公开(公告)号：US20070172348A1

公开(公告)日：2007-07-26

申请号：US11656394

申请日：2007-01-23

Applicant: Josef Battig

Inventor： Josef Battig

IPC: F04D29/56

CPC classification number: F01D17/165 ,  F04D29/462 ,  F05D2220/40 ,  F05D2260/50

Abstract: A guide device with adjustable guide vanes is provided with a drive for the adjustable guide vanes, in which a cylindrical driving pin and an adjusting lever are provided each with one surface pair which are matched to one another and which slide on one another in operation when the guide vanes are being adjusted. To adjust the guide vanes, the adjusting ring is moved, by which the driving pin attached to the adjusting ring slides in an elongated groove of the adjusting lever and applies a force to the adjusting lever. This approach yields an economical and durable structure which is easy to install. This results in surface support with the corresponding low compressive loads per unit area and consequently greatly reduced wear.

Abstract translation: 具有可调节导向叶片的引导装置设置有用于可调节导向叶片的驱动器，其中设置有圆柱形驱动销和调节杆，每个具有彼此匹配的一个表面对，并且在操作中彼此滑动， 导叶正在调整。 为了调整导向叶片，调节环被移动，通过该调节环，安装在调节环上的驱动销通过该调节环在调节杆的细长槽中滑动并向调节杆施加力。 这种方法产生经济耐用的结构，易于安装。 这导致表面支撑与每单位面积相应的低压缩载荷，从而大大减少磨损。

公开(公告)号：US20070172347A1

公开(公告)日：2007-07-26

申请号：US11654600

申请日：2007-01-18

Applicant: Josef Battig ,  Jean-Yves Werro ,  Janpeter Kuhnel

Inventor： Josef Battig ,  Jean-Yves Werro ,  Janpeter Kuhnel

IPC: F04D29/56

CPC classification number: F01D17/165 ,  F05D2220/40

Abstract: Guide vanes are supported in a two-part or multipart housing (32, 33). Housing separation takes place radially in the region of the bearing point (25) of the vane shaft so that the separating joint (36) between the housing parts (32, 33) leads through the bearing openings (34) which are designed to hold the vane shafts. The completely round opening (34) leads to the bearing point of the vane shaft having large-area support in any position. Thus high surface pressures can be avoided.

Abstract translation: 导叶支撑在两部分或多部分壳体（32,33）中。 壳体分离在叶片轴的轴承点（25）的区域中径向地发生，使得壳体部件（32,33）之间的分离接头（36）穿过轴承开口（34），轴承开口（34）被设计成保持 叶片轴。 完全圆形的开口（34）导致叶片轴的轴承点在任何位置具有大面积的支撑。 因此可以避免高表面压力。

公开(公告)号：US5052825A

公开(公告)日：1991-10-01

申请号：US432734

申请日：1989-10-30

Applicant: Josef Battig

Inventor： Josef Battig

IPC: F16C23/00 ,  F16C23/04 ,  G04B31/02

CPC classification number: F16C23/04 ,  F16C2360/24

Abstract: The axial mounting with skewing compensation for a turbomachine has a fastening flange (1) and a bearing housing (2) which is in one piece with the latter and which is subdivided into a middle housing part (9) and an outer housing part (10) by means of at least one pair of slots (4,7) in two respective planes. The slots (4,7) are widened in a lobe-like manner at their ends, and these ends respectively limit at least one pair of webs (5,8) located diametrically opposite one another in the said planes. These webs (5,8) perform the function of rigid joints for damping angular deflections of the shaft which are caused by operating loads. The webs (5,8) of the two planes are offset relative to one another by 90.degree., generally by the amount of half their circumferential division.

Abstract translation: PCT No.PCT / CH89 / 00058 Sec。 371日期：1989年10月30日 102（e）日期1989年10月30日PCT 1989年3月22日PCT公布。 公开号WO89 / 09345 日期为1989年10月5日。用于涡轮机的偏斜补偿的轴向安装具有紧固凸缘（1）和与后者成一体的轴承壳体（2），并且被分为中间壳体部件（9） 以及通过在两个相应平面中的至少一对槽（4,7）的外壳体部分（10）。 狭槽（4,7）在其端部以波瓣状加宽，并且这些端部分别限制在所述平面中彼此径向相对的至少一对腹板（5,8）。 这些腹板（5,8）执行刚性接头的功能，用于阻止由操作负载引起的轴的角度偏转。 两个平面的腹板（5,8）相对于彼此偏移90°，通常以其半周分数的量偏移。

公开(公告)号：US07240892B2

公开(公告)日：2007-07-10

申请号：US10500887

申请日：2003-01-15

Applicant: Josef Battig

Inventor： Josef Battig

IPC: F16M1/00 ,  F16M3/00 ,  F16M5/00 ,  F16M7/00

CPC classification number: F02B67/10 ,  F01D25/28 ,  F02C6/12 ,  F05D2220/40

Abstract: The invention proposes a securing device (26) for securing a turbocharger (12) comprising a turbocharger casing (14) to a base (28). The securing device (26) has a first foot (30) which can be fixed in the base (28) and a second foot (32) which can be fixed in the base (28), it being possible for the two feet (30, 32) to be connected to the turbocharger casing (14) at an axial distance from one another. The second foot (32) has a casing connection region (34), which can be connected to the turbocharger casing (14), and a base connection region (36), which can be connected to the base (28). The casing connection region (34) is designed in the form of a partial circle arc or circle arc. An axial strut arrangement (38) connects the casing connection region (34) and the base connection region (36) and includes an angle α in the range from 0° to 60° with the base (28).

