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1. 发明授权

US09249719B2 Turbine device 有权
标题翻译：涡轮装置
公开(公告)号：US09249719B2
公开(公告)日：2016-02-02
申请号：US13757840
申请日：2013-02-03
申请人： Kangyue Technology Co., Ltd.
发明人： Hang Wang , Chao Ma , Zhifu Zhu , Yongtai Li , Congcong Wang , Lihua Song , Xilu Guo
IPC分类号： F02B37/02 , F02B37/18 , F01N13/10 , F02B67/10 , F01D25/30
CPC分类号： F02B37/025 , F01D25/30 , F01N13/10 , F02B37/18 , F02B67/10 , F05D2220/40 , Y02T10/144
摘要： A turbine device, including: a turbine housing including an inlet, a flow channel, an outlet, a middle partition, an arced partition; a turbine impeller; a gas outlet; and an exhaust manifold. The turbine impeller and the gas outlet are arranged inside the turbine housing. The exhaust manifold is connected to the inlet. The flow channel is arranged inside the turbine housing. The outlet is arranged on the flow channel close to the turbine impeller. The middle partition is disposed inside the flow channel and divides the flow channel into a left flow channel and a right flow channel. The arced partition is arranged in both the left and right flow channels. One end of the arced partition is in a rigid connection with the middle partition, and the other end of the arced partition is close to the outlet of the turbine housing.
摘要翻译：一种涡轮机装置，包括：涡轮机壳体，其包括入口，流动通道，出口，中间隔板，弧形隔板; 涡轮叶轮; 气体出口和排气歧管。涡轮机叶轮和气体出口布置在涡轮机壳体的内部。排气歧管连接到入口。流道布置在涡轮机壳体的内部。出口布置在靠近涡轮机叶轮的流动通道上。中间分隔件设置在流动通道的内部，并将流动通道分成左流动通道和右流道。弧形分区布置在左右流道中。弧形隔板的一端与中间隔板刚性连接，弧形隔板的另一端靠近涡轮机壳体的出口。

2. 发明授权

US09494111B2 Quad layer passage variable geometry turbine for turbochargers in exhaust gas recirculation engines 有权
标题翻译：用于废气再循环发动机涡轮增压器的四层通道可变几何涡轮机
公开(公告)号：US09494111B2
公开(公告)日：2016-11-15
申请号：US14322039
申请日：2014-07-02
申请人： Kangyue Technology Co., Ltd
发明人： Wang Hang , Steven Don Arnold , Yuan Daojun , Li Yanzhao , Sang Wuhai
IPC分类号： F02B33/44 , F02M25/07 , F02B37/22 , F02D41/00 , F02B37/02 , F01D17/10 , F01D9/02 , F02B29/04
CPC分类号： F02M26/10 , F01D9/026 , F01D17/105 , F02B29/0437 , F02B37/025 , F02B37/22 , F02D41/0007 , F02D41/0065 , F02M26/05 , F02M26/43 , F05D2220/40 , Y02T10/144 , Y02T10/47
摘要： A variable geometry turbine for turbochargers in exhaust gas recirculation engines incorporates a turbine housing having an exhaust inlet with a first side receiving exhaust from cylinders having exhaust gas recirculation (EGR) and a second side receiving exhaust from non-EGR cylinders. The first side has a first EGR-driving passage and a second EGR-driving passage and the second side having a first non-EGR-driving passage and a second non-EGR-driving passage. A first control valve is associated with the second EGR-driving passage and a second control valve is associated with the second non-EGR-driving passage. A controller is adapted to control the first and second control valves.
摘要翻译：用于排气再循环发动机中的涡轮增压器的可变几何涡轮机包括具有排气入口的涡轮机壳体，其具有从具有废气再循环（EGR）的气缸接收排气的第一侧和从非EGR气缸接收排气的第二侧。第一侧具有第一EGR驱动通道和第二EGR驱动通道，第二侧具有第一非EGR驱动通道和第二非EGR驱动通道。第一控制阀与第二EGR驱动通道相关联，第二控制阀与第二非EGR驱动通道相关联。控制器适于控制第一和第二控制阀。

