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1. 发明授权

EP3117078B1 METHOD AND SYSTEM FOR VARYING THE WIDTH OF A TURBINE NOZZLE 有权
公开(公告)号：EP3117078B1
公开(公告)日：2018-09-26
申请号：EP15708419.5
申请日：2015-02-25
申请人： Fluid Equipment Development Company, LLC
发明人： HUNT, Jason B.
IPC分类号： F01D17/14 , B01D61/02 , B01D61/06 , F01D17/02
CPC分类号： F01D17/00 , B01D61/025 , B01D61/06 , B01D2313/243 , B01D2313/246 , F01D1/02 , F01D17/02 , F01D17/14 , F01D17/141 , F01D17/143 , F01D17/146 , F05D2220/40
摘要： A turbine and method of operating the same a turbine includes a housing having a volute, an inlet and an outlet an impeller rotatable coupled to the housing, a first shroud disposed within the housing comprising a plurality of nozzle vanes and a second shroud disposed within the housing adjacent to the first shroud so that a nozzle area is formed between the first shroud and the second shroud, said nozzle area having a variable width. The second shroud is movable relative to the first shroud to vary the width so that fluid flow from the inlet to the outlet is variable.

2. 发明授权

EP2474724B1 CONTROL DEVICE OF TURBOCHARGER 失效转让
公开(公告)号：EP2474724B1
公开(公告)日：2018-07-18
申请号：EP10846812.5
申请日：2010-11-12
申请人： TOYOTA JIDOSHA KABUSHIKI KAISHA
发明人： AZUMA, Yasuhiro
IPC分类号： F02B37/24 , F01D17/16
CPC分类号： F02D41/0007 , B60K6/445 , B60W20/00 , F01D15/10 , F01D17/143 , F01D17/165 , F02B37/24 , F02C6/12 , F02D41/042 , F02D41/062 , F02N11/0814 , F05D2220/40 , Y02T10/144 , Y02T10/6239
摘要： In a turbocharger including a variable nozzle vane mechanism including a plurality of nozzle vanes provided on an outer circumferential side of a turbine wheel, the variable nozzle vane mechanism adjusting a flow of an exhaust gas with the nozzle vanes; and an actuator driving the nozzle vane mechanism, a control is continued that causes a movable member of the variable nozzle vane mechanism to abut against a mechanical stopper limiting the range of the movement of the nozzle vanes as long as the engine is stopped while the vehicle is running. Thus, wear of, for example, a link and a rod constituting the variable nozzle vane mechanism can be prevented during an engine stop while the vehicle is running.

3. 发明公开

EP3258068A1 VARIABLE GEOMETRY ASSEMBLY FOR A TURBOMACHINE AND TURBOMACHINE COMPRISING SAID ASSEMBLY 有权转让
标题翻译：用于包含所述装配的涡轮机和涡轮机的可变几何组件
公开(公告)号：EP3258068A1
公开(公告)日：2017-12-20
申请号：EP17175524.2
申请日：2017-06-12
申请人： Nuovo Pignone Tecnologie SrL
发明人： FLORINDO, Federico
IPC分类号： F01D17/14 , F01D17/16
CPC分类号： F01D17/165 , F01D17/143 , F02C6/12 , F04D29/462 , F05D2220/40 , F05D2240/128
摘要： A variable geometry assembly for modulating a fluid flow in a turbomachine is disclosed. The assembly comprises: a first ring (33; 133) having a plurality of first wedge-shaped elements (37; 137) and having an axis (A-A); a second ring (35; 135) having a plurality of second wedge-shaped elements (39; 139) and having an axis (A-A). The second ring is substantially coaxial to the first ring. The second wedge-shaped elements (39; 139) co-act with the first wedge-shaped elements (37; 137). Flow passages (41) are defined between pairs of sequentially arranged first wedge-shaped elements (37; 137) and second wedge-shaped elements (39; 139). The first ring (33; 133) and the second ring (35; 135) are angularly displaceable one with respect to the other. Moreover, the first ring (33; 133) and the second ring (35; 135) are configured to move axially with respect to one another when the first ring and the second ring are angularly displaced one with respect to the other.
摘要翻译：公开了一种用于调制涡轮机中的流体流动的可变几何形状组件。该组件包括：第一环（33; 133），其具有多个第一楔形元件（37; 137）并具有轴线（A-A）; 具有多个第二楔形元件（39; 139）并且具有轴线（A-A）的第二环（35; 135）。第二环基本上与第一环同轴。第二楔形元件（39; 139）与第一楔形元件（37; 137）共同作用。流动通道（41）限定在成对的顺序布置的第一楔形元件（37; 137）和第二楔形元件（39; 139）之间。第一环（33; 133）和第二环（35; 135）可相对于另一个角位移一次。此外，第一环（33; 133）和第二环（35; 135）构造成当第一环和第二环相对于另一个成角度地移位一个时相对于彼此轴向移动。

