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Mechanisms for residence volume reduction in shallow sump

机译:浅水池集水区减少体积的机制

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摘要

Gas turbine aero-engines employ fast rotating shafts that are supported by bearings at several axial locations along the engine. Due to extreme load and heat, oil is injected to the bearings to aid lubrication and cooling. The oil is then shed to the bearing chamber before it is extracted out by a scavenge pump. Scavenging oil from the bearing chamber is challenging due to high windage induced by the fast rotating shafts as well as the two-phase nature of the flow. A deep sump has been found to increase scavenge performance due to its ability to shelter the pooled oil from the bulk rotating air flow thus minimizing two-phase mixing. However in many cases, a deep sump is not an option due to conflicting space requirements. The space limitation becomes more stringent with higher bypass ratio engines as the core becomes smaller. Therefore it is imperative to have a high performing shallow sump. However shape modification of a shallow sump is too constrained due to limited space and therefore has minimal impact on the scavenge performance. This research presents several alternative concepts to improve scavenge performance of a generic baseline shallow sump by augmenting it with attachments or inserts. These augmentations attempt to exploit two known mechanisms for reducing the residence volume: momentum reduction and sheltering. The experimental results show that some augmentations are able to reduce the residence volume of a shallow sump by up to 50% or more in some cases.
机译:燃气涡轮航空发动机采用快速旋转轴,该旋转轴由轴承沿发动机的多个轴向位置支撑。由于极高的负荷和热量,机油会注入轴承中,以帮助润滑和冷却。然后,在通过扫气泵将油抽出之前,将油排到轴承腔。由于快速旋转轴引起的高风阻以及流的两相特性,从轴承腔清除油具有挑战性。已发现深油槽可提高清除性能,这是因为其能够从大量旋转的气流中挡住积聚的油,从而最大程度地减少了两相混合。但是,在很多情况下,由于空间需求冲突,无法选择使用深水坑。随着核心的变小,更高的旁路比发动机的空间限制变得更加严格。因此,必须有一个高性能的浅水槽。然而,由于有限的空间,浅水槽的形状修改太受限制,因此对扫气性能的影响很小。这项研究提出了几个替代概念,通过增加附件或插入物来提高通用基线浅水槽的扫气性能。这些扩充尝试利用两种已知的减少居住量的机制:动量减少和掩蔽。实验结果表明,在某些情况下,进行一些扩建能够使浅水坑的居住量减少多达50%或更多。

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