公开(公告)号：US12065940B2

公开(公告)日：2024-08-20

申请号：US17298342

申请日：2019-11-22

申请人： BMTS Technology GmbH & Co. KG ,  Martin Berger

发明人： Martin Berger ,  Rüdiger Kleinschmidt ,  Frieder Stetter ,  Oliver Kuhne ,  Steffen Schmitt

IPC分类号： F01D25/16 ,  F02C6/12 ,  F02C7/06 ,  F16C17/10

CPC分类号： F01D25/166 ,  F02C6/12 ,  F02C7/06 ,  F16C17/105 ,  F16C17/107 ,  F05D2220/40 ,  F05D2240/53 ,  F16C2360/24

摘要： The invention relates to an exhaust gas turbocharger having a hydrodynamic plain bearing or a hydrodynamic plain bearing, comprising a rotor (10) and a counter-bearing part (50) assigned to the rotor (10), wherein a rotor bearing surface of the rotor (10) and a counterface of the counter-bearing part (50) face each other to form the hydrodynamic plain bearing in the form of a combined journal—thrust bearing, having a continuous hydrodynamically load bearing gap formed between the rotor bearing surface and the counterface, wherein the rotor bearing surface and/or the counterface, when cut longitudinally and through the axis of rotation (R) in sectional view, form(s) a bearing contour forming merging contour sections (17.1 to 17.3; 44.1 to 44.3; 53.1 to 53.3) to generate hydrodynamic load capacities in both the radial and the axial direction, wherein a contour section (17.3; 44.3; 53.3) in sectional view in a first bearing area forms a linear section that is part of a, in particular cylindrical or partially cylindrical, bearing section rotating at least sectionally about the axis of rotation (R), wherein a further contour section (17.1; 44.1; 53.1), in sectional view in a second bearing area, forms a further linear section, which is part of a further bearing area rotating at least sectionally about the axis of rotation (R), wherein this further linear section forms an angle with the axis of rotation (R), and wherein the first and the second bearing area merge via a transition section. According to the invention, a friction-optimized bearing system is to be created, which is easy to manufacture and ensures a reliable and effective bearing arrangement even under highly dynamic loads. According to the invention, this is achieved by the further linear section forming an angle in the range from >30° to

公开(公告)号：US20240263580A1

公开(公告)日：2024-08-08

申请号：US18608231

申请日：2024-03-18

申请人： RTX Corporation

发明人： Steven W. Burd

IPC分类号： F02C6/12 ,  F02B37/00 ,  F02C7/36 ,  F02K5/02

CPC分类号： F02C6/12 ,  F02B37/00 ,  F02C7/36 ,  F02K5/02 ,  F05D2220/40 ,  F05D2220/74

摘要： A system is provided that includes a compressor section, a turbine section, a first engine and a second engine. The compressor section includes a compressor rotor. The turbine section includes a turbine rotor configured to drive rotation of the compressor rotor. The first engine includes a first engine inlet, a first engine outlet and a first engine combustion zone fluidly coupled with and between the first engine inlet and the first engine outlet. The first engine inlet is fluidly coupled with and downstream of the compressor section. The first engine outlet is fluidly coupled with and upstream of the turbine section. The second engine includes a second engine inlet, a second engine outlet and a second engine combustion zone fluidly coupled with and between the second engine inlet and the second engine outlet. The second engine inlet is fluidly coupled with and downstream of the compressor section.

公开(公告)号：US20240247352A1

公开(公告)日：2024-07-25

申请号：US18182025

申请日：2023-03-10

申请人： Garrett Transportation I Inc.

发明人： Pavan Chintalapati ,  Ragupathy Kannusamy ,  Prashanth Chimangala Seetharamrao ,  Arthur Rene Fischer

