叶片入口深度对多翼离心风机气动性能的影响

    Influence of blade inlet depth on the aerodynamic performance of multi-blade centrifugal fans

    • 摘要: 针对传统清选离心风机因平直叶片结构导致性能差、效率低的问题,以及多翼离心风机设计理论缺乏的现状,该研究基于数值模拟与台架试验,探究叶片入口深度在39~74 mm范围时对风机全压、效率及流场特性的影响规律。研究表明,在额定转速1000 r/min下,增大入口深度能有效抑制涡流产生与流动分离,提升吸入换向能力与进气效率,当叶片入口深度69 mm时性能最优,相较于模型风机,全压提升11.8%,效率提升13.3%,且主频域压力脉动最小化,能量损失降低。基于最优叶轮模型开展台架试验,试验数据与仿真结果误差在9%以内,验证了仿真分析的可靠性。该研究揭示了叶片几何参数对流场的影响机制,可为联合收获机叶轮设计提供理论依据与参数化方法。

       

      Abstract: Centrifugal fans, as critical components of the cleaning device in combine harvesters, significantly influence the aerodynamic performance and operational efficiency of the device. Traditional agricultural cleaning centrifugal fans predominantly feature flat and straight blades, which exhibit suboptimal performance and low efficiency. These conventional designs often suffer from issues such as poor airflow control, excessive turbulence, and significant energy losses. Multi-blade centrifugal fans represent a promising direction for future advancements in agricultural cleaning; however, research on their application in agricultural machinery remains limited, with insufficient reference data available. This study takes the multi-blade centrifugal fan of a large foreign grain combine harvester as the prototype, and reduces its size according to the similarity principle to serve as the benchmark model fan in this paper. A combination of computational fluid dynamics (CFD) and bench experiments was employed to investigate the impact of blade inlet depth on fan performance and flow field characteristics. Firstly, a multi-blade centrifugal fan model is designed based on the similarity theory, the impeller contains 16 fan blades. The depth of the blade inlet is dimensionless to the depth-to-width ratio. Eight sets of impeller models were designed with varying blade inlet depth ranging from 39 mm to 74 mm (corresponding to the depth-to-width ratio of 0.26 to 0.54), focusing on the influence of suction commutating process and inlet efficiency by blade inlet depth of a multi-blade cleaning centrifugal fan. The performance test bench of the fan is set up to regulate the working conditions through the frequency converter, and the photoelectric speed sensor, hot film wind speed sensor and other equipment are used to collect the flow rate, full pressure and other data, so as to verify the reliability of the simulation results. The results demonstrate that optimizing the inlet depth significantly enhances fan performance. At a rated speed of 1000 r/min, increasing the inlet depth can effectively inhibit vortex generation and flow separation, and improve the suction reversal capability and air intake efficiency. The enhanced inlet depth provides a longer acceleration path for the airflow, enabling more efficient conversion of static pressure energy into kinetic energy. This results in a more stable and uniform flow field, reducing the occurrence of turbulent eddies and flow instabilities. The optimal performance is achieved when the blade depth-to-width ratio is increased to 0.46, the total pressure is increased by 11.8% to 194.42 Pa, and the full-pressure efficiency reaches 73.73%. At this time, the peak radial velocity of the airflow is increased by 21.26% compared with LAbs=39 mm, and the area of the high velocity zone at the outlet is enlarged by 24.3%, which significantly improves the uniformity of the flow field. The pressure pulsation analysis shows that the main frequency domain pressure amplitude is minimized at this depth, and the energy loss is reduced. Velocity streamline and vortex cloud analysis reveals that optimizing the inlet depth can delay the boundary layer separation and reduce the return flow at the tongue. 32% of the impeller curvature is increased at LAbs =69 mm, and the airflow completes the momentum conversion at 12 mm from the center disk, which realizes the high-efficiency commutation in advance compared with that of the model. The flow field visualization shows that the flow adhesion on the suction surface is enhanced and the intensity of secondary flow in the blade channel is reduced. Bench tests based on the optimal impeller model are carried out to verify the reliability of the simulation analysis. This study reveals the regulation mechanism of the blade geometric parameters on the scavenging flow field, which provides a theoretical basis and parameterization method for the design of the impeller of the combine harvester. The airflow stability and energy conversion efficiency can be improved by adjusting the inlet depth, which promotes the efficient development of agricultural centrifugal fans.

       

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