a third support part supporting the third roller so as to be relatively immovable with respect to the vane holding ring in the axial direction and in the radial direction.
摘要翻译： 在轴流式流体机械的可变叶片驱动装置中，支撑可动环的环支承单元包括：第一辊; 第一支撑部，其支撑所述第一辊，以相对于叶片保持环在径向方向和轴向上相对不可移动; 第二辊; 第二支撑部，其支撑所述第二辊，以相对于所述叶片保持环沿径向方向相对移动，并且沿径向按压所述第二辊; 第三辊，允许可动环在径向上相对移动并限制可动环在轴向方向上的相对运动; 以及第三支撑部，其支撑所述第三辊，以相对于所述叶片保持环在轴向方向和径向方向上相对不可移动。
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公开(公告)号：US20130216360A1
公开(公告)日：2013-08-22
申请号：US13610136
申请日：2012-09-11
IPC分类号： F01D17/00
CPC分类号： F01D17/00 , F01D17/162 , F04D29/563
摘要： In a variable vane drive device of an axial-flow fluid machine, a ring support unit supporting a movable ring includes: a first roller; a first support part supporting the first rollers so as to be relatively immovable with respect to a vane holding ring in a radial direction and in an axial direction; a second roller; a second support part supporting the second roller so as to be relatively movable with respect to the vane holding ring in the radial direction and pressing the second roller in the radial direction; a third roller allowing relative movement of the movable ring in the radial direction and restricting relative movement of the movable ring in the axial direction; and a third support part supporting the third roller so as to be relatively immovable with respect to the vane holding ring in the axial direction and in the radial direction.
摘要翻译： 在轴流式流体机械的可变叶片驱动装置中，支撑可动环的环支承单元包括：第一辊; 第一支撑部，其支撑所述第一辊，以相对于叶片保持环在径向方向和轴向上相对不可移动; 第二辊; 第二支撑部，其支撑所述第二辊，以相对于所述叶片保持环沿径向方向相对移动，并且沿径向按压所述第二辊; 第三辊，允许可动环在径向上相对移动并限制可动环在轴向方向上的相对运动; 以及第三支撑部，其支撑所述第三辊，以相对于所述叶片保持环在轴向方向和径向方向上相对不可移动。
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公开(公告)号：US08899934B2
公开(公告)日：2014-12-02
申请号：US13362629
申请日：2012-01-31
CPC分类号： F04D29/322 , F01D5/3038 , F01D5/32
摘要： The rotor structure is provided with a rotation shaft body in which a blade groove is formed at an outer circumference part, and extends in a circumferential direction of the axis line, and a plurality of blade bodies which are arrayed in the circumferential direction at the outer circumference part of the rotation shaft body, wherein a blade fixing piece is installed so as to be a positioned between at least one set of adjacent two blade bodies in the circumferential direction inside the blade groove, a projected part is formed at where either an opening wall part or the groove opening side of the blade groove and the blade fixing piece, and a recessed part which is fitted into the projected part is formed at where the other one of them.
摘要翻译： 转子结构设置有旋转轴体，其中，在外周部形成有叶片槽，沿轴线的圆周方向延伸，并且在外周沿圆周方向排列的多个叶片体 旋转轴体的圆周部，其中，叶片固定片安装成位于叶片槽内的圆周方向上的至少一组相邻的两个叶片体之间，形成有突起部， 叶片槽和刀片固定片的壁部分或凹槽开口侧，并且嵌入突出部分中的凹部形成在其中另一个处。
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公开(公告)号：US20120251329A1
公开(公告)日：2012-10-04
申请号：US13362629
申请日：2012-01-31
IPC分类号： F01D5/30
CPC分类号： F04D29/322 , F01D5/3038 , F01D5/32
摘要： The rotor structure is provided with a rotation shaft body in which a blade groove is formed at an outer circumference part, and extends in a circumferential direction of the axis line, and a plurality of blade bodies which are arrayed in the circumferential direction at the outer circumference part of the rotation shaft body, wherein a blade fixing piece is installed so as to be a positioned between at least one set of adjacent two blade bodies in the circumferential direction inside the blade groove, a projected part is formed at where either an opening wall part or the groove opening side of the blade groove and the blade fixing piece, and a recessed part which is fitted into the projected part is formed at where the other one of them.
