公开(公告)号：US20140286758A1

公开(公告)日：2014-09-25

申请号：US14190814

申请日：2014-02-26

Applicant: ABB TURBO SYSTEMS AG

Inventor： Stephan M. Senn

IPC: F02B37/22

CPC classification number: F02B37/22 ,  F01D9/041 ,  F05D2220/40 ,  F05D2260/961

Abstract: A segmented nozzle ring is disclosed having a throat area between neighboring vanes that is the same for each segment which is achieved by rotation (i.e., opening or closing of the throat area) of the individual vane compounds belonging to the different segments. The resulting uniform throat area leads to a uniform exit flow angle of the nozzle and a uniform inlet flow angle of the rotor. As a result, high-cycle fatigue excitations of the rotor caused by the non-uniform flow can be eliminated, the thermodynamic efficiency of the turbine stage can be improved, and the nozzle ring need not be arranged in a fixed position relative to the gas inlet casing.

Abstract translation: 公开了一种分段喷嘴环，其具有在相邻叶片之间的喉部区域，其对于通过属于不同段的各个叶片化合物的旋转（即，打开或关闭喉部区域）而实现的每个段相同。 所产生的均匀的喉部区域导致喷嘴的均匀出口流动角度和转子的均匀的入口流动角度。 结果，可以消除由不均匀流动引起的转子的高循环疲劳激励，可以提高涡轮级的热力学效率，并且喷嘴环不需要相对于气体布置在固定位置 入口外壳。

公开(公告)号：US20140140834A1

公开(公告)日：2014-05-22

申请号：US14083025

申请日：2013-11-18

Applicant: ABB Turbo Systems AG

Inventor： Matthias RICHNER ,  Josef BÄTTIG

IPC: F01D25/24

CPC classification number: F01D25/246 ,  F01D9/042 ,  F01D17/165 ,  Y10T29/49316

Abstract: An exemplary nozzle ring has two fastening rings and a plurality of guide vanes, wherein holes are provided in one of the fastening rings for accommodating pins of the guide vanes, and openings are provided in the other fastening ring for accommodating positioning aids on the guide vanes.

Abstract translation: 示例性喷嘴环具有两个紧固环和多个导向叶片，其中一个紧固环中的孔中设置有用于容纳导向叶片的销的孔，并且在另一紧固环中设置开口，用于在导向叶片上容纳定位助剂 。

公开(公告)号：US20040055299A1

公开(公告)日：2004-03-25

申请号：US10660498

申请日：2003-09-12

Applicant: ABB Turbo Systems AG

Inventor： Olivier Bernard

IPC: F02B033/44

CPC classification number: F02B37/16 ,  F02D41/0007 ,  Y02T10/144

Abstract: A method for operating an exhaust gas turbocharger serving for charging an internal combustion engine, in which a main flow of a gas is supplied to a compressor (14) of the exhaust gas turbocharger via an intake line (26), is compressed in the compressor (14) and is led into an intake duct of the internal combustion engine via a compressor line. The gas quantity transferred to the combustion chambers of the internal combustion engine via the intake duct is regulated by means of a throttle valve (36) arranged between the compressor (14) and the combustion chambers. When a vacuum occurs in the region downstream of the compressor (14) between the compressor (14) and the throttle valve (36), as compared with the pressure in the intake line (26) upstream of the compressor (14), this vacuum is utilized in order to generate a bypass flow (B) which is branched off upstream of the compressor (14) from the main flow led by the compressor (14), flows around the compressor (14) from its side located upstream to its side located downstream and is returned into the main flow again downstream of the compressor (14) and upstream of the throttle valve (36).