Abstract translation: 本发明提出一种用于将包括涡轮增压器壳体（14）的涡轮增压器（12）固定到基座（28）的固定装置（26）。 固定装置（26）具有可固定在基座（28）中的第一脚（30）和可固定在基座（28）中的第二脚（32），两脚（30 ，32）以彼此轴向距离连接到涡轮增压器壳体（14）。 第二脚（32）具有可连接到涡轮增压器壳体（14）的壳体连接区域（34）和可连接到基座（28）的基座连接区域（36）。 壳体连接区域（34）被设计成部分圆弧或圆弧的形式。 轴向支柱装置（38）连接壳体连接区域（34）和基座连接区域（36），并且包括与基座（28）在0°至60°范围内的角度α。

公开(公告)号：US20070140846A1

公开(公告)日：2007-06-21

申请号：US11703741

申请日：2007-02-08

Applicant: Peter Schellenberg ,  Detlef Behrendt ,  Josef Battig ,  Michael Jung ,  Ferdinand Mueller

Inventor： Peter Schellenberg ,  Detlef Behrendt ,  Josef Battig ,  Michael Jung ,  Ferdinand Mueller

IPC: F01D25/00

CPC classification number: F01D25/002 ,  F05D2220/40 ,  F05D2240/12 ,  F05D2260/607

Abstract: The cleaning device for the exhaust gas turbine comprises openings, which open out into the flow duct upstream of the nozzle ring, for injecting a cleaning liquid from the radially inner side into the annular flow duct, a cavity, which is connected to the openings, for distributing the cleaning liquid to the openings, and a supply line for supplying the cleaning liquid to the cavity. The cleaning device according to the invention provides a uniform distribution of water to nozzle ring or to the rotor blades of the turbine rotor wheel.

Abstract translation: 用于废气涡轮机的清洁装置包括开口，该开口在喷嘴环的上游开口流入管道，用于将清洁液体从径向内侧注入到环形流动管道中，连接到开口的空腔， 用于将清洁液分配到开口，以及用于将清洁液供给到空腔的供应管线。 根据本发明的清洁装置提供水到喷嘴环或涡轮转子轮的转子叶片的均匀分布。

公开(公告)号：US20050232775A1

公开(公告)日：2005-10-20

申请号：US10512581

申请日：2003-05-05

Applicant: Martin Thiele ,  Janpeter Kuhnel ,  Josef Battig

Inventor： Martin Thiele ,  Janpeter Kuhnel ,  Josef Battig

IPC: F01D5/04 ,  F01D1/00 ,  F01D5/02 ,  F01D11/02 ,  F01D25/16 ,  F02B39/00 ,  F04D29/26 ,  F16D1/06 ,  F16D1/08 ,  B63H1/20

CPC classification number: F04D29/266 ,  F01D5/025 ,  F05D2220/40 ,  F16D1/0835 ,  F16D1/0852 ,  F16D2001/062

Abstract: The fastening arrangement (26) for an impeller (22) on a shaft (14), in particular for an impeller (22) of a turbocharger on a turbocharger shaft (14), comprises a bush (34), which can be screwed onto a shaft journal (20) of the shaft (14), and a shaft-side hub extension (30) of the impeller (22) having a central recess (32), into which the bush (34) can be inserted in a frictional manner. The hub extension (30), at least in the region of its shaft-side end, is designed approximately in the form of a hollow cylinder. The fastening arrangement (26) also comprises a press sleeve (36) which can be frictionally connected radially on the outside to the hub extension (30).

Abstract translation: 用于在轴（14）上的叶轮（22）的紧固装置（26），特别是用于涡轮增压器轴（14）上的涡轮增压器的叶轮（22）的紧固装置（26）包括衬套（34​​），其可以拧到 所述轴（14）的轴颈（20）和所述叶轮（22）的轴侧轮毂延伸部（30）具有中心凹部（32），所述衬套（34​​）可以以摩擦 方式。 至少在其轴侧端部的区域中，轮毂延伸部（30）被设计成大致为中空圆柱体的形式。 紧固装置（26）还包括压力套筒（36），其能够在外部径向地摩擦连接到轮毂延伸部（30）上。

公开(公告)号：US5803612A

公开(公告)日：1998-09-08

申请号：US818981

申请日：1997-03-14

Applicant: Josef Battig

Inventor： Josef Battig

IPC: F02B39/00 ,  F01D25/16 ,  F04D29/056 ,  F04D29/059 ,  F16C27/00 ,  F16C27/04

CPC classification number: F16C19/542 ,  F01D25/164 ,  F16C27/045 ,  F05D2240/515 ,  F05D2250/42 ,  F16C2360/24

