公开(公告)号：US11428106B2

公开(公告)日：2022-08-30

申请号：US16645013

申请日：2018-09-17

申请人： SULZER TURBO SERVICES VENLO B.V.

发明人： Jozef H. G. Mattheij ,  Twan Antonius Martinus Althuizen

IPC分类号： F01D5/24 ,  F01D25/24 ,  F01D9/04

摘要： A vane assembly includes a plurality of vane units and a connecting part. Each vane unit includes a base having a through-hole positioned between opposing longitudinal faces of the base. The connecting part includes a lacing bar that is insertable into and through the through-holes for coupling at least two adjacent vane units into the vane assembly. In the vane assembly the connecting part is arranged through the through holes of the plurality of vane units clamping the vane units on the lacing bar.

公开(公告)号：US11280198B2

公开(公告)日：2022-03-22

申请号：US16675918

申请日：2019-11-06

申请人： GENERAL ELECTRIC COMPANY

发明人： Arnab Sen ,  Jeffrey Douglas Rambo ,  Rajesh Kumar ,  Bhaskar Nanda Mondal ,  Alan Roy Stuart ,  Robert Proctor ,  Christopher Charles Glynn

IPC分类号： F01D5/24 ,  F01D5/08 ,  F01D1/24 ,  F02K3/072 ,  F01D11/00 ,  F02C7/18 ,  F01D25/14 ,  F02C7/12 ,  F01D1/26

摘要： An apparatus for a turbine engine comprising an outer casing, an engine core provided within outer casing and having a at least one set of blades, and through which gasses flow in a forward to aft direction, an outer drum located within the outer casing to define an annular cavity. A set of seals extending between the first surface and the second surface to define at least one cooled cavity within the annular cavity.

公开(公告)号：US09410433B2

公开(公告)日：2016-08-09

申请号：US13812035

申请日：2011-07-20

申请人： Damien Alquier ,  Jacques Auguste Amedee Boury ,  Pascal Courtin ,  Huu-Thanh Tran

发明人： Damien Alquier ,  Jacques Auguste Amedee Boury ,  Pascal Courtin ,  Huu-Thanh Tran

IPC分类号： F01D11/00 ,  F01D5/12 ,  F01D5/24

CPC分类号： F01D5/12 ,  F01D5/22 ,  F01D5/24 ,  F01D11/006 ,  F05D2250/231 ,  Y02T50/672

摘要： An inter-blade sealing for a turbine or compressor wheel of a turbine engine includes inserts engaged in longitudinal cavities in side edges of platforms of blades and bearing, in operation, against facing side edges of platforms of adjacent blades. Each insert has a cylindrical elongate shape and includes in its outer cylindrical surface at least one annular groove for passing platform cooling air.

摘要翻译： 用于涡轮发动机的涡轮机或压缩机叶轮的叶片间密封件包括在操作中接合在叶片和轴承的平台的侧边缘中的相对于相邻叶片的平台的相对侧边缘的纵向空腔中的插入件。 每个插入件具有圆柱形细长形状并且在其外圆柱形表面中包括至少一个用于使平台冷却空气通过的环形槽。

公开(公告)号：US5984638A

公开(公告)日：1999-11-16

申请号：US289795

申请日：1994-08-12

申请人： M. Theodore Gresh ,  Francis Kushner

发明人： M. Theodore Gresh ,  Francis Kushner

IPC分类号： F01D5/24

CPC分类号： F01D5/24

摘要： A compressor blade vibration reduction mechanism for a high-speed radial impeller for minimizing fatigue failures from various excitation sources. The vibration reduction mechanism includes a plurality of loose-fitting lashing pins coupling each impeller blade to an adjacent impeller blade. Each lashing pin extends through a first aperture in a blade located adjacent to the blade tip and through a second aperture of an adjacent blade. The second aperture of each blade is located a greater distance from the leading edge of the blade than the first aperture. The second aperture is located in an area of the blade having lower vibration during operation than the blade location where the first aperture is located.