4. 发明公开

EP3204617A1 VARIABLE GEOMETRY TURBINE 有权
标题翻译：可变几何涡轮机
公开(公告)号：EP3204617A1
公开(公告)日：2017-08-16
申请号：EP15782061.4
申请日：2015-10-09
申请人： Cummins Ltd
发明人： HILL, Lisa Jane , BYWATER, John , PARKER, John F.
IPC分类号： F01D17/14
CPC分类号： F02B37/183 , F01D17/143 , F05D2220/40 , Y02T10/144
摘要： A variable geometry turbine having a turbine wheel, an inlet passageway, a movable wall member being moveable axially to vary the width of the inlet passageway, an annular seal being mounted to the movable wall member or an adjacent housing member to provide a seal between adjacent surfaces of the movable wall member and housing member respectively, wherein a bypass passage is provided in the other of said movable wall member or housing member, extending from an inlet bypass port to an outlet bypass port, said ports being spaced from each other and provided in said adjacent surface of said other of the movable wall member or housing member, arranged such that as the movable wall member moves axially, the annular seal moves axially relative to the ports to vary the flow that may pass from a region of the cavity inboard of the seal, through the bypass passage.
摘要翻译：一种可变几何涡轮机，其具有涡轮机叶轮（5），入口通道（9），可移动壁构件（11），其可轴向移动以改变入口通道的宽度，环形密封件（127）（11）和壳体构件（103）的相邻表面之间提供密封，其中旁路通道（150）设置在可动壁构件（11）和壳体构件所述可动壁构件（11）和壳体构件（103），所述旁路通道（150）从入口旁路端口（151）延伸到出口旁路端口（152），所述入口和出口旁路端口（151,152）（11）和壳体构件（103）的所述另一个的所述相邻表面上设置，使得当可动壁构件（11）轴向运动时，环形密封件（127）移动相对于入口和出口旁路端口（151,152）沿轴向轴向移动，以改变流动的程度其可以从密封件的腔内侧（113）的区域通过旁路通道（150）。

5. 发明公开

EP2540990A3 Seal assembly for a rotational fluid metering valve 有权转让
标题翻译： Dichtungsanordnung einer drehbaren Ventilvorrichtung zum Abmessen desKühlungsmediums
公开(公告)号：EP2540990A3
公开(公告)日：2017-04-12
申请号：EP12172885.1
申请日：2012-06-21
申请人： United Technologies Corporation
发明人： Smith, Darren M. , Brooks, Judith F.
IPC分类号： F01D17/14 , F01D25/14 , F02C7/18 , F02C9/18
CPC分类号： F01D17/143 , F01D25/14 , F02C7/18 , F02C9/18 , F05D2250/411 , F05D2260/50 , Y02T50/675
摘要： A seal assembly for a fan duct metering valve (30) disposed within a casing (70) of a gas turbine engine includes a tab (38) for extending through an opening (90) in the casing (70) and attaching to the valve (30), and a carrier (65) for extending into the opening (90) and engaging the valve (30) such that fluid does not leak between the valve (30) and the carrier (65).
摘要翻译：设置在燃气涡轮发动机的壳体（70）内的用于风扇管道计量阀（30）的密封组件包括用于延伸通过壳体（70）中的开口（90）并附接到阀（ 30）和用于延伸到开口（90）中并与阀（30）接合的载体（65），使得流体不会在阀（30）和载体（65）之间泄漏。

