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1. 发明公开

KR1020170115169A 차량의 엔진 흡기 구조 审中-实审
标题翻译：车辆的发动机进气结构
公开(公告)号：KR1020170115169A
公开(公告)日：2017-10-17
申请号：KR1020160041602
申请日：2016-04-05
申请人： 현대자동차주식회사 , 기아자동차주식회사
发明人： 추동호 , 이양걸
IPC分类号： F02B31/04 , F02D9/10 , F16K3/02 , F16K3/314
CPC分类号： F02F1/425 , F02B31/04 , F02D41/0002 , F02D2041/0015 , F02M35/10262 , Y02T10/146 , F02D9/10 , F16K3/02 , F16K3/314
摘要： 본발명은차량의엔진흡기구조에관한것으로, 흡기유로상에회동가능하도록장착되어흡기의유동단면적을조절하도록마련된가변플랩; 상기가변플랩의하류측에장착되고, 상기가변플랩과연동하여변위를형성하도록마련된포트플레이트; 상기가변플랩및 상기포트플레이트의변위형성을위한구동력을제공하도록마련된구동부; 및엔진의운전영역에따라상기가변플랩의회동각을결정하고, 상기구동부를구동시켜상기가변플랩의회동각을제어하도록마련된제어부;를포함하는차량의엔진흡기구조가소개된다.
摘要翻译：本发明涉及一种车辆的发动机进气结构，该发动机进气结构包括：可变挡板，该可变挡板可旋转地安装在进气流动路径上以调节进气的流动横截面积; 安装在所述可变襟翼的下游侧并构造成与所述可变襟翼接合以形成位移的端口板; 驱动单元，其被设置成为所述可变挡板提供驱动力和所述挡板的位移形成; 并且控制单元被配置成根据发动机的操作区域确定可变襟翼的旋转角度并且通过驱动驱动单元来控制可变襟翼的旋转角度。

2. 发明公开

KR1020160072929A 웨이스트 게이트 모듈 지지 장치 有权
标题翻译：用于支持废气门模块的装置
公开(公告)号：KR1020160072929A
公开(公告)日：2016-06-24
申请号：KR1020140180636
申请日：2014-12-15
申请人： 현대자동차주식회사 , 기아자동차주식회사
发明人： 추동호 , 정도근 , 배성관
IPC分类号： F02B37/22 , F02B39/00
CPC分类号： F02B39/16 , F02B37/16 , F02B37/183 , F02B2039/164 , Y02T10/144 , F02B37/22 , F02B37/225 , F02B39/00
摘要： 웨이스트게이트모듈과터보하우징을연결하는지지브라켓; 및상기지지브라켓중 웨이스트게이트모듈과대향하는면에형성되며단부가웨이스트게이트모듈과결합된결합돌기;를포함하는웨이스트게이트모듈지지장치가소개된다.
摘要翻译：公开了一种用于支撑废气门模块的装置。支撑废气门模块的装置包括：连接废气门模块和涡轮壳体的支撑支架; 以及联接突起，其端部联接到废气门模块，形成在与支撑支架中的废气门模块相对的表面上。本发明的目的是提供一种用于支撑废气门模块的装置，阻止或限制由废气产生的热的传递。

3. 发明公开

KR1020140026918A 인터쿨러의 쿨링핀 无效
标题翻译：冷却器冷却
公开(公告)号：KR1020140026918A
公开(公告)日：2014-03-06
申请号：KR1020120092797
申请日：2012-08-24
申请人： 현대자동차주식회사 , 기아자동차주식회사 , 갑을오토텍(주)
发明人： 추동호 , 이주현
IPC分类号： F28F1/10 , F02B29/04 , F28F1/32
CPC分类号： Y02T10/146 , F28F1/10 , F02B29/04 , F28F1/32
摘要： Presented is a cooling fin for an intercooler, including: a fin body which has a zigzag shape, and forms a distribution channel of air on each bent part; a cutting line which is vertically cut and formed on a central spot separated at respectively predetermined intervals from the top end and bottom end of an inclined plane for connecting the bent top end and bottom end of the fin body, and which is continuously formed along the length direction of the inclined plane at a predetermined interval; and external portion and internal portion alternately formed along the length direction of the inclined plane, by having inclined planes which are divided by the cutting line, and are crossing each other, bend and protrude externally or internally.
摘要翻译：提出了一种用于中间冷却器的冷却翅片，包括：翅片体，其具有锯齿形状，并且在每个弯曲部分上形成空气的分配通道; 切割线垂直切割并形成在与倾斜平面的顶端和底端分开预定间隔分开的中心点上，用于连接翅片本体的弯曲顶端和底端，并且沿着倾斜平面的长度方向以预定间隔; 并且沿着倾斜平面的长度方向交替地形成的外部部分和内部部分，通过由切割线分开的倾斜平面彼此交叉，从外部或内部弯曲并突出。