IPC分类号： C22C38/48 ,  C21D9/00 ,  C22C38/00 ,  C22C38/02 ,  C22C38/04 ,  F02C6/12

CPC分类号： C22C38/48 ,  C21D9/0068 ,  C22C38/001 ,  C22C38/02 ,  C22C38/04 ,  F02C6/12 ,  C21D2211/001 ,  F05D2220/40

摘要： Disclosed is an austenitic stainless steel alloy that includes or consists of, by weight, about 23.0% to about 25.0% chromium, about 8.5% to about 10.0% nickel, about 0.5% to about 2.0% manganese, about 0.8% to about 1.0% niobium, about 0.5% to about 1.5% silicon, about 0.35% to about 0.45% carbon, about 0.2% to about 0.28% nitrogen, a balance of iron, and other inevitable/unavoidable impurities that are present in trace amounts. The elements zirconium and sulfur are excluded from the alloy beyond impurity levels. Turbocharger turbine housings made of the stainless steel alloy, and methods of making the same, are also disclosed. The stainless steel alloy is suitable for use in turbocharger turbine applications for temperatures up to about 1,020° C.

公开(公告)号：US12044136B2

公开(公告)日：2024-07-23

申请号：US17663507

申请日：2022-05-16

申请人： Transportation IP Holdings, LLC

发明人： Louis Kobielski ,  Baris Uygun ,  Adam C. Felton

IPC分类号： F02C6/12 ,  F01D25/14 ,  F04D17/10

CPC分类号： F01D25/145 ,  F04D17/10 ,  F05D2220/40 ,  F05D2240/15

摘要： A rotary assembly is provided that may be operably connected to an engine. The rotary assembly may include a rotary device comprising a turbine wheel, a shaft connected to the turbine wheel, and a case that houses the shaft and the turbine wheel. The turbine wheel may receive exhaust gas from the engine which causes rotation of the turbine wheel and the shaft. The case may include an interior surface that defines a hollow volume in which the turbine wheel and the shaft are located. The case has a radial thickness extending from the interior surface to an exterior surface of the case. The case may include a lattice structure integrated within the radial thickness of the case. The lattice structure may include a repeating three-dimensional array of frame segments connected to one another at junctions and defining interstitial spaces between the frame segments.

公开(公告)号：US12025016B2

公开(公告)日：2024-07-02

申请号：US18195446

申请日：2023-05-10

申请人： BorgWarner Inc.

发明人： Wolfram Schaefer

IPC分类号： F01D25/14 ,  F01D25/12 ,  F02C6/12 ,  F04D29/58

CPC分类号： F01D25/14 ,  F01D25/125 ,  F02C6/12 ,  F04D29/584 ,  F05D2220/40 ,  F05D2240/55

摘要： A housing includes a seal, a first portion for receiving a first axial portion of a rotor, and a second portion for receiving a second axial portion of the rotor. The first portion includes a first cooling system having a cooling channel through which cooling medium flows and a first cooling channel intake, and a first abutment face which surrounds the first cooling channel intake. The second portion includes a second cooling system having a cooling channel through which cooling medium flows and a second cooling channel intake, and a second abutment face which surrounds the second cooling channel intake. The housing portions are connected so that the abutment faces rest on each other and the cooling channel intakes form a transition surrounded by the abutment faces. The seal is arranged between the abutment faces and extends around the transition and is spaced apart from the cooling channel intakes.

公开(公告)号：US12012861B2

公开(公告)日：2024-06-18

申请号：US15760077

申请日：2016-09-08

申请人： BorgWarner Inc.

发明人： Sascha Karstadt ,  Sascha Weiske ,  Cathrin Bergner ,  Marc Gugau ,  Ahmet Coksen ,  Uwe Tomm ,  Frank Kruse

IPC分类号： F01D17/16 ,  F01D9/02 ,  F01D9/04 ,  F02C6/12

CPC分类号： F01D17/165 ,  F01D9/026 ,  F01D9/041 ,  F02C6/12 ,  F05D2220/40 ,  F05D2240/121 ,  F05D2240/122 ,  F05D2240/128 ,  F05D2240/14

摘要： A cartridge for use in a pulse energy enhanced turbine of a turbocharger. At least first and second fixed separating blades (12) are provided between a nozzle ring (6) and a disk (29), the separating blades (12) maintaining separation of exhaust gas flows through a guide grid between a divided volute and a turbine wheel (11). Exhaust pulsation energy from different cylinders or cylinder groups of an engine or engine bank are kept separated up to the turbine wheel, so that the turbine wheel reacts to individual pulses of exhaust gas flow from engine exhaust ports.

