首页> 外国专利> Double independent adjustment system for independently adjusting the intake and exhaust cam lobes of a concentric camshaft assembly

Double independent adjustment system for independently adjusting the intake and exhaust cam lobes of a concentric camshaft assembly

机译:双独立调节系统,用于独立调节同心凸轮轴组件的进气和排气凸轮凸角

摘要

A double independent CVD (DIPS) adjuster assembly (120) comprising a first and a second phaser subassembly, each comprising a rotor (122, 128) with outwardly directed wings (124, 136), a stator (128 , 142) having inwardly directed protrusions (130, 144), each of the wings (124, 136) extending between a pair of the inwardly directed protrusions (130, 144) to communicate with chambers (146, 148, 132, 134) for Defining pressurized hydraulic fluid to advance or retain the rotor (122, 128) relative to the stator (128, 142), and front and rear covers (152, 154) covering the front and rear walls of the chambers (146, 148, 132, 134), wherein the rotors (122, 128) are adapted for connection to an inner camshaft (160, 162); a valve pinion (150) or disk that is or with the stator (128, 142) of one of the phaser subassemblies, wherein the valve pinion (150) or disc is configured to transmit radial loads into the outer camshaft (162); and wherein the first and second phaser subassemblies are preassembled as a unit together, characterized in that the second phaser subassembly is radially disposed about the first phaser subassembly and wherein the wings (136) of the second phaser rotor (128) are remote from the stator (128) of the first phaser subassembly extend outwards first adjuster substructure.
机译:双独立CVD(DIPS)调节器组件(120),包括第一移相器和第二移相器子组件,每个子组件均包括具有向外指向的机翼(124、136)的转子(122、128),向内指向的定子(128、142)突起(130、144),每个翼(124、136)在一对向内的突起(130、144)之间延伸,以与腔室(146、148、132、134)连通,以定义加压液压流体前进或相对于定子(128、142)固定转子(122、128),以及覆盖腔室(146、148、132、134)的前壁和后壁的前盖和后盖(152、154),其中转子(122、128)适于连接至内凸轮轴(160、162);气门小齿轮(150)或盘,该气门小齿轮(150)或盘与移相器组件之一的定子(128、142)一起,或者其中,气门小齿轮(150)或盘被配置为将径向载荷传递到外凸轮轴(162)中;并且其中第一和第二移相器子组件作为一个单元预组装在一起,其特征在于,第二移相器子组件围绕第一移相器子组件径向布置,并且第二移相器转子(128)的翼(136)远离定子第一移相器组件的(128)向外延伸第一调节器子结构。

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号