航空发动机传动齿轮流动显示内窥镜和两相流探头的研制

Hidenori Arisawa, Yuji Shinoda, Noguchi Yoshiyuki, T. Goi, Takahiko Banno, Hirofumi Akahori
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引用次数: 0

摘要

为了减少航空发动机齿轮箱中油流的动功率损失,油流的可视化和测量是有效的。在本文的研究中,我们开发了一种可以定性地显示油流的流动显示内窥镜和一种可以定量测量油气比和流速的两相流探头。流动可视化内窥镜由直径16mm的管道组成,管道中有一个用于去除油雾的空气吹扫通道,内窥镜与照明激光和光学透镜集成在一起,可以实现清晰的高速摄影。两相探头由直径5mm的管道和直径1mm的测量孔组成,管内有压力调节管。为进行验证,采用外围转速为100 m/s、供油量为20 l /min的带冠直齿齿轮。30000帧/秒成像下的流动显示,从叶冠开口流出的油在整个开口宽度上呈湍流扩散。两相流探头测量的油气比和流速表明,叶冠壁面上存在较薄的富油层,且流速较齿轮外周速度慢。我们开发的测量设备易于安装在变速箱上,因此有望应用于实际的航空发动机变速箱。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Developments of a Flow Visualization Borescope and a Two-Phase Flow Probe for Aeroengine Transmission Gears
In order to reduce oil dynamic power loss in aeroengine gearboxes, visualizations and measurements of the oil-flow are effective. In the research presented in this paper, we developed a flow visualization borescope which can qualitatively visualize oil flow and a two-phase flow probe which can quantitatively measure oil/air ratio and the flow velocity. The flow visualization borescope consists of a 16mm diameter pipe in which an air purge passage for removing oil mist and a borescope are integrated with an illumination laser light and optical lenses, enabling clear high-speed photography. The two-phase probe consists of a 5mm diameter pipe with a 1mm diameter measurement hole and has a pressure adjustment pipe inside the pipe. For a demonstration, a shrouded spur gear with 100 m/s peripheral speed and 20 liters/min oil supply was used. Flow visualization at 30000 frame/sec imaging shows that oil outflow from the shroud opening spreads turbulently over the whole width of the opening. Oil/air ratio and flow velocity measurement by the two-phase flow probe show that there was thin oil-rich layer on the shroud wall and the flow speed was slow compared with the gear peripheral speed. The measurement equipment we developed was easily installed to the gearbox and therefore it is expected to apply to real aeroengine gearboxes.
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