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Design and Development of a Restricted Intake Manifold for a Naturally Aspirated Four Cylinder SI Engine

机译:用于自然吸气的四缸Si发动机的限制进气歧管的设计与开发

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Intake manifold is one of the principal components of the engine system in the vehicle. The air intake manifold is the passage for air into the engine and thus affects the amount of air quantity. The objective of the present work is to design and development of a strong, reliable and light weight intake manifold for a multi cylinder spark ignition engine. The developed manifold will improve the airflow intake and provide equal mass flow rate in all runners to create better performance. In the present work, combinations of 1-D modeling using Ricardo Wave and CFD simulations on Star CCM+ were employed to substantiate the modeling. The designed manifold is ensured to have a throat velocity of the restrictor close of Mach 1and the plenum was simulated to have a zero velocity creating maximum pressure close to atmospheric pressure. The necessary structural strength to the intake manifold was ensured by performing FEA simulations using ANSYS software. Rapid Prototyping Technique was selected to avoid any disruption in the fluid flow and vortex formations among which Selective Laser Sintering Technique was selected based on decision matrix keeping in mind the strength, reliability, precision and light weightiness of intake components. Following this the testing and validation was carried out on a chassis dynamometer. In comparison with the last intake, there was a torque increment of 7 N-m in the operating engine rpm range, which was accompanied with a variation of nearly 3% in mass flow rate between the four runners. Also, performance curves of the simulation model and dynamometer testing exhibited close resemblance, corroborating the intake model boundary conditions.
机译:进气歧管是车辆中发动机系统的主要组成部分之一。进气歧管是用于空气进入发动机的通道,从而影响空气量的量。本作工作的目的是设计和开发用于多气缸火花点火发动机的强力,可靠,轻便的进气歧管。开发的歧管将改善气流摄入量,并在所有跑步者中提供相同的质量流量以产生更好的性能。在本作本作中,使用使用Ricardo波和CFD模拟的1-D建模的组合,用于证实建模。确保设计的歧管具有用于Mach的限流器关闭的喉部速度,并且模拟增压室以具有零速度产生接近大气压的最大压力。通过使用ANSYS软件执行FEA模拟来确保进气歧管的必要结构强度。选择快速原型技术,以避免流体流动和涡流的任何破坏,其中基于决策矩阵选择选择性激光烧结技术,该判定矩阵保持在进气组件的强度,可靠性,精度和光力。在此之后,测试和验证在底盘测功机上进行。与最后的进气相比,操作发动机RPM范围内存在7 n-m的扭矩增量,其伴随着四个跑道之间的质量流量的近3%的变化。此外,仿真模型和测功机测试的性能曲线表现出紧密相似,证实了进气模型边界条件。

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