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公开(公告)号：US4487550A
公开(公告)日：1984-12-11
申请号：US461424
申请日：1983-01-27
摘要： An improved high pressure turbine rotor blade and tip cap structure therefor is provided, which comprises, a plurality of metallic layers bonded to the tip end of the blade, each layer having a peipheral shape conforming to the camber of the blade, the layers defining a plurality of radially outwardly opening, serpentine-shaped passageways for passage of coolant fluid through the periphery of the tip end of the blade.
摘要翻译： 提供了一种改进的高压涡轮机转子叶片及其顶盖结构，其包括多个金属层，其结合到叶片的尖端，每层具有符合叶片外倾角的外围形状，这些层限定了 多个径向向外开口的蛇形通道，用于使冷却剂流体通过叶片末端的周边。
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公开(公告)号：US5131814A
公开(公告)日：1992-07-21
申请号：US505121
申请日：1990-04-03
申请人： James C. Przytulski , Richard L. Horvath , Philip H. Stoughton , Christopher C. Glynn , Richard A. Wesling , Robert J. Corsmeier
发明人： James C. Przytulski , Richard L. Horvath , Philip H. Stoughton , Christopher C. Glynn , Richard A. Wesling , Robert J. Corsmeier
CPC分类号： F01D5/3007 , Y02T50/671
摘要： A gas turbine engine having an outer annular turbine rotor, which is counterrotatable relative to an inner annular turbine rotor, includes attachment structure for attaching turbine blades in circumferential rows to the inner rotor. The attachment structure includes first and second male members of hook-like configurations spaced axially along and circumferentially extending about the rotor, and first and second grooves defined by flanges attached to the rotor and axially spaced along and circumferentially extending about the rotor. The grooves open in a common axial direction for receiving in mated relation respectively and concurrently the hook-like configured first and second male members. The attachment structure also includes several different locking arrangements for locking the male members in mated relation with the grooves to thereby restrain the turbine blade against radial and axial movements relative to the rotor. Some locking arrangements are adapted for locking all of the blades but a last or final one thereof in a circumferential row around the rotor. Other locking arrangements are adapted for locking all of the blades in the circumferential row. Still other locking arrangements are adapted for locking only the last or final blade to complete the circumferential row of blades.
摘要翻译： 具有外环形涡轮机转子的燃气涡轮发动机，其相对于内环形涡轮机转子可逆地旋转，包括用于将周向行中的涡轮叶片附接到内转子的附接结构。 附接结构包括钩状构造的第一和第二阳构件，所述第一和第二阳构件沿轴向并沿着转子周向延伸，以及由附接到转子并由轴向间隔开并围绕转子周向延伸的凸缘限定的第一和第二槽。 所述凹槽在共同的轴向方向上打开以分别接合并且同时形成钩状配置的第一和第二阳构件。 附接结构还包括几个不同的锁定装置，用于将阳构件与凹槽配合关系锁定，从而约束涡轮叶片抵抗相对于转子的径向和轴向运动。 一些锁定装置适用于锁定所有叶片，但是围绕转子的圆周排锁定其最后的或最后的叶片。 其他锁定装置适于锁定圆周排中的所有叶片。 还有其它锁定装置适于仅锁定最后的刀片或最终刀片以完成圆周排的刀片。
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公开(公告)号：US5131813A
公开(公告)日：1992-07-21
申请号：US505118
申请日：1990-04-03
CPC分类号： F01D5/3038 , F01D5/03 , F01D9/042 , Y02T50/673
摘要： A gas turbine engine having an outer annular turbine rotor, which is counterrotatable relative to an inner annular turbine rotor, includes attachment structure for attaching turbine blades in circumferential rows to the outer rotor. The attachment structure includes first and second male members spaced axially along and circumferentially extending about the rotor, and first and second grooves spaced axially along and extending circumferentially about the rotor being defined by flanges attached to the rotor. Each male member has a first portion attached to an end of a turbine blade and extending therefrom in a radial direction. The first male member has a second portion attached to its first portion and extending therefrom in an axial direction to define the first male member with an overall hook-like cross-sectional configuration. The first groove is cross-sectionally shaped for receiving in mated relation the second portion of the first male member. The second groove is cross-sectionally shaped for receiving in mated relation in the second groove a lock segment of the locking assembly and the first portion of the second male member to lock the male members in the respective grooves and thereby lock the turbine blade against radial and axial movements relative to the rotor.
