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An experimental study of windage due to rotating and static bolts in an enclosed rotor-stator system

机译:封闭转子 - 定子系统中旋转和静态螺栓的风阻实验研究

摘要

The cooling air in a gas turbine engine is subject to windage as it flows through the internaludair system. The work in this thesis focuses on the windage generated as the cooling airudpasses over the rotor surface, particularly for case where bolts are encountered. Reducingudwindage heating of the cooling air is of great importance to turbomachinery engineers,udparticularly in the aerospace industry, since the use of compressor air for cooling greatlyudreduces the thrust potential of an engine. The ability to accurately predict windage can helpudreduce the quantity of cooling air required, resulting in increased efficiency.ududA purpose built rig was used to measure both windage and rotor surface temperature as airudpasses through an enclosed rotor-stator cavity. A wide range of flow conditions were testedudwith some being close to those found in a modern gas turbine engine. A variety of bothudstator and rotor mounted bolts were investigated, of varying size and shape, as well asudcavities in the disc surface. In addition, PIV measurements of the core tangential velocityudwere obtained.ududTest results show that windage is increased substantially with rotor bolts present, compared with a plain disc, and that it increases with increasing bolt size. For hexagonal rotor bolts a new correlation was produced between the moment coefficient and bolt diameter to pitch ratio for a range of flow conditions, characterised by the rotational and throughflow Reynolds numbers. Stator bolts were shown to generate a large increase in disc surface temperature compared with the plain disc at engine representative conditions.ududPIV measurements of the core tangential velocity showed an increase of up to 80% aboveudthe plain disc with rotor bolts present and no superimposed flow. When throughflow wasudintroduced, the increase was around 300%. These measurements also demonstrate a localudincrease in tangential velocity in the region close to the bolt.
机译:燃气涡轮发动机中的冷却空气在流经内部 udair系统时会受到风阻。本文的工作集中在冷却空气越过转子表面时产生的风阻,特别是遇到螺栓的情况。对于涡轮机械工程师,尤其是在航空航天工业中,减少/降低冷却空气的加热非常重要,因为使用压缩机空气进行冷却大大降低了发动机的推力。准确预测风阻的能力可以帮助减少所需的冷却空气量,从而提高效率。 ud ud当空气穿过封闭的转子-定子腔时,使用专用的钻机测量风阻和转子表面温度。测试了各种流动条件,其中一些条件与现代燃气涡轮发动机中的条件相近。研究了各种安装在 s的螺栓,它们具有不同的大小和形状,以及在圆盘表面上的腔。此外,还获得了铁心切线速度的PIV测量。 ud ud测试结果表明,与普通盘相比,转子螺栓存在时风阻显着增加,并且随螺栓尺寸的增加而增大。对于六角形转子螺栓,在一定流量条件下,力矩系数与螺栓直径与螺距比之间产生了新的相关性,其特征在于旋转雷诺数和通流雷诺数。结果表明,在发动机代表性工况下,定子螺栓与平盘相比会产生很大的表面温度升高。 ud udPIV对芯线切向速度的测量表明,在有转子螺栓的情况下,芯盘的切向速度比平盘高出80%。并且没有叠加的流。引入流量后,增加量约为300%。这些测量结果还表明,在靠近螺栓的区域中,切向速度局部增加。

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    Miles Anna Louise;

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  • 年度 2012
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  • 正文语种 en
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