摘要翻译： 一种用于使来自各种激发源的疲劳失效最小化的用于高速径向叶轮的压缩机叶片减振机构。 减振机构包括将每个叶轮叶片联接到相邻的叶轮叶片的多个松配合的捆扎销。 每个捆扎销延伸穿过位于叶片尖端附近并通过相邻叶片的第二孔的刀片中的第一孔。 每个叶片的第二个孔距离叶片的前缘比第一孔更远的距离。 第二孔位于叶片的操作中比在第一孔所在的叶片位置处具有较低振动的区域。

公开(公告)号：US5201850A

公开(公告)日：1993-04-13

申请号：US655701

申请日：1991-02-15

申请人： Christopher H. Lenhardt ,  Carl Grant ,  Chellappa Balan

发明人： Christopher H. Lenhardt ,  Carl Grant ,  Chellappa Balan

IPC分类号： F01D5/10 ,  F01D5/22 ,  F01D5/24

CPC分类号： F01D5/225 ,  F01D5/10 ,  F01D5/24 ,  F05D2260/96 ,  Y10S416/50

摘要： A rotor includes a disc having a plurality of blades extending therefrom. The blades include tip shrouds, each having first and second axial ends, and first and second circumferential faces. The first and second faces of adjacent tip shrouds are spaced from each other to define gaps therebetween. The first and second ends each include U-shaped slots, each having an arcuate damper wire disposed therein. The slots are aligned generally parallel to an axial centerline axis of the rotor for allowing ease of manufacture and assembly while providing effective frictional damping by the damper wires urged by centrifugal force against the slots.

摘要翻译： 转子包括具有从其延伸的多个叶片的盘。 叶片包括具有第一和第二轴向端部以及第一和第二圆周面的顶端罩。 相邻尖端护罩的第一和第二面彼此间隔开以限定它们之间的间隙。 第一和第二端各自包括U形槽，每个槽具有设置在其中的弧形阻尼丝。 槽大致平行于转子的轴向中心线排列，以允许易于制造和组装，同时通过由离心力推压到狭槽的阻尼丝提供有效的摩擦阻尼。

公开(公告)号：US4482296A

公开(公告)日：1984-11-13

申请号：US408228

申请日：1982-08-16

申请人： Mark E. Wassell ,  John G. Mosimann

发明人： Mark E. Wassell ,  John G. Mosimann

IPC分类号： F01D5/22 ,  F01D5/24 ,  F01D5/30 ,  F01D5/32

CPC分类号： F01D5/326 ,  F01D5/22 ,  F01D5/225 ,  F01D5/24 ,  F05D2260/96 ,  Y10S416/50

摘要： The Assembly has a submerged root, turbine-wheel-blading configuration, and utilizes circumferentially oriented, buried, friction damping wires, and continuous, overlapping, tip shrouds to minimize vibratory response. The wires, in the presence of blade vibration, simultaneously rub on both the blades and surfaces of a recess in the wheel in which the blade roots are fixed. The continuous tip shrouding provides additional damping through shroud-to-shroud interface rubbing. The assembly has a stack of identical blades, obviating any need for relatively weak locking blades or pieces. The method defines the steps of forming a peripheral recess in a wheel, in which to secure root ends of blades, and setting the damping wires (or wire) therein prior to installing the blade root ends, and uniformly spacing-apart the blades after securing the same to the wheel.

摘要翻译： 该组件具有淹没的根部，涡轮机叶轮构造，并且利用周向定向的，埋入的摩擦阻尼线以及连续的，重叠的尖端护罩以使振动响应最小化。 在刀片振动的情况下，电线同时摩擦在叶片根部固定的车轮上的凹槽的两个叶片和表面上。 连续的尖端护罩通过护罩对护罩接口摩擦提供额外的阻尼。 组件具有相同刀片的堆叠，消除了对相对较弱的锁定刀片或件的任何需要。 该方法限定了在车轮中形成周边凹槽的步骤，其中固定刀片的根部端部，并且在安装刀片根部末端之前将阻尼丝（或线）设置在其中，并且在固定之后均匀地间隔开刀片 相同的轮子。

公开(公告)号：US3857650A

公开(公告)日：1974-12-31

申请号：US40833573

申请日：1973-10-23

申请人： FIAT SPA

发明人： CERRATO R

IPC分类号： F01D5/22 ,  F01D21/04 ,  F01D5/24

CPC分类号： F01D21/045 ,  F01D5/225

摘要： A vaned rotor of the type comprising a central metal hub or rotor body carrying a plurality of rotor blades made of a ceramic material, in which the blades are simply located on the rotor body and held in place by a coil of carbon fibres or ceramic fibres which surrounds the blades. To form a support surface for the coil each blade has a transverse part at the radially outer end thereof, which is partly cylindrical and which together with the transverse parts of the other blades, forms a substantially cylindrical support surface for the coil.

