叶片式MRF减振器阻尼力矩模型的建立

MRF阻尼器具有体积小、能耗低、阻尼力连续可调等优点,是一种对结构实施半主动控制的理想装置,将其用于履带式车辆悬挂系统,可以提高车辆的越野机动性能。介绍了一种以传统叶片式液压减振器为基础设计的叶片式MRF减振器。基于流体的平行板流动模型和MRF的Bingham模型,建立了叶片式MRF减振器的阻尼力矩计算模型。计算结果表明,不加磁场时,叶片式MRF减振器具有与传统叶片式液压减振器相近的阻尼特性,加磁场时,减振器可获得较大的阻尼可调倍数。     

基于UG的液力变矩器叶片参数化设计

液力变矩器叶片的设计工作一直都是液力变矩器设计的重点和难点.为了设计出合理的叶片形状,以提高变矩器的效率,在液力变矩器叶片的参数化设计中,应用了UG软件,把液力计算所得到的参数转化为叶片的实体模型,可以提高液力变矩器的制造水平,缩短研制周期.     

Influence of propagation direction on operation performance of rotating detonation combustor with turbine guide vane

Due to the pressure gain combustion characteristics, the rotating detonation combustor (RDC) can enhance thermodynamic cycle efficiency. Therefore, the performance of gas-turbine engine can be further improved with this combustion technology. In the present study, the RDC operation performance with a turbine guide vane (TGV) is experimentally investigated. Hydrogen and air are used as propellants while hydrogen and air mass flow rate are about 16.1 g/s and 500 g/s and the equivalence ratio is about 1.0. A pre-detonator is used to ignite the mixture. High-frequency dynamic pressure transducers and silicon pressure sensors are employed to measure pressure oscillations and static pressure in the combustion chamber. The experimental results show that the steady propagation of rotating detonation wave (RDW) is observed in the combustion chamber and the mean propagation velocity is above 1650 m/s, reaching over 84% of theoretical Chapman-Jouguet detonation velocity. Clockwise and counterclockwise propagation directions of RDW are obtained. For clockwise propagation direction, the static pressure is about 15% higher in the combustor compared with counterclockwise propagation direction, but the RDW dominant frequency is lower. When the oblique shock wave propagates across the TGV, the pressure oscillations reduces significantly. In addition, as the detonation products flow through the TGV, the static pressure drops up to 32% and 43% for clockwise and counterclockwise propagation process respectively.