基于变循环发动机的空油热交换器在飞行任务中的性能优势评价

Congcong Huang, Guoqiang Xu, J. Wen, Meng Li, Laihe Zhuang
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摘要

在航空发动机中加入空气-油换热器有利于提高涡轮冷却空气的冷却质量,但其对整个飞行包线的影响机理尚不明确。本文通过建立集变循环发动机(VCE)、空气-油换热器、叶片温度评价模型为一体的综合性能仿真模型,对空气-油换热器的性能优势进行评价。结果表明,基于典型飞行任务:在不改变循环参数的情况下增加换热器,降低了发动机的整体性能,但改善了叶片热环境,在各种工况下冷却空气的温降可达到45-214K。增加热交换器,调整引气比或涡轮入口温度,可以明显提高推力。对于这两个参数,调整涡轮入口温度可以获得更大的航空发动机性能提升。在需要大推力的起飞、爬升和空战条件下,推力增加不小于15%,有效提高了装配飞机的爬升率、服役极限和机动性。基于飞行包线:飞行环境对两种模态VCE的影响是一致的,在高ma区域冷却空气温度和叶片表面温度较高。此外,从发动机内部热环境来看,双涵道模式更适合低空低速区域,单涵道模式更适合高空高速区域。此外,换热器可以有效改善高毫安区域热端部件的热环境,保证发动机在安全工况下运行。总之,本研究指出了空气-油热交换器在VCE上的性能优势,为解决未来先进发动机的热问题提供了帮助。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Performance Advantage Evaluation of Air-Oil Heat Exchanger Based on Variable Cycle Engine in Flight Mission
Adding an air-oil heat exchanger to the aero-engine is beneficial to improve the cooling quality of turbine cooling air, while its influence mechanism during the whole flight envelope is still ambiguous. This paper evaluates the performance advantages of the air-oil heat exchanger by building a comprehensive performance simulation model integrating variable cycle engine (VCE), air-oil heat exchanger, and blade temperature evaluation model. The results show, based on typical flight tasks: adding a heat exchanger without changing the cycle parameters reduces the engine’s overall performance, but the blade thermal environment improves, and the temperature drop of the cooling air can reach 45–214K under various operating conditions. Adding a heat exchanger and adjusting bleed air ratio or turbine inlet temperature can increase thrust obviously. For these two parameters, adjusting turbine inlet temperature can gain more enhancement in aeroengine performance. The increase in thrust is no less than 15% in take-off, climbing, and air combat conditions when high thrust is needed, effectively improving the climbing rate, service limit, and maneuverability of the assembled aircraft. Based on the flight envelope: the influence of flight environment on the two modes of VCE is consistent, the cooling air temperature and blade surface temperature are higher in the high-Ma region. Moreover, from the perspective of the engine’s internal thermal environment, double bypass mode is more suitable in low-altitude and low-speed regions, while single bypass mode is more fit in high-altitude and high-speed regions. Furthermore, the heat exchanger can effectively improve the thermal environment of hot-end components in the high-Ma region, ensuring the engine runs in safe conditions. In conclusion, this study points out the performance advantages of air-oil heat exchangers on VCE, which could help solve thermal problems in future advanced engines.
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