摘要翻译： 一种包括中心金属毂或转子体的叶片式转子，该中心金属毂或转子体承载由陶瓷材料制成的多个转子叶片，其中叶片简单地位于转子体上并通过碳纤维或陶瓷纤维线圈保持在适当位置 其围绕叶片。 为了形成用于线圈的支撑表面，每个叶片在其径向外端处具有横向部分，该横向部分是部分圆柱形的，并且与其它叶片的横向部分一起形成用于线圈的基本上圆柱形的支撑表面。

公开(公告)号：US3719439A

公开(公告)日：1973-03-06

申请号：US3719439D

申请日：1971-04-06

申请人： ROLLS ROYCE

发明人： BRACEY K ,  DAWSON L ,  PETRIE J

IPC分类号： F01D5/22 ,  F01D5/24

CPC分类号： F01D5/22 ,  F01D5/24

摘要： A BLADED ROTOR FOR A GAS TURBINE ENGINE HAS A ROW OF BLADES, EACH BLADE HAVING TWO PART SPHERICALLY FACED DEPRESSIONS OF OPPOSITE FACES AND HOLES THROUGH THE BLADE THICKNESS WHICH LEAD INTO THE DEPRESSIONS. TIE MEMBERS EXTEND BETWEEN ADJACENT BLADES, THE ENDS OF THE TIE MEMBERS PASSING THROUGH THE HOLES AND BEING RETAINED BY PART SPHERICALLY FACE NUTS WHICH ENGAGE IN THE PART SPHERICAL DEPRESSIONS. THE TIE MEMBERS ARE THUS ALLOWED TO MOVE RELATIVE TO THE BLADES AND TO TAKE UP THE NATURAL POSITION WITHOUT STRESSING THE BLADE UNDULY.

公开(公告)号：US3708244A

公开(公告)日：1973-01-02

申请号：US3708244D

申请日：1971-04-09

申请人： ROLLS ROYCE

发明人： DAWSON L ,  PETRIE J ,  BRACEY K

IPC分类号： F01D5/22 ,  F01D5/10 ,  F01D5/24

CPC分类号： F01D5/22

摘要： A bladed rotor for a gas turbine engine comprising a row of blades in which each blade is tied to the next adjacent blade by a Z-shaped metal tie having a center section which is inwardly curved such that centrifugal forces acting on itself are evidenced as compressive stresses within the tie and end limbs or lugs extending from the center section in opposite directions generally chordally of the blades and each being attached to the blades by bolts spaced apart transversely of the blade, the bolts extending through the blade to also attach a similar limb or lug to the opposite blade face.

摘要翻译： 一种用于燃气涡轮发动机的叶片转子，其包括一排叶片，其中每个叶片通过Z形金属扎带固定在下一个相邻叶片上，该Z形金属扎带具有向内弯曲的中心部分，使得作用在其上的离心力被证明为压缩 从中心部分沿相反方向延伸的连接件和端部四肢或突出部内的应力通常与叶片并排，并且每个通过与叶片横向间隔开的螺栓附接到叶片，螺栓延伸穿过叶片，以连接相似的肢体 或凸耳到相对的刀片面。

公开(公告)号：US3601500A

公开(公告)日：1971-08-24

申请号：US3601500D

申请日：1969-08-12

申请人： ROLLS ROYCE

发明人： PALFREYMAN JACK ,  MIDDLETON HENRY EDWARD

IPC分类号： F04D29/32 ,  F01D5/22 ,  F01D5/24 ,  F01D21/04

CPC分类号： F01D21/045 ,  F01D5/225 ,  Y02T50/673

摘要： A rotor assembly for a fluid flow machine comprising a rotor hub member provided with a plurality of angularly spaced apart rotor blades, and at least one load-distributing member which transmits predetermined torsional loads between the various rotor blades, the load-distributing member being free to move with respect to all the rotor blades but engaging the latter to distribute the load whenever any rotor blade, as a result of the application thereto of such a predetermined torsional load, moves with respect to the remaining rotor blades.