Abstract translation: 一种用于对内燃机进行充气的排气涡轮增压器的操作方法，其中气体的主流经由进气管路（26）供给到排气涡轮增压器的压缩机（14），在压缩机 （14），经由压缩机管路引导到内燃机的进气管道。 通过进气管道传递到内燃机的燃烧室的气体量通过布置在压缩机（14）和燃烧室之间的节流阀（36）来调节。 当在压缩机14与节流阀36之间的压缩机14的下游区域发生真空时，与压缩机14的上游的进气管路26的压力相比，该真空 被利用以产生从压缩机（14）引导的主流体在压缩机（14）的上游分支的旁通流（B），其从位于其上游侧的一侧流过压缩机（14） 位于下游，并且在压缩机（14）的下游和节流阀（36）的上游再次返回主流。

公开(公告)号：US10473115B2

公开(公告)日：2019-11-12

申请号：US15630938

申请日：2017-06-22

Applicant: ABB Turbo Systems AG

Inventor： Christian Kreienkamp ,  Armin Reichl ,  Daniel Rusch

IPC: F04D29/44 ,  F04D29/58 ,  F04D29/68 ,  F04D27/02

Abstract: The present disclosure relates to a diffuser for a radial compressor. The diffuser may comprise a diffusor duct portion formed by first and second side walls that are arranged so as to diverge at least partially from one another in a direction of flow, a blade ring having a number of blades arranged at least partially in the diffusor duct portion with each blade having a pressure side and a suction side delimited by a blade leading edge and by a blade trailing edge of the respective blade, a number of pressure equalizing openings incorporated into at least one of the first and second side walls of the diffuser duct portion in a region where the first and second side walls diverge from one another with each of the pressure equalizing openings being arranged between the pressure side of one blade and the suction side of an adjacent blade of the blade ring, and a first annular duct arranged behind the pressure equalizing openings and fluidically connected to the diffuser duct portion via at least two of the pressure equalizing openings, such that a number of regions between two adjacent blades of the blade ring in the diffuser duct portion are fluidically connectable together.

公开(公告)号：US20160208821A1

公开(公告)日：2016-07-21

申请号：US15075646

申请日：2016-03-21

Applicant: ABB Turbo Systems AG

Inventor： Christoph Morath ,  Stefan Gantert

IPC: F04D29/62 ,  F01D5/06 ,  F04D29/28 ,  F02C6/12

CPC classification number: F04D29/626 ,  F01D5/025 ,  F01D5/06 ,  F02C6/12 ,  F04D29/284 ,  F05D2220/40 ,  F05D2230/60

Abstract: The exhaust turbocharger comprises a turbine having a turbine wheel and a compressor having a compressor wheel. The turbine wheel and the compressor wheel are connected by a shaft rotatably mounted in a bearing housing. A means for axially securing the shaft and the turbine wheel connected thereto is provided between the compressor wheel and the turbine wheel, wherein this means for axial securing limits an axial movement of the shaft and of the turbine wheel connected thereto in the direction of the turbine in the event of the compressor wheel bursting.The means for axially securing the shaft and the turbine wheel connected thereto comprises a component which is connected to the shaft or mounted on the shaft and is fixed in the axial direction in the housing. According to the application, this component for axially securing is screwed onto the shaft during mounting.

Abstract translation: 排气涡轮增压器包括具有涡轮机叶轮的涡轮机和具有压缩机叶轮的压缩机。 涡轮机叶轮和压缩机叶轮通过可旋转地安装在轴承壳体中的轴连接。 设置在压缩机叶轮和涡轮机叶轮之间的用于轴向固定轴和连接到其上的涡轮机的装置，其中用于轴向固定的装置限制了轴和连接到其上的涡轮机的涡轮机在涡轮机的方向上的轴向运动 在压缩机轮胎爆裂的情况下。 用于轴向固定轴和连接到其上的涡轮机的装置包括连接到轴上或安装在轴上并在壳体中沿轴向固定的部件。 根据应用，这种用于轴向固定的部件在安装时被拧到轴上。