6. 发明授权

EP2423485B1 SUPERCHARGER SYSTEM FOR INTERNAL COMBUSTION ENGINES 有权
标题翻译：充电内燃机
公开(公告)号：EP2423485B1
公开(公告)日：2016-12-14
申请号：EP09843666.0
申请日：2009-04-24
申请人： TOYOTA JIDOSHA KABUSHIKI KAISHA
发明人： TANADA, Masayuki
IPC分类号： F02B37/013 , F02B37/18 , F02B39/00 , F02C6/12
CPC分类号： F02B37/013 , F01D9/026 , F01D17/143 , F02B37/004 , F02B37/025 , F02B37/18 , F02C6/12 , F05D2220/40 , F05D2240/40 , Y02T10/144

7. 发明公开

EP3017169A4 GAS TURBINE ENGINE SYSTEM FOR MODULATING FLOW OF FAN BY-PASS AIR AND CORE ENGINE AIR 有权转让
标题翻译：燃气轮机驱动系统，用于通过连续的空气和核心发动机空气调节风扇流量
公开(公告)号：EP3017169A4
公开(公告)日：2016-07-27
申请号：EP14820627
申请日：2014-06-26
申请人： UNITED TECHNOLOGIES CORP
发明人： LOVETT JEFFREY A
IPC分类号： F02K1/08 , F01D17/14 , F02C9/18 , F02K1/15 , F02K1/38 , F02K1/46 , F02K3/075 , F02K3/10
CPC分类号： F02K1/08 , F01D17/143 , F01D17/148 , F02K1/15 , F02K1/386 , F02K1/46 , F02K3/075 , F02K3/10 , F05D2250/182 , F05D2250/41 , F05D2270/62
摘要： The system (10) provides a modulator ring (54) secured adjacent an exhaust end (56) of an inner wall of a by-pass fan air duct (40) and secured adjacent a convergent nozzle section (38) of the engine wherein flow of by-pass fan air (42) and core engine air (18) converge within an exhaust nozzle (34), The modulator ring (54) may be actuated to extend beyond the exhaust end (56) of the duct (40) to decrease air passage (62) forcing more air into the core engine (14) for greater thrust from the core engine (14) with minimal loss of thrust from the by-pass fan air (42). The modulator ring (54) stay alternatively rotate to uncover trailing-edge slots in the exhaust end (56) of the duct to also modulate flow rates of by-pass fan air (42) into the convergent nozzle section (38).
摘要翻译：系统（10）提供了一个调制环（54），该调节环围绕旁通风扇空气管道（40）的内壁的排气端（56）固定并且紧固在发动机的会聚喷嘴部分（38）附近，其中流动旁路风扇空气（42）和核心发动机空气（18）会聚在排气喷嘴（34）内。调节器环（54）可以被致动以延伸超过管道（40）的排气端（56）到减少空气通道（62），从而使来自核心发动机（14）的更大的推力迫使更多的空气进入到核心发动机（14）中，同时来自旁路风扇空气（42）的推力损失最小。调节器环（54）保持交替地旋转以露出管道的排气端（56）中的后缘槽口，以调节旁路风扇空气（42）进入会聚喷嘴部分（38）的流量，

8. 发明公开

EP2778375A3 Axial-flow turbine and power plant including the same 审中-公开
标题翻译：轴流式水轮机和电站订单
公开(公告)号：EP2778375A3
公开(公告)日：2016-06-29
申请号：EP14155838.7
申请日：2014-02-19
申请人： Kabushiki Kaisha Toshiba
发明人： Onoda, Akihiro , Mimura, Yuki , Ito, Shoko
IPC分类号： F02C9/20 , F01D9/04 , F01D25/12 , F02C7/12
CPC分类号： F01D25/12 , F01D11/001 , F01D11/02 , F01D11/025 , F01D17/141 , F01D17/143 , F01D17/145 , F02C3/13 , F02C7/12 , F02C7/18 , F02C9/18 , F02C9/20 , F02C9/22 , F05D2260/20 , F05D2260/61 , Y02E20/18 , Y02E20/185
摘要： An axial-flow turbine (10) according to an embodiment includes a plurality of nozzle structures (20) and a plurality of blade structures (40). At least one nozzle structure includes an outer ring diaphragm (21) and an inner ring diaphragm (22). The outer ring diaphragm and the inner ring diaphragm form an annular opening portion which extends in a circumferential direction therebetween. A nozzle (25) is provided in a portion of a region of the annular opening portion in the circumferential direction, and a closing part (30) is provided in another portion of the region of the annular opening portion in the circumferential direction. The closing part closes this other portion of the region to prevent a working fluid from flowing into this other portion of the region. A closing part medium passage (33) is provided in the closing part and is configured to flow a cooling medium which cools the closing part.

