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公开(公告)号：US06209198B1
公开(公告)日：2001-04-03
申请号：US09213403
申请日：1998-12-16
申请人： Andrew J. Lammas , Wayne R. Bowen
发明人： Andrew J. Lammas , Wayne R. Bowen
IPC分类号： B23P1500
CPC分类号： F01D17/162 , F01D25/28 , F05D2230/64 , Y10T29/49323 , Y10T29/49325
摘要： A method and fixture assembly for assisting in the matching and assembly of components of a variable stator vane assembly of a gas turbine engine. The method generally entails a stator vane configured to be assembled to a casing with a spacer. The vane has a surface at a perimeter thereof and a seat offset from the surface. The spacer to which the vane is to be assembled has first and second surfaces offset relative to each other, the first surface being adapted to engage the seat of the vane and the second surface adapted to face the surface of the vane. The vane is installed within an opening in the casing so that a first sealing member is between the casing and the vane, the casing is between the first sealing member and a second sealing member, and the seat extends through the opening. A fixture is then mounted to the vane so that the casing and the first and second sealing members are clamped between the fixture and the vane under a load. The position of the seat of the vane is then detected, and a spacer is selected having an offset dimension between its first and second surfaces based on the position of the seat.
摘要翻译： 一种用于辅助燃气涡轮发动机的可变定子叶片组件的部件的匹配和组装的方法和固定装置。 该方法通常需要将定子叶片配置成用间隔件组装到壳体上。 叶片在其周边具有表面，并且座面偏离表面。 要组装叶片的间隔件具有相对于彼此偏移的第一和第二表面，第一表面适于接合叶片的座和适于面对叶片表面的第二表面。 叶片安装在壳体的开口内，使得第一密封构件位于壳体和叶片之间，壳体位于第一密封构件和第二密封构件之间，并且座部延伸穿过开口。 然后将夹具安装到叶片上，使得壳体和第一和第二密封构件在负载下夹在固定装置和叶片之间。 然后检测叶片的座位的位置，并且基于座椅的位置，选择具有在其第一和第二表面之间的偏移尺寸的间隔件。
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公开(公告)号：US5209633A
公开(公告)日：1993-05-11
申请号：US839275
申请日：1992-02-25
IPC分类号： F04D27/02
CPC分类号： F04D29/542 , F04D27/023
摘要： A high pressure compressor flowpath bleed extraction slot is provided wherein an articulated portion of the outer band of the compressor forms a slot for providing efficient conversion of core air to diffuser air while retaining substantial pressure and velocity energies. The diffuser slot can be applied to an earlier compressor stage with improved performance.
摘要翻译： 提供了一种高压压缩机流路泄放提取槽，其中压缩机的外带的铰接部分形成用于提供核心空气到扩散空气的有效转换的槽，同时保持大量的压力和速度能量。 扩散器槽可以应用于具有改进性能的较早的压缩机级。
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公开(公告)号：US6146093A
公开(公告)日：2000-11-14
申请号：US213402
申请日：1998-12-16
申请人： Andrew J. Lammas , Wayne R. Bowen
发明人： Andrew J. Lammas , Wayne R. Bowen
CPC分类号： F01D11/005 , F01D11/00 , F01D17/162
摘要： A seal and a washer for a variable vane assembly in a turbine engine are described. The seal includes a first portion and a second portion that are substantially perpendicular. The seal is positioned between a variable vane and a casing. The washer is substantially flat and is located between the casing and a spacer.
摘要翻译： 描述了一种用于涡轮发动机中的可变叶片组件的密封件和垫圈。 密封件包括基本垂直的第一部分和第二部分。 密封件位于可变叶片和壳体之间。 垫圈基本上是平的，并且位于壳体和间隔件之间。
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公开(公告)号：US6139261A
公开(公告)日：2000-10-31
申请号：US293382
申请日：1999-04-16
CPC分类号： F16C33/201 , F16C17/02 , F16C3/00
摘要： A bushing assembly as a means to enable guided movement of a shaft in an opening of a housing comprises a stationary bushing support carried by a housing internal wall. The bushing support has a support internal wall defining a bushing support opening through the bushing support to receive a movable shaft. Carried by the shaft is a removable wear sleeve having a wear sleeve outer wall in juxtaposition with and spaced apart from the support internal wall to permit relative axial movement of the wear sleeve with the shaft within the bushing support opening. Disposed between and for contact with the support internal wall and with the wear sleeve outer wall is an anti-friction layer.