公开(公告)号：US20140251719A1

公开(公告)日：2014-09-11

申请号：US14199583

申请日：2014-03-06

Applicant: ABB TURBO SYSTEMS AG

Inventor： Heinz-Jürgen FELD ,  Llija Mrvelj ,  Philipp Meyer

IPC: F02M35/12

CPC classification number: F02M35/1272 ,  F02C7/045 ,  F04D25/024 ,  F04D29/4213 ,  F04D29/664 ,  F04D29/701 ,  F05D2220/40

Abstract: A sound attenuator on the intake side of a compressor of an exhaust-gas turbocharger includes a tubular sound attenuator housing, which encases a flow duct between a face-side inlet opening and a rear-side outlet opening. A holding plate is provided in the sound attenuator housing in the flow direction and is perforated in the flow direction. For example, the holding plate can have a multiplicity of holes extending in the flow direction. The sound attenuator on the intake side of the compressor of an exhaust-gas turbocharger has a compact, lightweight and inexpensive structural form. The intake air is subjected to low resistance as it flows through the attenuation elements.

Abstract translation: 在排气涡轮增压器的压缩机的进气侧的声音衰减器包括管状声音衰减器壳体，其在面侧入口和后侧出口之间包围流路。 声音衰减器壳体沿流动方向设置保持板，并沿流动方向穿孔。 例如，保持板可以具有沿流动方向延伸的多个孔。 废气涡轮增压器的压缩机进气侧的声音衰减器具有紧凑，重量轻且价廉的结构形式。 进气在流经衰减元件时经受低阻力。

公开(公告)号：US20140241887A1

公开(公告)日：2014-08-28

申请号：US14268466

申请日：2014-05-02

Applicant: ABB Turbo Systems AG

Inventor： Peter NEUENSCHWANDER ,  Bruno Ammann ,  Marco Di Pietro ,  Markus Städeli

IPC: F01D25/16 ,  F01D25/18 ,  F04D29/057

CPC classification number: F01D25/168 ,  F01D25/18 ,  F04D29/057 ,  F05D2240/53 ,  F16C17/04 ,  F16C17/18 ,  F16C33/1075 ,  F16C2360/24

Abstract: A hydrodynamic axial bearing for mounting a shaft which is mounted rotatably in a bearing housing, including an axial stop of the bearing housing and a bearing comb which rotates with the shaft. A lubricating gap, which is loaded with lubricating oil and is delimited by a profiled circular ring face and a sliding face, being formed between the axial stop and the bearing comb. The profiled circular ring face and the sliding face are configured in such a way that the lubricating gap is constricted radially to the outside with regard to the axial direction. As a result, temperature deformations which occur during operation and deformations on account of centrifugal, shearing and other forces in the bearing comb can be compensated for.

Abstract translation: 一种用于安装轴的流体动力轴向轴承，其可旋转地安装在轴承壳体中，包括轴承壳体的轴向止动件和与轴一起旋转的轴承梳齿。 润滑间隙，其装载有润滑油并由形状圆形的环面和滑动面限定，形成在轴向止动件和轴承梳之间。 异形圆环面和滑动面构成为使得润滑间隙相对于轴向朝向外侧径向收缩。 结果，可以补偿由于轴承梳中的离心，剪切和其他力而导致的操作和变形期间发生的温度变形。

公开(公告)号：US20200277879A1

公开(公告)日：2020-09-03

申请号：US16756384

申请日：2018-10-17

Applicant: ABB Turbo Systems AG

Inventor： Stephan SENN ,  Christoph MATHEY

IPC: F01D25/30 ,  F02B37/18

Abstract: The invention relates to an exhaust gas turbine, comprising a turbine rotor (12) having a plurality of turbine rotor blades (2) with a turbine rotor blade height H. The exhaust gas turbine further comprises a diffuser arrangement (20) having a transverse diffuser (1) and an exhaust gas collection chamber (9). The transverse diffuser (1) is arranged downstream of the turbine rotor blades (2). The transverse diffuser (1) has a curved diffuser channel (13) which opens into the exhaust gas collection chamber (9) at a diffuser channel outlet (17). A M/H ratio between an axial extension M of the exhaust gas collection chamber (9) and the turbine rotor blade height H has a value of 1.0≤M/H≤4.6 and a P/H ratio between a radial extension P of the diffuser arrangement (20) and the turbine rotor blade height H has a value of 2.7≤P/H≤4.9. A D/H ratio between a radial expansion D of the diffuser channel section (13) and the turbine rotor blade height H has a value of 2.5≤D/H≤3.0 and a R/H ratio between a turbine hub radius R and the turbine rotor blade height H has a value of 1.1≤R/H≤1.5.