4. 发明授权

KR101326845B1 자동차의 가스켓 有权
标题翻译：汽车用垫
公开(公告)号：KR101326845B1
公开(公告)日：2013-11-11
申请号：KR1020110126334
申请日：2011-11-29
申请人： 현대자동차주식회사 , 기아자동차주식회사
发明人： 홍진원 , 추동호 , 김용훈
IPC分类号： F02F11/00 , F16J15/08
CPC分类号： F16J15/061 , F16J15/0825 , F16J15/0831 , F16J2015/085
摘要： 본 발명은 배기매니폴드에 구비되며, 씰링성능이 개선됨으로써 터보차저의 성능을 향상시킬 수 있는 자동차의 가스켓에 관한 것이다.
본 발명의 실시예에 따른 자동차의 가스켓은, 엔진의 실린더와 상기 실린더로부터 터보차저로 배기가스를 공급하도록 형성된 배기배니폴드의 결합부에 개재되는 자동차의 가스켓에 있어서, 상기 실린더와 상기 배기배니폴드를 결합하시키는 체결수단이 관통하도록 형성된 체결홀; 상기 체결홀 간의 폭이 상대적으로 큰 부분에 형성되는 더블하프비드부; 및 상기 체결홀 간의 폭이 상대적으로 작은 부분에 형성되는 하프비드부; 를 포함하되, 상기 더블하프비드부는, 수평하게 형성된 제1사이드랜드면; 상기 제1사이드랜드면의 일단에서 경사지게 연장되는 제1경사면; 상기 제1경사면의 일단에서 수평하게 연장되는 중앙랜드면; 상기 중앙랜드면의 일단에서 연장되며, 상기 중앙랜드면을 기준으로 상기 제1경사면과 대칭으로 형성되는 상기 제2경사면; 및 상기 제2경사면의 일단에서 연장되며, 상기 중앙랜드면을 기준으로 상기 제1사이드랜드면과 대칭으로 형성되는 제2사이드랜드면; 을 포함하는 복수개의 더블하프비드가 겹쳐짐으로써 형성되고, 상기 하프비드부는, 수평하게 형성된 제1랜드면; 상기 제1랜드면의 일단에서 경사지게 연장되는 경사면; 및 상기 경사면의 일단에서 수평하게 연장되는 제2랜드면; 을 포함하는 복수개의 하프비드가 겹쳐짐으로써 형성될 수 있다.

5. 发明公开

KR1020130060049A 자동차의 가스켓 有权
标题翻译：汽车用垫
公开(公告)号：KR1020130060049A
公开(公告)日：2013-06-07
申请号：KR1020110126334
申请日：2011-11-29
申请人： 현대자동차주식회사 , 기아자동차주식회사
发明人： 홍진원 , 추동호 , 김용훈
IPC分类号： F02F11/00 , F16J15/08
CPC分类号： F16J15/061 , F16J15/0825 , F16J15/0831 , F16J2015/085
摘要： PURPOSE: A vehicle gasket is provided to be applied with a double half bead part to the large width part between coupling units, thereby improving sealing efficiency. CONSTITUTION: A vehicle gasket includes a double half bead part and a half bead part. The double half bead part is formed at the relatively large width part between double holes. The half bead part is formed at the relatively small width part between the coupling holes. The double half bead part includes a plurality of double half beads which include a first side land surface (140), a first inclined surface (142), a center land surface, a second inclined surface (146), and a second side land surface (148). The half bead part is overlapped with a plurality of half beads which include a first land surface, an inclined surface, and a second land surface.
摘要翻译：目的：提供一种汽车垫片，以在耦合单元之间的大宽度部分上施加双半胎圈部分，从而提高密封效率。构成：车辆垫圈包括双半胎圈部分和半胎圈部分。双半胎圈部分形成在双孔之间的较大宽度部分。半胎圈部分形成在连接孔之间相对较小的宽度部分。双半胎圈部分包括多个双半胎圈，其包括第一侧面接地面（140），第一倾斜面（142），中心接地面，第二倾斜面（146）和第二侧面（148）。半胎圈部分与包括第一平台表面，倾斜表面和第二平台表面的多个半珠重叠。