摘要翻译： 作为用于使轴在壳体的开口中引导移动的装置的衬套组件包括由壳体内壁承载的固定衬套支撑件。 衬套支撑件具有支撑内壁，其限定穿过衬套支撑件的衬套支撑开口以接收可移动轴。 由轴承载的是可拆卸的耐磨套筒，其具有与支撑内壁并置并与其间隔开的耐磨套管外壁，以允许耐磨套筒与套管支撑孔内的轴相对轴向运动。 设置在支撑内壁和用于与支承内壁接触并与磨损套筒外壁之间的是抗摩擦层。
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公开(公告)号：US06290465B1
公开(公告)日：2001-09-18
申请号：US09364605
申请日：1999-07-30
申请人： Andrew J. Lammas , Nicholas J. Kray
发明人： Andrew J. Lammas , Nicholas J. Kray
IPC分类号： F01D514
CPC分类号： F01D5/3007 , F01D5/141 , F01D21/045 , F04D29/324
摘要： A rotor blade for a turbine engine including a blade root section and an airfoil section which extends radially outward along a radial line RAS from the blade root section, is described. The radial line RAS extends at an angle relative to a plane extending across a top surface of the platform, rather than normal, or perpendicular, to such plane. As a result, and during a blade out event, an over turning moment is generated in a root of the airfoil section. The overturning moment facilitates bending the airfoil section reducing damage to the stator.
摘要翻译： 描述了一种用于涡轮发动机的转子叶片，其包括叶片根部和沿着径向线RAS从叶根部径向向外延伸的翼型部。 径向线RAS相对于延伸穿过平台顶表面的平面以一定角度延伸，而不是垂直于该平面。 结果，并且在叶片断开事件期间，在翼型部分的根部中产生过度转弯。 倾翻力矩有利于弯曲翼型部分，减少对定子的损坏。
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6.发明授权公开(公告)号：US06267558B1
公开(公告)日：2001-07-31
申请号：US09318641
申请日：1999-05-26
IPC分类号： B63H120
CPC分类号： F01D5/3007 , C21D7/06 , F01D5/286 , F01D5/3092
摘要： An article and a method for improving an article that results in a reduction or elimination of damage due to fretting from contact of similar metals. The invention specifically reduces wear-related fretting between titanium alloy parts by lowering the stresses between mating parts. An aluminum bronze coating is applied to one of the parts. The aluminum bronze coating provides an improvement over prior art coatings in reducing coefficient of friction between the parts. Additionally, the cumulative stresses at the surface of the parts is reduced by a dual intensity peening treatment. This involves a first peening operation using large peening media that provides a compressive stress to the required depth. This first peening operation is followed by a second peening operation that provides additional compressive stresses closer to the dovetail surface. The combined metallurgical and mechanical improvement results in a system with less susceptibility to fretting damage and corresponding improved fatigue resistance.
摘要翻译： 一种用于改善制品的制品和方法，其导致由于类似金属的接触而导致的微小损伤的减少或消除。 本发明通过降低配合部件之间的应力来具体地减少钛合金部件之间的磨损相关的微动。 将铝青铜涂层施加到其中一个部件。 铝青铜涂层在减少部件之间的摩擦系数方面提供了优于现有技术的涂层。 另外，通过双重强度喷丸处理减少了部件表面的累积应力。 这涉及使用提供压缩应力到所需深度的大型喷丸介质的第一次喷丸操作。 该第一喷丸操作之后是第二喷丸操作，其提供更靠近燕尾表面的附加压缩应力。 组合的冶金和机械改进导致系统对微动损坏的敏感性较小并且相应地改善的耐疲劳性。
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公开(公告)号：US06250166B1
公开(公告)日：2001-06-26
申请号：US09327276
申请日：1999-06-04
IPC分类号： G01N302
CPC分类号： G01N3/32 , G01N2203/0246
摘要： A dovetail of a rotor blade is mounted in a complementary slot in a rotor disk. Life of the dovetail is simulated by providing a specimen dovetail mounted in a complementary slot in a fixture. Relative stiffness of the specimen dovetail and fixture are tailored to simulate the loading profile between the blade dovetail and rotor disk. Load is cycled between the specimen dovetail and fixture for determining life of the dovetail.