3. 发明申请

US20130136587A1 CENTRIFUGAL COMPRESSOR 有权
标题翻译：离心式压缩机
公开(公告)号：US20130136587A1
公开(公告)日：2013-05-30
申请号：US13749654
申请日：2013-01-24
申请人： KANGYUE TECHNOLOGY CO., LTD.
发明人： Hang WANG , Chao MA , Zhifu ZHU , Yongtai LI , Lihua SONG , Xilu GUO , Congcong WANG
IPC分类号： F04D17/10
CPC分类号： F04D17/10 , F04D17/127 , F04D19/024 , F04D25/0606 , F04D27/007 , F04D27/0292 , F04D29/4213 , F04D29/444 , F05D2250/51 , F05D2250/52
摘要： A centrifugal compressor, including: a housing, the housing including: an inlet, a flow channel, an impeller outlet, and an air diffusing channel; a centrifugal impeller disposed inside the housing; a rotating wall, the rotating wall including a front cascade; and a rotating disc, the rotating disc including a rear cascade. The impeller outlet is disposed adjacent to a rear part of the centrifugal impeller and is connected to the flow channel via the air diffusing channel. The rotating wall is disposed between the centrifugal impeller and the housing. The front cascade is disposed inside the front part of the rotating wall and is connected to a dynamic driving device. The rotating disc is disposed inside the housing adjacent to the air diffusing channel and is in a rigid connection with the rotating wall.
摘要翻译：一种离心压缩机，包括：壳体，所述壳体包括：入口，流动通道，叶轮出口和空气扩散通道; 设置在所述壳体内的离心式叶轮; 旋转壁，旋转壁包括前级联; 和旋转盘，所述旋转盘包括后级联。叶轮出口邻近离心式叶轮的后部设置，并经由空气扩散通道连接到流动通道。旋转壁设置在离心式叶轮和壳体之间。前级联设置在旋转壁的前部内部并连接到动态驱动装置。旋转盘设置在壳体内部，与空气扩散通道相邻并且与旋转壁刚性连接。

4. 发明授权

US10662870B2 Variable geometry wastegate turbine 有权
公开(公告)号：US10662870B2
公开(公告)日：2020-05-26
申请号：US15553542
申请日：2015-08-04
申请人： KANGYUE TECHNOLOGY CO., LTD.
发明人： Hang Wang , Wuhai Sang , Daojun Yuan , Lihua Song , Xiaofen Xin , Wei Li
IPC分类号： F02B37/18 , F02B37/22 , F02B37/02 , F02M26/05 , F01D9/04 , F02B75/18 , F01D9/02 , F01D17/10
摘要： A variable geometry turbine having a wastegate includes a turbine housing, a power turbine, and a regulating valve. The turbine housing is provided with an inner intake gas flow channel and an outer intake gas flow channel. The turbine housing is further provided with a wastegate pipeline configured to bypass the power turbine, and a wastegate valve configured to control communication of the wastegate pipeline. One of the regulating valve and the wastegate valve has a regulating face having a varying axial height in a rotation direction of the regulating valve, and the other of the regulating valve and the wastegate valve has a linking portion which makes contact and cooperates with the regulating face. Thus, the efficiency of the turbine is improved significantly and backflow of the gas flow is reduced.

5. 发明授权

US10018107B2 Balanced vanes and integrated actuation system for a variable geometry turbocharger 有权
公开(公告)号：US10018107B2
公开(公告)日：2018-07-10
申请号：US14796798
申请日：2015-07-10
申请人： Kangyue Technology Co., Ltd
发明人： Steven Don Arnold , Wang Hang , Li Yanzhao , Xiaofen Xin
IPC分类号： F01D17/16 , F02B37/22 , F02B37/24
CPC分类号： F02B37/22 , F02B37/24 , Y02T10/144
摘要： A variable geometry turbine (VGT) for turbochargers incorporates a turbine nozzle having a plurality of vanes, each vane having an airfoil with an inner disc and an outer disc. A first nozzle plate incorporates pockets to receive the inner discs with the inner discs substantially flush with a nozzle surface on the first nozzle plate. A second nozzle plate has pockets to receive the outer discs with outer discs substantially flush with a second nozzle surface. An integral actuation system rotates the plurality of vanes for variation of the nozzle geometry.