公开(公告)号：US20240183308A1

公开(公告)日：2024-06-06

申请号：US18441122

申请日：2024-02-14

申请人： BorgWarner Inc.

发明人： Vincent Hernandez-Gonzalez

IPC分类号： F02C6/12 ,  F02C7/04 ,  H01M8/04089

CPC分类号： F02C6/12 ,  F02C7/04 ,  H01M8/04097 ,  F05D2220/40 ,  H01M2250/20

摘要： A recirculation fan turbocharger assembly (23) recycles hydrogen and supplies air in a fuel cell system. The assembly (23) includes a fan (25), a compressor (27), and an electric drive (31) and/or a turbine (29). The fan (25) has an impeller (255) which is designed to convey a hydrogen containing recycle stream (250) to a fuel cell unit (1). The compressor (27) has a compressor wheel (275) which is designed to compress an air stream (270) for a fuel cell unit. The compressor wheel (275) and the impeller (255) are coupled to one another in a rotationally fixed manner. The electric drive (31) and/or a turbine (29) is/are designed to drive the impeller (255) and the compressor wheel (275) simultaneously.

公开(公告)号：US12000337B2

公开(公告)日：2024-06-04

申请号：US17614274

申请日：2019-05-24

申请人： Cummins Ltd.

发明人： Thomas Daniel Morton

IPC分类号： F02C6/12 ,  F01D17/10 ,  F02B37/18 ,  F02C7/06

CPC分类号： F02C6/12 ,  F02B37/186 ,  F02C7/06 ,  F01D17/105 ,  F05D2220/40 ,  F05D2240/54 ,  F05D2260/57

摘要： There is disclosed a bush comprising an internal surface and an external surface. The internal surface defines a bore and is configured to support movement of a body received in the bore. The external surface defines an outer radius. The external surface comprises one or more recesses.

公开(公告)号：US11982227B2

公开(公告)日：2024-05-14

申请号：US18160840

申请日：2023-01-27

申请人： Transportation IP Holdings, LLC

发明人： Christopher Homison

IPC分类号： F02C6/12 ,  F01D15/10 ,  F01D19/00 ,  F01D21/00 ,  F02B37/12 ,  F02B39/10 ,  F02C1/10 ,  H02K7/00 ,  H02K7/18 ,  H02P3/06

CPC分类号： F02C6/12 ,  F01D15/10 ,  F02B37/12 ,  F02B39/10 ,  F02C1/10 ,  H02K7/003 ,  H02K7/1823 ,  H02P3/06 ,  F01D19/00 ,  F01D21/00 ,  F05D2210/12 ,  F05D2220/40 ,  F05D2220/76 ,  Y02T10/12

摘要： Methods and systems are provided for a Brayton cycle system. In one example, a system for an air Brayton cycle includes a chamber that can receive a first energy source and a second energy source, a turbocharger, and a motor/generator coupled to a shaft of the turbocharger between a compressor and a turbine.

公开(公告)号：US11982199B2

公开(公告)日：2024-05-14

申请号：US17796497

申请日：2020-02-20

申请人： MITSUBISHI HEAVY INDUSTRIES ENGINE & TURBOCHARGER, LTD.

发明人： Yoshitomo Noda ,  Takuya Arakawa ,  Yosuke Dammoto ,  Shuichi Isayama ,  Hiroaki Takeuchi

IPC分类号： F01D25/16 ,  F01D25/18 ,  F02C6/12

CPC分类号： F01D25/164 ,  F01D25/18 ,  F02C6/12 ,  F05D2220/40 ,  F05D2240/54 ,  F05D2260/96 ,  F05D2260/98

摘要： A turbocharger is provided with: a rotational shaft; a rolling bearing rotatably supporting the rotational shaft; an oil film damper disposed radially outward of an outer ring of the rolling bearing; and a housing having a first axial retaining portion and a second axial retaining portion, disposed adjacent to both ends of the oil film damper in the axial direction, respectively, for restricting movement of the outer ring in the axial direction. An axial end surface of the outer ring, or a facing surface of the first axial retaining portion or the second axial retaining portion facing the axial end surface of the outer ring has: a coefficient of static friction smaller than that of a portion of the housing excluding the first axial retaining portion and the second axial retaining portion; or has a recess where oil of the oil film damper can enter.