内部旁路条件对变循环高压压缩系统双旁路匹配特性的影响

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-08-13 DOI:10.1016/j.ast.2024.109489
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引用次数: 0

摘要

可变循环高压压缩系统(VCHCS)由核心驱动风扇级(CDFS)和高压压缩机(HPC)组成,它们是控制可变循环发动机旁路比的关键部件。然而,人们对 VCHCS 的双旁路(DB)匹配机制仍然了解不足。本研究重点研究了 VCHCS 在不同代表性内部旁通条件下的 DB 匹配特性。研究结果表明,当内部旁路条件从接近扼流过渡到接近失速时,VCHCS 的外部旁路稳定裕度逐渐减小,HPC 的外部旁路特性曲线呈现近似 "逆时针旋转 "的模式。此外,CDFS 的运行状态以及内外旁路流量的重新分配共同决定了压缩机系统的匹配状态。在前文总结的内部旁路条件对 VCHCS 匹配特性影响的基础上,本研究结合流场分析,解释了典型运行条件下的失速机理。研究发现,当设计点下的内旁路工况和外旁路工况接近失速边界时,低能流体在外侧旁路出口导叶处发生过量积聚,进而引发失速。具体而言,当内部旁路工况接近失速点时,进一步提高或降低外部旁路背压的主要限制因素是大量低能流体在 HPC 第二级定子吸入面上的广泛堵塞。
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Influence of internal bypass conditions on the double bypass matching characteristics of variable cycle high-pressure compression system

The variable cycle high-pressure compression system (VCHCS) consists of a core driven fan stage (CDFS) and a high-pressure compressor (HPC), which are crucial components for controlling the variable cycle engine's bypass ratio. However, the double bypass (DB) matching mechanism of the VCHCS remains insufficiently understood. This study focuses on investigating the DB matching characteristics of the VCHCS under different representative internal bypass conditions. The findings demonstrate that as the internal bypass conditions transition from near choke to near stall, the external bypass stability margin of the VCHCS decreases progressively, and the external bypass characteristic curve of the HPC exhibits an approximate “counter-clockwise rotation” pattern. Furthermore, the operating state of the CDFS and the redistribution of internal and external bypass flow rate, collectively determine the matching state of the compressor system. Building upon the aforementioned summarization regarding the impact of internal bypass conditions on the matching characteristics of the VCHCS, this research integrates flow field analysis to explicate the mechanism of stall under typical operating conditions. The investigation reveals that, when the internal bypass condition under design point and the external bypass condition approaches the stall boundary, an excessive accumulation of low-energy fluid occurs at the external bypass outlet guide vane, subsequently triggers the occurrence of stall. Specifically, when the internal bypass conditions under the near stall point, the predominant limitation on further elevation or reduction of external bypass back pressure lies in the extensive blockage of a massive low-energy fluid on the suction surface of the HPC second stage stator.

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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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