共查询到17条相似文献,搜索用时 140 毫秒
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螺旋进气道在铸造和机械加工过程中会出现各种各样的偏差,从而影响直喷式柴油机的动力经济性和排放特性。作者设计了几种机构来模拟不同类型的偏差,如带有倾斜误差的进气道、带有纵向胀大误差的进气道以及带有偏心误差的进气道等。在稳流试验台上检测气道的流动特性。实验结果表明,倾斜气道会显著影响涡流比。抬高气道入口端会明显降低涡流比,反之则涡流比提高;气道胀大会使流量系数和涡流比都降低;当偏心出现在气道出口方向时,涡流比略有增加;当偏心出现在气道入口方向时,涡流比会显著降低。 相似文献
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用自行设计的喷气式可变涡流进气系统(AIVSIS)调节气缸内的涡流水平,试验研究了进气涡流对连用直喷式柴油机微粒排放的影响。结果表明,中速工况为较低的微粒比排放工况,螺旋进气道形成的涡流水平基本可以满足燃料燃烧的要求,改变涡流水平对改善柴油机微粒排放贡献不大。而低速高负荷工况是柴油机较高的微粒比排放区,适度提高气缸内的涡流水平,可以有效降低柴油机微粒的排放量,使微粒降低的主要因素是不可溶组分排放的降低。高速工况螺旋进气道形成的涡流水平较高。降低气缸内的涡流水平可以降低柴油机微粒的排放量,使微粒排放降低的主要因素是可溶性有机组分排放的降低。 相似文献
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基于传统PFI汽油机进气道设计了2种倾角的GDI汽油机进气道,分别进行了2种不同倾角的GDI汽油机进气道的双气门开启、单气门开启2种方式下的气道稳流试验,研究了不同气道倾角的进气道气流特性,以及产生涡流和滚流的能力。试验结果表明:在不同的气门升程下,气道倾角α=39°的进气道比气道倾角α=34°的进气道流量系数大;就滚流比和涡流比而言,当气门升程较大时,单气门开启时比双气门开启时有所增大;当气门升程大于3mm时,α=39°的进气道比α=34°进气道的滚流比和涡流比均有所增大。此外,与普通PFI汽油机进气道相比,2种倾角的GDI汽油机进气道流通性能更佳。 相似文献
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本文主要介绍通过改进进气道形状,减小进气涡流,从而降低6200系列柴油机燃油消耗率和排放烟度的试验研究工作 相似文献
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This paper investigates the effect of intake port configuration on the swirl that is generated within a direct injec- tion (D.I.) diesel engine. The in-cylinder flow characteristics are known to have significant effects on fuel-air mixing, combustion, and emissions. To clarify how to intensify the swirl flow, a swirl control valve (SCV) and a bypass were selected as design parameters for enhancing the swirl flow. The optimal intake port shape was also chosen as a parameter needed to efficiently generate a high swirl ratio. The results revealed that a key factor in generating a high swirl ratio was to control the intake airflow direction passing through the intake valve seat. Further, the swirl intensity was influenced by changing the distance between the helical and tangential ports, and the swirl flow was changed by the presence of a bypass near the intake valve seat. Additionally, the effect of in- take port geometry on the in-cylinder flow field was investigated by using a laser sheet visualization method. The experimental results showed a correlation of swirl ratio and mass flow rate. In addition, we found that employing the bypass was an effective method to increase swirl ratio without sacrificing mass flow rate. 相似文献
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本文针对CA6102发动机燃烧慢、循环变动率偏大等问题,对进气道和燃烧室进行了改进。研究了不同进气道和燃烧结构(六种匹配方案)对燃烧过程和性能的影响,发现涡流比和性能之间无单调的相关关系,与燃烧期之间存在二次抛物线型的逆变相关关系,CA6102发动机合适的涡流比在0.9左右,燃烧室设计因素中火花塞的位置对燃烧过程和性能影响最大,火花塞靠近中心布置方案同原机相比,最低燃油消耗率降低了4.1%,最大扭 相似文献
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