6. 发明公开

KR1020120064453A 중력 주조용 금형 및 이를 이용한 중력 주조 방법 有权
标题翻译：使用模具的重量压力铸造模具和重量压力铸造方法
公开(公告)号：KR1020120064453A
公开(公告)日：2012-06-19
申请号：KR1020100125696
申请日：2010-12-09
申请人： 현대자동차주식회사 , 기아자동차주식회사 , 삼신정밀 (주)
发明人： 추동호 , 최동창 , 이재용
IPC分类号： B22C9/22 , B22C9/06 , B22D23/00
CPC分类号： B22C9/103 , B22C9/10 , B22C9/24 , B22C23/00 , B22D25/02
摘要： PURPOSE: A gravity pressure casting mold is provided to easily discharge evaporated gas of mold wash by arranging the end part of a twin scroll part, which becomes an outlet of a turbine housing upwardly, and arranging the sprue of the turbine housing to correspond with the end part of a twin scroll part. CONSTITUTION: A gravity pressure casting mold comprises a first mold, a second mold, an exhaust runner mold(15), a twin scroll mold(17), an auxiliary twin-scroll mold(19), a core supporting mold(21), a gate core(23), an exhaust runner core(25), a twin scroll part core(27), and a bypass part core. The second mold forms the cavity of a turbine housing for the end part of the twin scroll part to face top. The exhaust runner mold forms a sprue in turbine housing side by being corresponded to the end part of the twin scroll part. The twin scroll mold forms the bottom of the cavity of the turbine housing. The core supporting mold installed between the first mold and the second mold, in the other side of the cavity of the turbine housing. The gate core forms a plurality of gate(G) connecting the spure(S) and the cavity of the turbine housing. The exhaust runner core forms an exhaust runner part of the exhaust manifold.
摘要翻译：目的：提供一种重力压力铸造模具，通过将成为涡轮机壳体的出口向上的双涡旋部分的端部布置，并将涡轮机壳体的直浇口对准，从而容易地排出模具清洗的蒸发气体双滚动部分的末端部分。构成：重力压铸模具包括第一模具，第二模具，排气流道模具（15），双涡旋模具（17），辅助双涡旋模具（19），芯支撑模具（21）门芯（23），排气流道铁芯（25），双涡卷部分芯（27）和旁路部分铁芯。第二模具形成用于将双涡卷部分的端部到顶部的涡轮机壳体的空腔。排气流道模具通过对应于双涡卷部件的端部而在涡轮机壳体侧形成浇道。双涡旋模具形成涡轮壳体的空腔的底部。安装在第一模具和第二模具之间的核心支撑模具，在涡轮机壳体的空腔的另一侧。门芯形成连接喷嘴（S）和涡轮壳体的空腔的多个门（G）。排气流道芯形成排气歧管的排气流道部分。

7. 发明公开

KR1020120064452A 터보 차저용 트윈 스크롤 터빈 하우징 无效
标题翻译：涡轮发电机双滚动涡轮机外壳
公开(公告)号：KR1020120064452A
公开(公告)日：2012-06-19
申请号：KR1020100125695
申请日：2010-12-09
申请人： 현대자동차주식회사 , 기아자동차주식회사 , 삼신정밀 (주)
发明人： 박상준 , 추동호 , 이재용
IPC分类号： F02B39/00 , F01D25/24
摘要： PURPOSE: A twin scroll turbine housing for turbochargers is provided to improve castability by distributing thermal stress while equalizing the variation in the sectional area of a flow path. CONSTITUTION: A twin scroll turbine housing(5) for turbochargers comprises two scroll paths, a bypass passage, and a joining part. The two scroll paths is divided by a partition wall(11). The bypass passage is divided by a first partition curtain. . The inner flow path of the joining part is divided through the second partition curtain. The twin scroll turbine housing for the turbochargers is integrally formed with an exhaust manifold through the joining part. The partition wall is tapered toward the front end of the scroll path from the joining part.
摘要翻译：目的：提供一种用于涡轮增压器的双涡轮涡轮机壳体，用于通过分配热应力同时均衡流路截面面积的变化来提高铸造性。构成：用于涡轮增压器的双涡轮涡轮机壳体（5）包括两个涡旋通道，旁通通道和接合部分。两个滚动路径被分隔壁（11）分隔。旁路通道由第一分隔帘幕分开。。连接部分的内部流路通过第二分隔帘幕分开。用于涡轮增压器的双涡轮涡轮机壳体与通过接合部分的排气歧管整体形成。分隔壁从接合部朝向涡旋路径的前端逐渐变细。

