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FINE SWIRL FLOW GENERATING DEVICE OF SWIRL CHAMBER TYPE COMBUSTION CHAMBER FOR DIESEL ENGINE

机译:柴油机旋流室式燃烧室的细旋流产生装置

摘要

PURPOSE:To generate a large volume of fine swirl flows in a combustion chamber in which a fine swirl flows generating recessed part is provided on the inner peripheral surface of a nozzle hole communicating a swirl chamber with a main combustion chamber by forming the recessed part of a specially shaped ring-groove formed over the entire periphery in the circumferential direction on the inner peripheral surface of the nozzle hole. CONSTITUTION:With a swirl chamber type combustion chamber 12, a main combustion chamber 1 is communicated through a nozzle hole 2 with a swirl chamber 3, and a fuel injection nozzle 4 faces the swirl chamber 3. Further, a fine swirl flows generating recessed part 5 is provided on the inner peripheral surface of the nozzle hole 2. In this case, the fine swirl flows generating recessed part 5 consists of a ring-groove 10 formed over the entire periphery in the circumferential direction on the inner peripheral surface of the nozzle hole 2, and the ring-groove 10 is shaped so that fine swirl flows are generated over the entire periphery of compressed air flow 6 passing through the nozzle hole 2 in the compression stroke, and fine swirl flows are generated over the entire periphery of expanded gas flow passing through the nozzle hole 2 on the expansion stroke. That is, the ring-groove 10 is formed, at about intermediate position in the axis 14 direction of the nozzle hole 2, into a ring-like form of circular cross section, along a plane intersecting the axis 14 of the nozzle hole 2 at a right angle.
机译:用途:为了在燃烧室中产生大量的细旋流,在细旋流中形成凹部,该凹部设置在通过形成凹部而使旋流室与主燃烧室连通的喷嘴孔的内周面上。在喷嘴孔的内周面上在圆周方向的整个圆周上形成有特殊形状的环形槽。组成:涡流室式燃烧室12,主燃烧室1通过喷嘴孔2与涡流室3连通,燃料喷嘴4面对涡流室3。此外,细微的涡流流动会产生凹进部分在喷嘴孔2的内周面上设置有图5所示的喷嘴。在这种情况下,产生细微的旋流的凹部5由在喷嘴的内周面上在周向上遍及整个圆周的环状槽10构成。孔2的形状和环形槽10的形状使得在压缩冲程中在通过喷嘴孔2的压缩空气流6的整个圆周上产生细旋流,并且在膨胀管的整个圆周上产生细旋流。在膨胀冲程中,气流通过喷嘴孔2。即,环形槽10在喷嘴孔2的轴线14方向上的大约中间位置处沿着与喷嘴孔2的轴线14相交的平面形成为圆形截面的环状。直角。

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