6. 发明申请

US20180238226A1 VARIABLE GEOMETRY WASTEGATE TURBINE MEETING THE REQUIREMENTS OF EGR CIRCULATION 审中-公开
公开(公告)号：US20180238226A1
公开(公告)日：2018-08-23
申请号：US15553542
申请日：2015-08-04
申请人： KANGYUE TECHNOLOGY CO., LTD.
发明人： Hang WANG , Wuhai SANG , Daojun YUAN , Lihua SONG , Xiaofen XIN , Wei LI
IPC分类号： F02B37/18 , F02M26/05 , F01D9/02 , F01D17/10 , F02B75/18 , F01D9/04
CPC分类号： F02B37/186 , F01D9/026 , F01D9/041 , F01D9/045 , F01D17/105 , F02B37/025 , F02B37/183 , F02B37/22 , F02B75/18 , F02B2075/1824 , F02M26/05 , F05D2220/40 , F05D2240/128 , F05D2240/14 , Y02T10/144
摘要： A variable geometry turbine having a wastegate, which meets the requirements of EGR circulation, includes a turbine housing and a power turbine. The turbine housing is provided with an inner intake gas flow channel and an outer intake gas flow channel which is configured to guide exhaust gas of an engine to the power turbine for driving the power turbine to rotate. The turbine housing is further provided with a wastegate pipeline configured to discharge the exhaust gas without passing through the power turbine, and a wastegate valve configured to control communication and cutting off of the wastegate pipeline, and in the case that an intake gas amount of the exhaust gas entering into the turbine exceeds a preset value, the wastegate valve is opened to discharge a part of the exhaust gas via the wastegate pipeline.

7. 发明申请

US20170009645A1 BALANCED VANES AND INTEGRATED ACTUATION SYSTEM FOR A VARIABLE GEOMETRY TURBOCHARGER 有权
标题翻译：用于可变几何涡轮增压器的平衡叶片和集成驱动系统
公开(公告)号：US20170009645A1
公开(公告)日：2017-01-12
申请号：US14796798
申请日：2015-07-10
申请人： Kangyue Technology Co., Ltd
发明人： Steven Don Arnold , Wang Hang , Li Yanzhao , Xiaofen Xin
IPC分类号： F02B37/22 , F04D27/00 , F04D17/10
CPC分类号： F02B37/22 , F02B37/24 , Y02T10/144
摘要： A variable geometry turbine (VGT) for turbochargers incorporates a turbine nozzle having a plurality of vanes, each vane having an airfoil with an inner disc and an outer disc. A first nozzle plate incorporates pockets to receive the inner discs with the inner discs substantially flush with a nozzle surface on the first nozzle plate. A second nozzle plate has pockets to receive the outer discs with outer discs substantially flush with a second nozzle surface. An integral actuation system rotates the plurality of vanes for variation of the nozzle geometry.
摘要翻译：用于涡轮增压器的可变几何涡轮机（VGT）包括具有多个叶片的涡轮喷嘴，每个叶片具有带有内盘和外盘的翼型件。第一喷嘴板包括用于容纳内盘的凹部，内盘基本上与第一喷嘴板上的喷嘴表面齐平。第二喷嘴板具有用于接收外盘的凹部，外盘与第二喷嘴表面基本齐平。整体致动系统旋转多个叶片以改变喷嘴几何形状。

8. 发明授权

US09347450B2 Centrifugal compressor 有权
标题翻译：离心式压缩机
公开(公告)号：US09347450B2
公开(公告)日：2016-05-24
申请号：US13749654
申请日：2013-01-24
申请人： Kangyue Technology Co., Ltd.
发明人： Hang Wang , Chao Ma , Zhifu Zhu , Yongtai Li , Lihua Song , Xilu Guo , Congcong Wang
IPC分类号： F04D17/10 , F04D25/06 , F04D27/00 , F04D29/44 , F04D27/02 , F04D17/12 , F04D19/02 , F04D29/42
CPC分类号： F04D17/10 , F04D17/127 , F04D19/024 , F04D25/0606 , F04D27/007 , F04D27/0292 , F04D29/4213 , F04D29/444 , F05D2250/51 , F05D2250/52
摘要： A centrifugal compressor, including: a housing, the housing including: an inlet, a flow channel, an impeller outlet, and an air diffusing channel; a centrifugal impeller disposed inside the housing; a rotating wall, the rotating wall including a front cascade; and a rotating disc, the rotating disc including a rear cascade. The impeller outlet is disposed adjacent to a rear part of the centrifugal impeller and is connected to the flow channel via the air diffusing channel. The rotating wall is disposed between the centrifugal impeller and the housing. The front cascade is disposed inside the front part of the rotating wall and is connected to a dynamic driving device. The rotating disc is disposed inside the housing adjacent to the air diffusing channel and is in a rigid connection with the rotating wall.
摘要翻译：一种离心压缩机，包括：壳体，所述壳体包括：入口，流动通道，叶轮出口和空气扩散通道; 设置在所述壳体内的离心式叶轮; 旋转壁，旋转壁包括前级联; 和旋转盘，所述旋转盘包括后级联。叶轮出口邻近离心式叶轮的后部设置，并经由空气扩散通道连接到流动通道。旋转壁设置在离心式叶轮和壳体之间。前级联设置在旋转壁的前部内部并连接到动态驱动装置。旋转盘设置在壳体内部，与空气扩散通道相邻并且与旋转壁刚性连接。