Abstract: The object of the invention is to provide an improved bearing support arrangement for rapidly rotating rotors, with which arrangement the service life of the bearing device is increased and both its fabrication costs and the expenditure on assembly are reduced. This is achieved according to the invention in that the bearing support arrangement (10) is of one-piece design. It comprises an outer flange (11) connected to the housing (2), a gimbal ring (12) and an inner bearing bush (13) which receives the bearing or the bearings (3). In each case a circumferential slot (14, 15) is formed both between the gimbal ring (12) and the outer flange (11) and between the gimbal ring (12) and the bearing bush (13). The gimbal ring (12) is respectively connected to the bearing bush (13) and to the outer flange (11) via two inner and two outer webs (16, 17) which interrupt the respective circumferential slot (14, 15). The annular gap (25) is formed between the bearing bush (13) and the housing (2) and is arranged axially offset with respect to the gimbal ring (12). At least one centering surface (22, 23) is arranged both on the outer flange (11) and on the housing (2), the said centering surfaces (22, 23) being arranged so as to correspond to one another and so as to be concentric with respect to the bearing/bearings (3).

Abstract translation: 本发明的目的是提供一种用于快速旋转转子的改进的轴承支撑装置，利用该轴承支撑装置，轴承装置的使用寿命增加，并且其制造成本和装配成本都降低。 这是根据本发明实现的，因为轴承支撑装置（10）是一体式设计的。 其包括连接到壳体（2）的外部凸缘（11），容纳轴承或轴承（3）的万向环（12）和内部轴承衬套（13）。 在每种情况下，在万向环（12）和外凸缘（11）之间以及在万向环（12）和轴承衬套（13）之间形成圆周槽（14,15）。 万向节环（12）分别通过中断相应的周向槽（14,15）的两个内部腹板（16,17）连接到轴承衬套（13）和外部凸缘（11）。 环形间隙（25）形成在轴承衬套（13）和壳体（2）之间，并且相对于万向环（12）轴向偏移地布置。 至少一个定心表面（22,23）均布置在外凸缘（11）和壳体（2）上，所述对中表面（22,23）被布置成彼此对应，以便 与轴承（3）相同。

公开(公告)号：US5743707A

公开(公告)日：1998-04-28

申请号：US742810

申请日：1996-11-01

Applicant: Josef Battig ,  Mehmet Guven Kutay

Inventor： Josef Battig ,  Mehmet Guven Kutay

IPC: F16J15/32 ,  F16C33/78 ,  F16J9/00 ,  F16J15/16 ,  F16J15/44 ,  F01D11/00

CPC classification number: F16J15/164 ,  F16C2360/24

Abstract: A contact seal for turboengines is disclosed which is suitable for high circumferential speeds and high temperatures. The contact seal is of at least a two-part design and includes a thin carrier ring and a sealing ring. The sealing ring is constructed from a wear, oil, and heat resistant material, while the carrier ring includes an elastic material which is completely reversible even under high loads, and preferably is constructed of spring steel. The carrier ring has an inner fastening pan and an outer carrying part. The carrying part is positively connected to the sealing ring. The carrying part is designed to be inclined in the direction of the sealing face.

Abstract translation: 公开了用于涡轮机的接触密封件，其适用于高圆周速度和高温度。 接触密封件至少具有两部分设计，并且包括薄的载体环和密封环。 密封环由耐磨，耐油和耐热材料构成，而承载环包括即使在高负载下也完全可逆的弹性材料，并且优选地由弹簧钢构成。 承载环具有内紧固盘和外承载部。 承载部分与密封环正确连接。 承载部被设计成沿着密封面的方向倾斜。

公开(公告)号：US4734010A

公开(公告)日：1988-03-29

申请号：US860827

申请日：1986-05-08

Applicant: Josef Battig

Inventor： Josef Battig

IPC: F01D5/26 ,  F01D5/22 ,  F16F15/12 ,  F16F15/133

CPC classification number: F01D5/22 ,  Y10S416/50

Abstract: The present invention relates to a damping element for independent blades of a turbomachine in which the blades fastened in the rotor are connected together, preferably in the radially outer region, the connection between two blades consists of an elastically deformable platelet curved towards the center of the rotor, which platelet engages in retention features on the suction side of one blade and on the pressure side of a second, neighboring blade. The retention features on the blades can be either recesses or protruding lugs, in or on which the platelets are supported.

Abstract translation: 本发明涉及一种用于涡轮机的独立叶片的阻尼元件，其中固定在转子中的叶片优选地连接在一起，优选在径向外部区域中，两个叶片之间的连接由朝向中心的弯曲的可弹性变形的小片组成 转子，哪个血小板与一个叶片的吸入侧和第二个相邻叶片的压力侧的保持特征接合。 叶片上的保持特征可以是在支撑血小板的或在其上的凹槽或突出的凸耳。