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Compressor surge based on a 1D-3D coupled method - Part 2: Surge investigation

机译:基于1D-3D耦合方法的压缩机喘振-第2部分:喘振研究

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Compressor characteristics and system parameters, which include pipe lengths, plenum volumes, and throttle coefficients, greatly affect compressor surge. The one-dimensional-three-dimensional (1D-3D) coupled method, is established in Part 1, combines a 3D solver for compressor internal flows and a 1D solver for pipe, plenum, and throttle flows to simulate compressor surge in a compression system, In this paper, the capability of the method to reflect changes of compressor characteristics and system parameters will be demonstrated. Given a centrifugal compressor, variable inlet prewhirl and variable diffuser vanes are employed to adjust compressor characteristics; based on the setup of a datum test rig, the pipe length, plenum volume and throttle coefficient in the 1D solver are modified to get different system setups. Thus, the compressor system can be numerically configured with various compressor characteristics and system parameters, and the 1D-3D coupled method is applied to simulate compressor surge in various configurations. Simulation results show that compressor surge flow rates decrease, and surge periods prolong in the case of positive inlet prewhirl, which is consistent with known results concerning inlet prewhirl; if the diffuser vanes are closed by 5 degrees, the compressor would get out of surge and operate stably, which aligns with expectations. In terms of system parameters, simulation results indicate that the surge period is shortened and the trajectory of surge cycle on the performance map shrinks if the pipe length or plenum volume reduces. Mild surge, mixed surge, and deep surge are captured while the throttle is set with big, moderate and small openings, respectively. Thus, the 1D-3D coupled method is proved being sensitive to changes of compressor characteristics and system parameters, justifying using the 1D-3D coupled method to explore several research topics concerning compressor characteristics and system parameters in compressor surge. This paper lays a foundation of using the 1D-3D coupled method to investigate the relation between compressor surge and stall, compressor surge in a dynamic compression system, structures and dynamics during compressor surge, and the flow instability boundary. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:压缩机的特性和系统参数(包括管道长度,气室容积和节流系数)极大地影响了压缩机的喘振。在第1部分中建立了一维-三维(1D-3D)耦合方法,该方法结合了用于压缩机内部流的3D解算器和用于管道,气室和节气门流的1D解算器,以模拟压缩系统中的压缩机喘振在本文中,将展示该方法反映压缩机特性和系统参数变化的能力。在给定离心式压缩机的情况下,采用可变进气口预涡流和可变扩压器叶片来调节压缩机特性。根据基准测试设备的设置,修改一维求解器中的管道长度,气室体积和节流系数,以获得不同的系统设置。因此,压缩机系统可以在数值上配置各种压缩机特性和系统参数,并且采用1D-3D耦合方法来模拟各种配置下的压缩机喘振。仿真结果表明,在进气预涡旋为正的情况下,压缩机的喘振流量减小,喘振周期延长,这与有关进气预涡旋的已知结果一致;如果扩压器叶片关闭5度,则压缩机将摆脱喘振并稳定运行,这符合预期。在系统参数方面,仿真结果表明,如果管道长度或充气体积减小,性能图上的喘振周期会缩短,喘振周期的轨迹会缩小。当油门分别设置有大,中和小开度时,将捕获轻度喘振,混合喘振和深度喘振。因此,事实证明1D-3D耦合方法对压缩机特性和系统参数的变化很敏感,证明了使用1D-3D耦合方法探索与压缩机喘振相关的压缩机特性和系统参数的若干研究主题是合理的。本文为利用一维至三维耦合方法研究压缩机喘振与失速,动态压缩系统中的压缩机喘振,压缩机喘振期间的结构和动力学以及流动不稳定性边界之间的关系奠定了基础。 (C)2019 Elsevier Masson SAS。版权所有。

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