9. 发明申请

US20160003196A1 QUAD LAYER PASSAGE VARIABLE GEOMETRY TURBINE FOR TURBOCHARGERS IN EXHAUST GAS RECIRCULATION ENGINES 有权
标题翻译：四面体通气可变式几何涡轮涡轮机在排气再循环发动机
公开(公告)号：US20160003196A1
公开(公告)日：2016-01-07
申请号：US14322039
申请日：2014-07-02
申请人： Kangyue Technology Co., Ltd
发明人： Wang Hang , Steven Don Arnold , Yuan Daojun , Li Yanzhao , Sang Wuhai
IPC分类号： F02M25/07 , F01D17/10 , F02B37/02 , F02B37/22 , F02D41/00
CPC分类号： F02M26/10 , F01D9/026 , F01D17/105 , F02B29/0437 , F02B37/025 , F02B37/22 , F02D41/0007 , F02D41/0065 , F02M26/05 , F02M26/43 , F05D2220/40 , Y02T10/144 , Y02T10/47
摘要： A variable geometry turbine for turbochargers in exhaust gas recirculation engines incorporates a turbine housing having an exhaust inlet with a first side receiving exhaust from cylinders having exhaust gas recirculation (EGR) and a second side receiving exhaust from non-EGR cylinders. The first side has a first EGR-driving passage and a second EGR-driving passage and the second side having a first non-EGR-driving passage and a second non-EGR-driving passage. A first control valve is associated with the second EGR-driving passage and a second control valve is associated with the second non-EGR-driving passage. A controller is adapted to control the first and second control valves.
摘要翻译：用于排气再循环发动机中的涡轮增压器的可变几何涡轮机包括具有排气入口的涡轮机壳体，其具有从具有废气再循环（EGR）的气缸接收排气的第一侧和从非EGR气缸接收排气的第二侧。第一侧具有第一EGR驱动通道和第二EGR驱动通道，第二侧具有第一非EGR驱动通道和第二非EGR驱动通道。第一控制阀与第二EGR驱动通道相关联，第二控制阀与第二非EGR驱动通道相关联。控制器适于控制第一和第二控制阀。

10. 发明申请

US20130142650A1 TURBINE DEVICE 有权
标题翻译：涡轮装置
公开(公告)号：US20130142650A1
公开(公告)日：2013-06-06
申请号：US13757840
申请日：2013-02-03
申请人： KANGYUE TECHNOLOGY CO., LTD.
发明人： Hang WANG , Chao MA , Zhifu ZHU , Yongtai LI , Congcong WANG , Lihua SONG , Xilu GUO
IPC分类号： F02K1/18
CPC分类号： F02B37/025 , F01D25/30 , F01N13/10 , F02B37/18 , F02B67/10 , F05D2220/40 , Y02T10/144
摘要： A turbine device, including: a turbine housing including an inlet, a flow channel, an outlet, a middle partition, an arced partition; a turbine impeller; a gas outlet; and an exhaust manifold. The turbine impeller and the gas outlet are arranged inside the turbine housing. The exhaust manifold is connected to the inlet. The flow channel is arranged inside the turbine housing. The outlet is arranged on the flow channel close to the turbine impeller. The middle partition is disposed inside the flow channel and divides the flow channel into a left flow channel and a right flow channel. The arced partition is arranged in both the left and right flow channels. One end of the arced partition is in a rigid connection with the middle partition, and the other end of the arced partition is close to the outlet of the turbine housing.
摘要翻译：一种涡轮机装置，包括：涡轮机壳体，其包括入口，流动通道，出口，中间隔板，弧形隔板; 涡轮叶轮; 气体出口和排气歧管。涡轮机叶轮和气体出口布置在涡轮机壳体的内部。排气歧管连接到入口。流道布置在涡轮机壳体的内部。出口布置在靠近涡轮机叶轮的流动通道上。中间分隔件设置在流动通道的内部，并将流动通道分成左流动通道和右流道。弧形分区布置在左右流道中。弧形隔板的一端与中间隔板刚性连接，弧形隔板的另一端靠近涡轮机壳体的出口。

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