9. 发明公开

EP2960460A4 VARIABLE GEOMETRY TURBOCHARGER 审中-公开
标题翻译：具有可变几何形状的TURBOLADER
公开(公告)号：EP2960460A4
公开(公告)日：2016-03-09
申请号：EP13875521
申请日：2013-02-21
申请人： MITSUBISHI HEAVY IND LTD
发明人： IBARAKI SEIICHI , SUZUKI HIROSHI , YOKOYAMA TAKAO
IPC分类号： F02B37/22 , F01D5/18 , F01D17/14 , F01D17/16 , F02B39/00
CPC分类号： F02B37/22 , F01D5/18 , F01D17/143 , F01D17/16 , F02B37/168 , F02B37/24 , F02B39/005 , F04D27/002 , F05D2220/40 , Y02T10/144

10. 发明公开

EP2960460A1 VARIABLE GEOMETRY TURBOCHARGER 审中-公开
标题翻译： TURBOLADER MIT VARIABLER GEOMETRIE
公开(公告)号：EP2960460A1
公开(公告)日：2015-12-30
申请号：EP13875521.0
申请日：2013-02-21
申请人： Mitsubishi Heavy Industries, Ltd.
发明人： IBARAKI, Seiichi , SUZUKI, Hiroshi , YOKOYAMA, Takao
IPC分类号： F02B37/24 , F02B39/00
CPC分类号： F02B37/22 , F01D5/18 , F01D17/143 , F01D17/16 , F02B37/168 , F02B37/24 , F02B39/005 , F04D27/002 , F05D2220/40 , Y02T10/144
摘要： A variable geometry exhaust gas turbocharger comprises: a turbine rotor 26 including a rotating shaft 24 and a turbine wheel 12; a bearing housing 20 accommodating a bearing unit 22; a turbine housing 10 accommodating the turbine wheel rotatably and having formed an annular turbine scroll part 16 in which exhaust gas flows; and a variable geometry mechanism 40 provided in an annular nozzle part 18 to guide the exhaust gas flowing in the turbine scroll part into the turbine wheel; wherein the variable geometry mechanism 40 comprises: a nozzle vane 42 protruding, in a state of being unable to rotate, from at least one of a shroud side or a hub side of the nozzle part toward the nozzle part; an annular nozzle wall 44 configured to be movable forward and backward from the hub side toward the shroud side or from the shroud side toward the hub side of the nozzle part, and configured to permit a nozzle width B of the nozzle part to be variable over all circumference; and a driving part 46 for moving the nozzle wall forward and backward.
摘要翻译：可变几何形状废气涡轮增压器包括：涡轮转子26，其包括旋转轴24和涡轮机叶轮12; 容纳轴承单元22的轴承壳体20; 涡轮壳体10，其可旋转地容纳涡轮机叶轮，并且形成有排气流动的环形涡轮涡旋部分16; 以及可变几何机构40，其设置在环形喷嘴部分18中，以将在涡轮涡旋部分中流动的废气引导到涡轮机叶轮中; 其中所述可变几何机构40包括：喷嘴叶片42，其处于不能从所述喷嘴部分的护罩侧或轮毂侧中的至少一个朝向所述喷嘴部分旋转的状态; 环形喷嘴壁44，其能够从所述轮毂侧朝向所述护罩侧或从所述护罩侧向所述喷嘴部的所述轮毂侧前后移动，并且，能够使所述喷嘴部的喷嘴宽度B变化全周以及用于向前和向后移动喷嘴壁的驱动部分46。

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