摘要翻译： 转子叶片的燕尾安装在转子盘的互补槽中。 通过提供安装在夹具中的互补槽中的样本燕尾榫来模拟燕尾榫的寿命。 试样燕尾和夹具的相对刚度被定制以模拟叶片燕尾榫和转子盘之间的载荷分布。 在样品燕尾榫和夹具之间循环加载，以确定燕尾榫的寿命。
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公开(公告)号：US5435694A
公开(公告)日：1995-07-25
申请号：US155967
申请日：1993-11-19
CPC分类号： F01D5/141 , F01D5/3007 , Y02T50/673
摘要： The present invention relieves the stress at a fillet of a blade shank using at least one axially extending pocket on the shank near an axially extending fillet of a shank to root interface or a shank to platform interface on a pressure or suction side of the blade and the pocket is axially shorter than the fillet. The stress relief pocket has a radially extending pocket width that is substantially wider than a fillet width between generally axially extending edges of the fillet wherein the pocket width may be several times wider than the fillet width. The wider pocket shields the fillet thereby reducing the stress concentration at the fillet.
摘要翻译： 本发明使用刀柄上的至少一个轴向延伸的口袋靠近刀柄的轴向延伸圆角至叶片的根部界面或柄与柄与平台界面之间在叶片的压力或吸力侧接近而减轻叶片柄部的应力，并且 口袋的轴向短于圆角。 应力释放袋具有径向延伸的袋宽度，其宽度大大大大于圆角的大致轴向延伸的边缘之间的圆角宽度，其中袋宽可以比圆角宽度多数倍。 更宽的口袋可以防护圆角，从而减少鱼片上的应力集中。
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公开(公告)号：US06375421B1
公开(公告)日：2002-04-23
申请号：US09710656
申请日：2000-11-09
申请人： Andrew J. Lammas , Philip W. Dietz
发明人： Andrew J. Lammas , Philip W. Dietz
IPC分类号： F01D102
CPC分类号： F04D29/644 , F01D5/005 , F01D5/025 , F01D5/34 , F04D29/321 , F05D2230/642 , F05D2230/70 , F05D2230/80 , Y02T50/671 , Y02T50/673
摘要： A compressor rotor includes coaxially adjoining disks having corresponding rows of rotor blades. A forward shaft is affixed to a forward disk and includes an annular seat for being mounted in a bearing to support the rotor at its forward end. A blisk coaxially surrounds the shaft axially between the seat and forward disk, and is removably fixedly joined piggyback to the shaft. In a repair method, the blisk may be removed from the compressor rotor without requiring teardown of the compressor rotor itself.
摘要翻译： 压缩机转子包括具有相应行转子叶片的同轴相邻盘。 前轴固定到前盘，并且包括一个环形座，用于安装在轴承中以支撑转子在其前端。 叶片同轴地轴套在座椅和前盘之间围绕轴，并且可拆卸地固定地连接到轴上。 在修理方法中，叶片可以从压缩机转子中移除，而不需要拆除压缩机转子本身。
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公开(公告)号：US06174130B1
公开(公告)日：2001-01-16
申请号：US09345191
申请日：1999-06-30
IPC分类号： F01D1712
CPC分类号： F01D17/162 , F16C3/12 , F16C3/22 , F16C2226/60 , F16C2360/23
摘要： A shaft assembly for movement of an array of adjustable members comprises a hollow shaft body including a shaft body wall with a wall outer surface. A plurality of spaced apart clevises, secured with the shaft body wall on the wall outer surface, each includes connection means disposed away from the wall outer surface for connection with an actuator for movement of the adjustable members.
摘要翻译： 用于移动可调节构件阵列的轴组件包括中空轴体，其包括具有壁外表面的轴体壁。 在壁外表面上固定有轴体壁的多个间隔开的夹子各自包括远离壁外表面设置的连接装置，用于与用于可调节构件的运动的致动器连接。
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