엔진용 캠 샤프트
    9.
    发明授权
    엔진용 캠 샤프트 失效
    엔진용캠샤프트

    公开(公告)号:KR100380067B1

    公开(公告)日:2003-04-11

    申请号:KR1020000060274

    申请日:2000-10-13

    Inventor: 권오영

    Abstract: PURPOSE: A camshaft for an engine is provided to improve endurance of the camshaft by locating a welding unit of a hollow shaft on an oil groove-processing unit. CONSTITUTION: A cam shaft of an engine comprises a front end piece(5) installing a cam pulley(3) on a cam shaft(1); a cam(7) formed on an outer portion of a hollow shaft(9); a bolt hole(11) arranged on a front end of the front end piece to mount the cam pulley; am oil seal face(13) mounted on an outer circumference of the bolt hole with a trust face(15); a bearing(19) placed on a neck face(17); and valve lift opening or closing a suction/drain valves by being attached to the cam. A welding unit welded by inserting the front-end piece into the hollow shaft. Thereby, the camshaft of the engine improves endurance of the camshaft by locating the welding unit of the hollow shaft on an oil groove-processing unit.

    Abstract translation: 目的:提供一种用于发动机的凸轮轴,其通过将空心轴的焊接单元定位在油槽处理单元上来提高凸轮轴的耐久性。 构成:发动机的凸轮轴包括在凸轮轴(1)上安装凸轮皮带轮(3)的前端部件(5); 在中空轴(9)的外部形成的凸轮(7); 螺栓孔(11),其布置在前端件的前端以安装凸轮皮带轮; 油封面(13),其安装在螺栓孔的外圆周上并具有可信面(15); 置于颈面(17)上的轴承(19); 和阀门升降机通过连接到凸轮打开或关闭吸入/排出阀门。 通过将前端件插入空心轴而焊接的焊接单元。 由此,通过将空心轴的焊接单元定位在油槽处理单元上,发动机的凸轮轴提高了凸轮轴的耐久性。

    직접분사식 연소실 보울 에지부의 강성을 위한 가공구조
    10.
    发明公开
    직접분사식 연소실 보울 에지부의 강성을 위한 가공구조 无效
    直接喷射式燃烧室的边缘部分刚性加工结构

    公开(公告)号:KR1020020051979A

    公开(公告)日:2002-07-02

    申请号:KR1020000081031

    申请日:2000-12-23

    Inventor: 권오영

    CPC classification number: Y02T10/125

    Abstract: PURPOSE: A machining structure for rigidity of a bowl edge portion of a direct injection type combustion chamber is provided to improve the rigidity of a bowl edge portion of a combustion chamber and increase the durability. CONSTITUTION: A combustion chamber(2) is formed with a bowl machining after cutting the upper surface of a piston(1). A machining structure for rigidity of a bowl edge portion of a direct injection type combustion chamber is formed on the upper surface of a lip portion(22) of the combustion chamber. A crown machining surface(3) has a larger inner diameter than the diameter of the lip portion. A crown machining surface(3) is downward formed toward the lip portion(22). An edge portion, which is a starting point of the lip portion is increased in the diameter. Thus, the rigidity of an edge portion of a combustion chamber is improved.

    Abstract translation: 目的:提供直喷式燃烧室的碗边部的刚性加工结构,以提高燃烧室的碗边部的刚性,提高耐久性。 构成:在切割活塞(1)的上表面之后,燃烧室(2)形成有碗加工。 在燃烧室的唇部(22)的上表面上形成有用于直接喷射型燃烧室的碗边部的刚性的加工结构。 冠加工面(3)的内径比唇部的直径大。 顶面加工面(3)朝向唇部(22)向下形成。 作为唇部的起点的边缘部分的直径增加。 因此,燃烧室的边缘部的刚性提高。

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