首页> 外国专利> METHOD FOR PERFORMING LONGER STROKE AT REAL EXPANSION STROKE TIME THAN AT REAL COMPRESSION STROKE TIME WHEN PISTON VALVE AND ROTARY VALVE ARE USED IN 4-CYCLE ENGINE AND 6-CYCLE ENGINE

METHOD FOR PERFORMING LONGER STROKE AT REAL EXPANSION STROKE TIME THAN AT REAL COMPRESSION STROKE TIME WHEN PISTON VALVE AND ROTARY VALVE ARE USED IN 4-CYCLE ENGINE AND 6-CYCLE ENGINE

机译:在4冲程和6冲程发动机中使用活塞阀和旋转阀时,在实际膨胀冲程时执行比实际压缩冲程时更长的冲程的方法

摘要

PROBLEM TO BE SOLVED: To transmit energy by an explosion to a piston sufficiently or plenty as much as possible by arranging two kinds of valves and air ports of a valve and an air port which open in the upper dead center and close in the lower dead center at intake stroke time and a valve and an air port which open in the lower dead center and close before the upper dead center at compression stroke time. ;SOLUTION: In case of a 4-cycle engine, three rotary valves 12 to 14 are used. The rotary valve 12 is formed in a cross-sectional H shape, and is provided with an intake port 32 exclusive to an air-fuel mixture and an exhaust port 33, and the rotary valve 13 is formed in a cross-sectional H shape, and is provided with an air port 34 which opens in the upper dead center and closes in the lower dead center at intake stroke time and an air port 35 which opens in the lower dead center and closes before the upper dead center at compression stroke time. The rotary valve 14 is provided with an air port 35 which opens in the lower dead center and closes before the upper dead center at compression stroke time, as a measure against excessively opening time, and an air exclusive intake port 36 which opens before becoming rotational resistance when it excessively expands and closes in the lower dead center at expansion stroke time. Therefore, the ratio of (the compression ratio the expansion ratio) becomes high.;COPYRIGHT: (C)1998,JPO
机译:解决的问题:通过布置在上止点处打开并在下止点处关闭的两种阀以及阀的空气口和空气口,将爆炸产生的能量充分或尽可能多地传递到活塞上在进气冲程时间处于中心位置,并且在压缩冲程时间在下止点处打开并在上止点之前关闭的阀和空气口。 ;解决方案:对于四冲程发动机,使用了三个旋转阀12至14。旋转阀12形成为截面H形状,并设有空气混合气专用的进气口32和排气口33,旋转阀13形成为截面H形状,空气口35具有在进气冲程时在上止点处开口并在下死点处关闭的空气口34和在压缩冲程时在下止点处开口并在上止点之前关闭的空气口35。旋转阀14设置有空气口35,该空气口35在压缩冲程时间在下止点处打开并且在上止点之前关闭,以作为过度打开时间的措施,以及专用进气口36在旋转之前打开。当它在膨胀冲程时间过度膨胀并在下死点闭合时的最大阻力。因此,(压缩比<膨胀比)的比率变高。;版权所有:(C)1998,JPO

著录项

  • 公开/公告号JPH10196376A

    专利类型

  • 公开/公告日1998-07-28

    原文格式PDF

  • 申请/专利权人 NAKADA OSAMU;

    申请/专利号JP19960360058

  • 发明设计人 NAKADA OSAMU;

    申请日1996-12-31

  • 分类号F02B29/08;F01L1/00;F01L1/26;F01L1/38;F01L7/02;F02B29/02;F02B75/02;F02B75/18;

  • 国家 JP

  • 入库时间 2022-08-22 03:05:38

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