公开(公告)号：US09540954B2

公开(公告)日：2017-01-10

申请号：US13873717

申请日：2013-04-30

Applicant: ABB Turbo Systems AG

Inventor： Joel Schlienger ,  Markus Lebong ,  Olaf Baudisch ,  Patrick Aberle

IPC: F02C6/12 ,  F01D25/24 ,  F01D21/04

CPC classification number: F01D25/24 ,  F01D21/045 ,  F02C6/12 ,  F05D2220/40

Abstract: An exemplary arrangement for securing the shaft of an exhaust-gas turbocharger includes a catch ring with a central opening and a radial projection on the shaft. The catch ring having an inner contour in the region of the central opening. The radial projection on the shaft is provided with an outer contour. The inner contour on the catch ring and the outer contour on the shaft are configured such that, during mounting of the shaft and of the turbine wheel connected thereto and in at least one specified angle position of the shaft with respect to the housing, the radially outwardly protruding projection on the shaft can be passed in an axial direction through the central opening of the housing element. The radially outwardly protruding projection abuts in the axial direction against the housing element in specified angle positions of the shaft with respect to the housing.

Abstract translation: 用于固定排气涡轮增压器的轴的示例性布置包括具有中心开口和轴上的径向突起的卡环。 卡环在中心开口的区域具有内轮廓。 轴上的径向突起设置有外轮廓。 捕获环上的内轮廓和轴上的外轮廓被构造成使得在安装轴和连接到其上的涡轮机叶轮和在轴的至少一个指定的角度位置相对于壳体的径向 轴上的向外突出的突出部可以沿轴向通过壳体元件的中心开口。 径向向外突出的突起在轴的相对于壳体的指定角度位置处抵靠壳体元件沿轴向抵接。

公开(公告)号：US09228549B2

公开(公告)日：2016-01-05

申请号：US14199583

申请日：2014-03-06

Applicant: ABB TURBO SYSTEMS AG

Inventor： Heinz-Jürgen Feld ,  Llija Mrvelj ,  Philipp Meyer

IPC: F02M35/12 ,  F04D29/66 ,  F04D25/02 ,  F04D29/42 ,  F04D29/70 ,  F02C7/045

CPC classification number: F02M35/1272 ,  F02C7/045 ,  F04D25/024 ,  F04D29/4213 ,  F04D29/664 ,  F04D29/701 ,  F05D2220/40

Abstract: A sound attenuator on the intake side of a compressor of an exhaust-gas turbocharger includes a tubular sound attenuator housing, which encases a flow duct between a face-side inlet opening and a rear-side outlet opening. A holding plate is provided in the sound attenuator housing in the flow direction and is perforated in the flow direction. For example, the holding plate can have a multiplicity of holes extending in the flow direction. The sound attenuator on the intake side of the compressor of an exhaust-gas turbocharger has a compact, lightweight and inexpensive structural form. The intake air is subjected to low resistance as it flows through the attenuation elements.

Abstract translation: 在排气涡轮增压器的压缩机的进气侧的声音衰减器包括管状声音衰减器壳体，其在面侧入口和后侧出口之间包围流路。 声音衰减器壳体沿流动方向设置保持板，并沿流动方向穿孔。 例如，保持板可以具有沿流动方向延伸的多个孔。 废气涡轮增压器的压缩机进气侧的声音衰减器具有紧凑，重量轻且价廉的结构形式。 进气在流经衰减元件时经受低阻力。