摘要翻译： 转子结构设置有旋转轴体，其中，在外周部形成有叶片槽，沿轴线的圆周方向延伸，并且在外周沿圆周方向排列的多个叶片体 旋转轴体的圆周部，其中，叶片固定片安装成位于叶片槽内的圆周方向上的至少一组相邻的两个叶片体之间，形成有突起部， 叶片槽和刀片固定片的壁部分或凹槽开口侧，并且嵌入突出部分中的凹部形成在其中另一个处。
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公开(公告)号：US20070271930A1
公开(公告)日：2007-11-29
申请号：US11416454
申请日：2006-05-03
申请人： Yoshimasa Takaoka , Masato Araki , Vincent Laurello , Masahito Kataoka , Junichiro Masada , Koichi Ishizaka , Naoki Hagi
发明人： Yoshimasa Takaoka , Masato Araki , Vincent Laurello , Masahito Kataoka , Junichiro Masada , Koichi Ishizaka , Naoki Hagi
IPC分类号： F02C7/12
CPC分类号： F01D5/06 , F01D5/082 , F01D5/084 , F01D5/085 , Y02T50/676
摘要： A gas turbine includes a cooling-air transfer system. The cooing-air transfer system extracts part of air discharged from a compressor to a chamber, and transfers the part of air as cooling air to a rotor disk. The cooling-air transfer system includes a plurality of tubular nozzles independently arranged in a circle inside the chamber to surround a rotor, and a seal disk having seal-disk cooling conduits arranged in a circle around the axis of the rotor so as to receive cooling air ejected from the tubular nozzles. The cooling-air transfer system swirls the cooling air ejected from the tubular nozzles.
摘要翻译： 燃气轮机包括冷却空气输送系统。 冷凝空气输送系统将从压缩机排出的空气的一部分提取到室，并将作为冷却空气的空气的一部分转移到转子盘。 冷却空气传送系统包括多个管状喷嘴，其独立地设置在腔室内的圆周中以围绕转子;以及密封盘，其具有围绕转子轴线布置成圆形的密封盘冷却导管，以便接收冷却 从管状喷嘴排出的空气。 冷却空气传送系统使从管状喷嘴喷出的冷却空气旋转。
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公开(公告)号：US20120269622A1
公开(公告)日：2012-10-25
申请号：US13357179
申请日：2012-01-24
IPC分类号： F01D9/02
CPC分类号： F16J15/0887 , F01D9/04 , F01D11/005 , F05D2240/55 , F16J15/4476
摘要： A turbine vane of the invention includes: a plurality of outer shrouds (8a) that are provided along the turbine circumferential direction so as to be adjacent to each other and form an outer wall of a main passageway; inner shrouds (8b) that form an inner wall; a airfoil body (8c) that protrudes from a front surface of the inner shroud (8b) and defines a flow of combustion gas directed from the upstream side of the main passageway toward the downstream side thereof; and a retainer (8d) which protrudes from a rear surface of the inner shroud (8b) and extends along the turbine circumferential direction, wherein the retainer (8d) is disposed on the downstream side in relation to an intersection point (Q) between a dividing gap (K1) of the adjacent inner shrouds (8b) and a throat line (P) which connects the contact points of a minimal inscribed circle according to the blade shapes of the adjacent airfoil bodies (8c).
摘要翻译： 本发明的涡轮叶片包括：沿着涡轮机圆周方向设置成彼此相邻并形成主通道的外壁的多个外护罩（8a）; 形成内壁的内护罩（8b） 从所述内护罩（8b）的前表面突出并限定从所述主通道的上游侧向其下游侧引导的燃烧气体流的翼型体（8c）; 以及从所述内罩（8b）的后表面突出并沿着所述涡轮机周向延伸的保持器（8d），其中，所述保持器（8d）相对于所述内护罩 根据相邻翼型体（8c）的叶片形状，相邻的内护罩（8b）的分隔间隙（K1）和连接最小内切圆的接触点的喉管（P）。
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