首页> 外国专利> METHOD FOR MAKING ACTUAL EXPANSION STROKE IN EXPANSION STROKE LONGER IN STROKE THAN ACTUAL COMPRESSION STROKE IN COMPRESSION STROKE IN THE CASE OF USING PISTON VALVE AND ROTARY VLAVE IN 4-CYCLE ENGINE OR 6-CYCLE ENGINE

METHOD FOR MAKING ACTUAL EXPANSION STROKE IN EXPANSION STROKE LONGER IN STROKE THAN ACTUAL COMPRESSION STROKE IN COMPRESSION STROKE IN THE CASE OF USING PISTON VALVE AND ROTARY VLAVE IN 4-CYCLE ENGINE OR 6-CYCLE ENGINE

机译:在4冲程发动机或6冲程发动机中使用活塞阀和旋转阀的情况下,使膨胀冲程中的实际冲程比压缩冲程中的实际压缩冲程更长

摘要

PROBLEM TO BE SOLVED: To make the expansion stroke longer than the compression stroke by provid ing a valve and an intake port which are opened at the upper dead center and closed at the lower dead center in the intake stroke, and a valve and an intake port which are opened at the lower dead center and closed before the upper dead center in the compression stroke. SOLUTION: Engines are provided with two types of valves and intake ports. One type of valve and intake port are opened at the upper dead center and closed at the lower dead center in the intake stroke, and the other type of valve and intake port and opened at the lower dead center and closed before the upper dead center. By these two types of valves and intake ports, the stroke of the compression ratio expansion ratio is enabled. Further, space is provided at the tip of passage to two bypass of valves and intake ports, whereby at a next intake stroke, air-fuel mixture or air is reduced to a cylinder. Further, in the case of a 4-cycle engine and a 6-cycle engine, air-fuel mixture is reduced so as to improve fuel efficiency. The passages to the spaces of two types of valves and air ports are provided at the ends of the space, whereby air-fuel mixture or air flows in a fixed direction.
机译:解决的问题:通过在进气冲程中在上止点处打开并在下死点处关闭的阀和进气口以及阀和进气口,使膨胀冲程比压缩冲程更长在压缩冲程中在下止点处打开并在上止点之前关闭的端口。解决方案:发动机配有两种类型的气门和进气口。在进气冲程中,一种类型的阀和进气口在上死点处打开,而在下部死点处关闭,另一种类型的气门和进气口在下死点处打开,并在上死点之前关闭。通过这两种类型的阀和进气口,可以实现压缩比<膨胀比的冲程。此外,在通道的尖端处提供了到阀和进气口的两个旁通的空间,由此在下一个进气冲程中,空气-燃料混合物或空气被减少到气缸中。此外,在四冲程发动机和六冲程发动机的情况下,减少了空气燃料混合物,从而提高了燃料效率。在该空间的端部设有通向两种类型的阀和空气口的空间的通道,由此,空气燃料混合物或空气沿固定方向流动。

著录项

  • 公开/公告号JP2001082187A

    专利类型

  • 公开/公告日2001-03-27

    原文格式PDF

  • 申请/专利权人 NAKADA OSAMU;

    申请/专利号JP19990312794

  • 发明设计人 NAKADA OSAMU;

    申请日1999-09-13

  • 分类号F02D13/02;F01L1/38;F01L7/02;F02B67/00;F02B75/12;

  • 国家 JP

  • 入库时间 2022-08-22 01:30:35

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