航空活塞发动机冷启动过程中电控参数对混合气形成及燃烧特性的影响及灰色关联分析

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Langjian Yang , Jilin Lei , Dongfang Wang , Xiwen Deng , Dewen Jia , Kang Liu , Liang Sun
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引用次数: 0

摘要

高原或极冷环境下冷启动性能恶化是制约航空活塞发动机环境适应性的主要挑战。建立了表征冷启动运行的三维燃烧数值模型,并通过发动机整体试验和恒容燃烧室(CVCC)喷雾试验进行了验证。研究了6个电控参数对喷雾、混合气形成、点火、燃烧特性及参数灵敏度的影响。结果表明,先导喷射(PiI)策略有助于形成更大的等效比区域(0.6 ~ 1),这有利于主喷射(MI)后喷雾核心周围的点火和燃烧。pii2正时对缸内压力、压力上升速率(PRR)和热释放速率(HRR)的影响最小。增加pii2和pii1的数量会提高燃烧压力,在动力行程期间的PRR和HRR,尽管它们的峰值阶段先提前后延迟。本研究确定最佳心肌梗死时间为- 15°CA BTDC。随着喷射压力从40 MPa增加到160 MPa,喷雾的LPL和VPL逐渐增大,而Sauter平均直径(SMD)逐渐减小。这有利于改善喷雾雾化质量,形成更大的近化学计量当量比区域(0.8 ~ 1.2),加速了低温燃烧(LTC)向高温燃烧(HTC)的转变,从而提高了平均燃烧温度。在温度高于2000 K的区域产生OH,温度越高,OH的生成量越多。同时,在动力行程期间,缸内压力、PRR、HRR及其峰值逐渐增大。对最大缸内压力和OH质量分数峰影响的敏感性顺序为:先导喷射次数>;喷射压力>; pii2量>; pii1量>; pii2定时>;这些发现支持优化电子控制参数,以实现稳健的冷启动策略。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Effects and grey relational analysis of electronic control parameters on mixture formation and combustion characteristics of an aviation piston engine during cold-start
Deteriorated cold-start performance in plateau or extremely cold environments is a major challenge limiting the environmental adaptability of the aviation piston engines. A 3D combustion numerical model characterizing cold-start operation was developed and validated through overall engine tests and constant volume combustion chamber (CVCC) spray experiments. The effects of 6 electronic control parameters on spray, mixture formation, ignition, combustion characteristics, and parametric sensitivity were investigated. Results show that pilot injection (PiI) strategies helped form a larger equivalence ratio region (0.6∼1) that was more favorable for ignition and combustion around the periphery of the spray core after main injection (MI). PiI 2 timing had minimal influence on in-cylinder pressure, pressure rise rate (PRR) and heat release rate (HRR). Increasing PiI 2 and PiI 1 quantities enhanced combustion pressure, PRR and HRR during power stroke, though their phases of peaks first advanced and then retarded. The optimal MI timing in this study was identified as −15 °CA BTDC. As injection pressure increased from 40 to 160 MPa, LPL and VPL of spray gradually increased, while the Sauter mean diameter (SMD) gradually decreased. This facilitated to improvement of the spray atomization quality to form a larger near stoichiometric equivalence ratio region (0.8∼1.2) and accelerated the transition from low-temperature combustion (LTC) to high-temperature combustion (HTC), thus increasing the mean combustion temperature. OH was generated in the region of temperature above 2000 K, and the higher the temperature, the more OH was produced. Simultaneously, during power stroke, in-cylinder pressure, PRR, HRR and their peaks progressively increased. The order of sensitivity to the effects of maximum in-cylinder pressure and OH mass fraction peak was: pilot injection number > injection pressure > PiI 2 quantity > PiI 1 quantity > PiI 2 timing > MI timing. These findings support optimizing electronic control parameters for robust cold-start strategies.
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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