船舶与海洋工程

醇类混合燃料发动机运行参数优化

  • 任现冲 ,
  • 高海波 ,
  • 游伏兵 ,
  • 王忠俊 ,
  • 左文博 ,
  • 潘志强
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  • (1.武汉理工大学 船海与能源动力工程学院, 武汉 430063;2.中国船舶重工集团公司第七一一研究所,上海 201101)
任现冲(1997 — ),男,硕士生,E-mail:xianchongren@whut.edu.cn

收稿日期: 2022-02-13

  修回日期: 2022-04-14

  网络出版日期: 2022-04-14

基金资助

国家自然科学基金重点项目(U1709215)

Operating parameters optimization of  alcohol blended fuel engine

  • REN Xian-chong ,
  • GAO Hai-bo ,
  • YOU Fu-bing ,
  • WANG Zhong-jun ,
  • ZUO Wen-bo ,
  • PAN Zhi-qiang
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  • (1. School of Naval Architecture,Ocean and Energy Power Engineering,Wuhan University of Technology,Wuhan 430063,China;2. Shanghai Marine Diesel Engine Research Institute,Shanghai 201101,China)

Received date: 2022-02-13

  Revised date: 2022-04-14

  Online published: 2022-04-14

摘要

为在点燃式发动机上利用醇类混合燃料实现减碳节能的目标,基于 LJ4K18QS 发动机建模,利用醇类混合燃料对运行参数开展优化研究,揭示了空燃比及点火提前角
对发动机动力性、经济性和排放特性的影响规律。 结果表明:在负荷特性下,随着空燃比的增加,发动机扭矩和 NOx排放先增大后减小,发动机燃油消耗率先减小后增大,CO排放逐渐减少,HC 排放逐渐增大;随着点火提前角的减小,发动机的扭矩先增大后减小,燃油消耗率和 CO 排放先减小后增大,NOx 排放逐渐减小,HC 排放逐渐增大;同时,得到了发动机在不同负荷下的最佳空燃比和最佳点火提前角,可为后续研究提供一定的理论参考。

本文引用格式

任现冲 , 高海波 , 游伏兵 , 王忠俊 , 左文博 , 潘志强 . 醇类混合燃料发动机运行参数优化[J]. 大连海事大学学报, 2022 , 48(3) : 72 -79 . DOI: 0. 16411 / j. cnki. issn1006-7736. 2022. 03. 009

Abstract

In  ord er to a chieve t he goal  of re duci ng car bon and saving e nergy by u sing alcoho l blende d fuel on s park ignition engine, bas ed o n LJ4 K1 8QS eng ine modeling, the alcohol ble nded fuel was us ed to op timiz e the operati ng param eters,  an d the i nfluence of air-fue l rat io and ig nition advance angle on engine power, economy and emission characteristics were reve aled . The re sult s show  that un der loa d chara cteri stics, with the increase of air -fuel rati o, engine torque and NOx emission s increase f irstly and then decrea se, e ngine fuel con- sumpt ion decrea ses and then inc reases, CO emissio ns de- crease gradually and H C emission s in crease graduall y. As the ignitio n ad vanc e angle dec reas es, t he engine tor que incre ases firstly and then de creases , the fuel consumpti on rate and CO emission s decrease firs tly a nd then i ncrease, NOx emissi ons dec rease gradu ally and HC emissio ns in crea se gradu ally. At the s am e ti me, the optimu m air-fue l ratio and ignition a dvance ang le of the en gine under different l oad s are obtain ed, which can provide the theo retical refer ence for subsequent research.

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