8. 发明授权

KR101145629B1 중력 주조용 금형 有权
标题翻译：重型压铸模具
公开(公告)号：KR101145629B1
公开(公告)日：2012-05-15
申请号：KR1020090120051
申请日：2009-12-04
申请人： 현대자동차주식회사 , 기아자동차주식회사
发明人： 추동호 , 고영상
IPC分类号： B22C9/22 , B22C9/10 , B22C9/08
摘要： PURPOSE: A mold for gravity pressure casting is provided to form a separate gas discharging hole at one side of a female mold connected to a turbine cavity, to prevent gas generated by a molten metal and inserted in a lower scroll part from mixing with a molten metal and inserted in a upper scroll part, and to prevent a surface detaching phenomenon. CONSTITUTION: The mold for gravity pressure casting composed of a support mold(15); a gate swirl core(17); a feeder mold; an exhaust runner swirl core(23); a twin scroll part swirl core(25); and a bypass part swirl core(27). The support mold is installed between a female mold and a male mold. The gate swirl core forms a runner interlinking a cavity of an exhaust manifold and a cavity of turbine housing. The gate swirl core forms a plurality of gates. The plurality of gates connects the cavity lower part of the turbine housing. The feeder mold forms a feeder head hole connecting to the cavity of the exhaust manifold. The exhaust runner swirl core forms an exhaust runner part of the exhaust manifold. The twin scroll part swirl core and the bypass part swirl core form a twin scroll part and bypass part respectively.

9. 发明公开

KR1020110062365A 터보차저 일체형 배기매니폴드 구조 无效
标题翻译：排气管结构与涡轮增压器组合
公开(公告)号：KR1020110062365A
公开(公告)日：2011-06-10
申请号：KR1020090119068
申请日：2009-12-03
申请人： 현대자동차주식회사 , 기아자동차주식회사
发明人： 추동호
IPC分类号： F01N13/10 , F02B39/00 , F01N5/04
CPC分类号： Y02T10/16 , F01N13/10 , B60Y2304/03 , B60Y2304/05 , B60Y2400/435 , F01N2260/18 , F01N2340/06 , F01N2410/00
摘要： PURPOSE: An exhaust manifold structure integrated with a turbocharger is provided to ensure increased connectivity strength between the exhaust manifold and the turbocharger since the exhaust manifold has a structure of a 4-2-1 runner and a connecting part is integrated with the leading end of the exhaust manifold. CONSTITUTION: An exhaust manifold structure integrated with a turbocharger is as follows. First to fourth runners are connected to exhaust port of each cylinder of a 4-stroke engine. The first and fourth runners are joined at a first joining part(5a). The second and third runners are joined at a second joining part(5b). Bypass passages are formed on the first and second joining parts, respectively. The bypass passages are a third joining part(5c) to form a structure of 4-2-1 runner.
摘要翻译：目的：提供与涡轮增压器集成的排气歧管结构，以确保排气歧管和涡轮增压器之间的连接强度增加，因为排气歧管具有4-2-1流道的结构，并且连接部分与排气歧管。构成：与涡轮增压器集成的排气歧管结构如下。第一至第四运行器连接到四冲程发动机的每个气缸的排气口。第一和第四流道在第一连接部分（5a）处接合。第二和第三流道在第二连接部分（5b）处连接。旁路通道分别形成在第一和第二接合部分上。旁通通路是形成4-2-1转轮结构的第三接合部（5c）。

10. 发明公开

KR1020100132849A 가스켓 및 이를 구비한 엔진 无效
标题翻译：垫圈和发动机是用垫圈提供的
公开(公告)号：KR1020100132849A
公开(公告)日：2010-12-20
申请号：KR1020090051647
申请日：2009-06-10
申请人： 현대자동차주식회사 , 기아자동차주식회사
发明人： 추동호
IPC分类号： F16J15/12 , F16J15/10
CPC分类号： F16J15/0818 , F02F11/007 , F16J15/0806 , F16J15/128 , Y10S277/908 , Y10S277/935
摘要： PURPOSE: A gasket and engine with the gasket are provided to absorb thermal deformation and secure improved sealing structure around a stud because a gap is formed between a non-metal support member and a metal support member. CONSTITUTION: A gasket(110) comprises first and second metal plates(300a,300b), a metal support member(320), and a non-metal support member(310). The first and second metal plates are located facing each other at an interval to form top and bottom sides, and have stud holes(200) which a stud passes through. The metal support member is interposed along the stud holes between the first and second metal plates. The non-metal support member is filled in the rest space except for the metal support member. The outer surface of the first metal plate contacts the exhaust flange(100) of an exhaust manifold while that of the second metal plate contacts the turbo flange of a turbo supercharger.
摘要翻译：目的：提供具有垫圈的垫圈和发动机以吸收热变形并且确保在螺柱周围的改进的密封结构，因为在非金属支撑构件和金属支撑构件之间形成间隙。构成：垫圈（110）包括第一和第二金属板（300a，300b），金属支撑构件（320）和非金属支撑构件（310）。第一和第二金属板以间隔彼此相对定位以形成顶侧和底侧，并且具有螺柱穿过的螺柱孔（200）。金属支撑构件沿着第一和第二金属板之间的螺栓孔插入。非金属支撑构件填充在除了金属支撑构件之外的其余空间中。第一金属板的外表面接触排气歧管的排气凸缘（100），而第二金属板的外表面接触涡轮增压器的涡轮法兰。

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