摘要翻译： 具有外环形涡轮机转子的燃气涡轮发动机，其相对于内部环形涡轮机转子可反转，包括用于将涡轮机叶片以周向排附接到外转子的附接结构。 附接结构包括沿着转子轴向间隔开并在周向上延伸的第一和第二阳构件，并且围绕转子沿轴向间隔开并且围绕转子周向延伸的第一和第二槽由连接到转子的凸缘限定。 每个阳构件具有附接到涡轮叶片的端部并且沿径向方向从其延伸的第一部分。 第一阳构件具有附接到其第一部分的第二部分并且在轴向方向上从第二部分延伸以限定具有整体钩状横截面构造的第一阳构件。 第一槽是横截面形状的，用于以配合的关系接收第一阳构件的第二部分。 第二凹槽是横截面形状的，用于在第二凹槽中以配合关系接收锁定组件的锁定段和第二阳构件的第一部分，以将阳构件锁定在相应的凹槽中，从而将涡轮叶片锁定在径向 和相对于转子的轴向移动。
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4.发明授权Interstage seal arrangement for airfoil stages of turbine engine counterrotating rotors 失效涡轮发动机调速转子的飞行器间隔密封安装
公开(公告)号：US5197281A
公开(公告)日：1993-03-30
申请号：US505120
申请日：1990-04-03
CPC分类号： F01D11/001 , B64C11/48 , F01D11/12 , F01D5/225 , F02K3/072 , Y10T29/49321
摘要： A gas turbine engine has outer and inner counterrotatable annular turbine rotors and pluralities of turbine blades disposed in alternating rows and mounted on and extending between the respective rotors. An interstage seal arrangement for the engine is composed of a sequence of alternating inner and outer seals. Each outer seal is disposed between an interior side of the outer rotor and outer ends of the blades in one plurality thereof being spaced radially inward at their outer ends from the outer rotor and being mounted at their inner ends to the exterior side of the inner rotor. Each inner seal is disposed between the exterior side of the inner rotor and inner ends of the blades in another plurality thereof being spaced radially outward at their inner ends from the inner rotor and being mounted at their outer ends to the interior side of the outer rotor. Each inner seal is composed of an annular honeycomb component attached to the blade inner ends and a plurality of annular seal elements or teeth mounted on the exterior side of the inner rotor and projecting radially outwardly therefrom for sealably interfacing with the honeycomb component concurrently as the outer and inner rotors counterrotate relative to one another.
摘要翻译： 燃气涡轮发动机具有外部和内部可反向旋转的环形涡轮转子和多个涡轮叶片，其以交替的排布置并安装在各个转子之间并在相应的转子之间延伸。 用于发动机的级间密封装置由一系列交替的内密封件和外密封件组成。 每个外部密封件设置在外部转子的内侧和多个叶片的外端之间，在其外端处与外转子径向向内间隔开，并且其内端安装在内转子的外侧 。 每个内密封件设置在内转子的外侧和另一多个叶片的内端之间，在其内端处与内转子径向向外间隔开，并且其外端安装在外转子的内侧 。 每个内密封件由附接到叶片内端的环形蜂窝构件和安装在内转子的外侧上并从其径向向外突出的多个环形密封元件或齿组成，以与蜂窝构件同时作为外部密封连接 并且内转子相对于彼此逆转。
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公开(公告)号：US5119565A
公开(公告)日：1992-06-09
申请号：US770441
申请日：1991-10-03
申请人： James Horvath , Richard L. Horvath
发明人： James Horvath , Richard L. Horvath
IPC分类号： G01C9/28
CPC分类号： G01C9/28
摘要： A corner level apparatus arranged for alignment of structural components at a corner intersection includes intersecting first and second arms, wherein the arms define an acute included angle therebetween, generally at forty-five degrees. A mount projects rearwardly of the junction for securement of a spirit level arranged parallel to a top surface of the first and second arms. A modification of the invention includes support legs telescopingly and adjustably mounted relative to a bottom surface of the arms projecting downwardly therefrom for support of the level structure for use as a gauge and a securement of various structural components at the corner intersection of a dwelling, wherein the apparatus in a further refinement includes chalk lines retractably mounted within each of the arms for alignment of the arms and use of the chalk line as a gauge in structural construction.
摘要翻译： 布置成用于在角部交叉处对准结构部件的角落级装置包括相交的第一和第二臂，其中臂之间限定了锐角，一般为四十五度。 安装座在接合处向后突出以确保平行于第一和第二臂的顶表面布置的水平线。 本发明的修改包括相对于从其向下突出的臂的底表面可伸缩并可调节地安装的支撑腿，用于支撑水平结构以用作尺度和在住宅的拐角交叉处固定各种结构部件，其中 该装置在进一步的改进中包括可伸缩地安装在每个臂内的用于对准臂的白垩线和使用粉笔线作为结构构造的量规。
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公开(公告)号：US4540339A
公开(公告)日：1985-09-10
申请号：US616380
申请日：1984-06-01
申请人： Richard L. Horvath
发明人： Richard L. Horvath
IPC分类号： F01D5/20
CPC分类号： F01D5/20
摘要： An improved high pressure turbine rotor blade and tip cap structure therefor is provided which comprises a tip end closure for the blade bonded to the end wall of the blade casting and including a base plate member and a pair of upstanding side walls defining a peripheral contour coincidental with and faired to the cambered side walls of the casting, the base plate member having a plurality of radially outwardly opening passageways therethrough and disposed along the chord of the blade and communicating with a channel included in the radially outwardly facing surface of the casting along a chord of the blade, the passageways disposed along axes at angles to the base plate whereby coolant fluid flowing therethrough is directed against the tip side wall surfaces; and opening is provided through the end wall of the casting in the form of a slit or a plurality of holes along the chord of the blade and intersecting the channel, to define an outlet through the end wall for passage of coolant fluid through the blade.
摘要翻译： 提供了一种改进的高压涡轮机转子叶片及其顶盖结构，其包括用于叶片的尖端封闭件，其结合到叶片铸件的端壁，并且包括底板构件和一对直立侧壁，其限定了外周轮廓巧合 与铸件的弧形侧壁相连接，基板构件具有多个径向向外开口的通道，沿着叶片的弦线设置，并且沿铸造件的径向向外的表面中包括的通道沿着 所述通道沿着轴线与所述基板成角度设置，由此流过其中的冷却剂流体被引向所述末端侧壁表面; 并且开口通过铸件的端壁以沿刀片的弦线的狭缝或多个孔的形式提供，并且与通道相交，以限定通过端壁的出口，用于使冷却剂流体通过刀片。
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