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Reaction thrust characteristics of high-pressure submerged water jet of cylinder nozzles 被引量:1
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作者 李晓晖 《Journal of Chongqing University》 CAS 2009年第1期63-69,共7页
The shapes and geometrical parameters of nozzles are key factors for fluidics. The relationship among the reaction thrust, flow rate pressure, diameter do and length L of a cylinder nozzle is analyzed theoretically. T... The shapes and geometrical parameters of nozzles are key factors for fluidics. The relationship among the reaction thrust, flow rate pressure, diameter do and length L of a cylinder nozzle is analyzed theoretically. The simulation of the flow field characteristics was conducted via the FLUENT computational fluid dynamics package. Effects of the inlet conditions and the nozzle dimensions on the reaction thrust of a water jet were addressed particularly. The reaction thrust experiments were performed on a custom-designed test apparatus. The experimental results reveal that a) the nozzle diameter and the inlet conditions exert great influence on the water jet reaction thrust; and b) for L≤4d0, where the nozzle is treated as a thin plate-orifice, the reaction thrust is independent of nozzle length; for L〉4d0, where the nozzle is treated as a long orifice, the reaction thrust can reach maximum under the condition of a certain flow rate. These findings lay a theoretical foundation for the design of nozzles and have significant value, especially for the future development of high-oressure water-let orooulsion technology. 展开更多
关键词 cylindrical nozzle pressure distribution reaction thrust characteristics turbulent flow water jet
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Research on the Structural Rigidity Characteristics of a Reconfigurable TBM Thrust Mechanism 被引量:3
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作者 Younan Xu Xinjun Liu Jiyu Xu 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2019年第6期35-47,共13页
To improve the adaptability of TBMs in diverse geological environments,this paper proposes a reconfigurable Type-V thrust mechanism(V-TM)with rearrangeable working states,in which structural stiffness can be automatic... To improve the adaptability of TBMs in diverse geological environments,this paper proposes a reconfigurable Type-V thrust mechanism(V-TM)with rearrangeable working states,in which structural stiffness can be automatically altered during operation.Therefore,millions of configurations can be obtained,and thousands of instances of working status per configuration can be set respectively.Nonetheless,the complexity of configurations and diversity of working states contributes to further complications for the structural stiffness algorithm.This results in challenges such as difficulty calculating the payload compliance index and the environment adaptability index.To solve this problem,we use the configuration matrix to describe the relationship between propelling jacks under reconfiguration and adopt pattern vectors to describe the working state of each hydraulic cylinder.Then,both the dynamic compatible equation between propeller forces of the hydraulic cylinders and driving forces,and the kinematic harmonizing equation between the hydraulic cylinder displacements and their deformations are established.Next,we derive the stiffness analytical equation using Hooke’s law and the Jacobian Matrix.The proposed approach provides an effective algorithm to support structural rigidity analysis,and lays a solid theoretical foundation for calculating the performance indexes of the V-TM.We then analyze the rigidity characteristics of typical configurations under different working states,and obtain the main factors affecting structural stiffness of the V-TM.The results show the deviation degree of structural parameters in hydraulic cylinders within the same group,and the working status of propelling jacks.Finally,our constructive conclusions contribute valuable information for matching and optimization by drawing on the factors that affect the structural rigidity of the V-TM. 展开更多
关键词 Reconfigurable TBM thrust mechanism Structural rigidity characteristics Configuration matrix Patternvector Kinematic harmonizing equation Dynamic compatible equation Structural stiffness equations
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空间拦截器动力系统小推力高压燃烧室特性研究 被引量:3
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作者 陈新华 沈赤兵 《指挥技术学院学报》 1997年第1期13-20,共8页
介绍了空间拦截器服务系统性能参数预测数学模型,以及数学模型的求解方法。利用此数学模型对高室压和低室压情况下空间拦截器动力系统特性和小推力液体火箭燃烧室的性能进行了计算,简要分析评价了小推力高压燃烧室性能优缺点。
关键词 空间拦截器 动力系统 轨控发动机 燃烧室
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