共查询到16条相似文献,搜索用时 156 毫秒
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目的解决工程结构在交变静载荷和动载荷联合作用下的疲劳寿命预估难题。方法拟设计一梁结构试验件,方便施加静力与动载荷,并具有合适的疲劳寿命,用于静动联合加载下疲劳寿命预估研究。并采用名义应力法计算出静载荷作用下结构的寿命,采用频域法计算动载荷单独作用下结构的寿命,再以线性损伤累积理论为基础,以载荷块为单位来计算静动载荷联合加载下的寿命。结果初步给出试验载荷,得到静动载荷联合加载下危险点的寿命为1225 s。试件在1 h之内失效,满足设计要求。结论通过该方法,可以用来校核试件的实际寿命,以设计试件。 相似文献
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目的 设计一种能够模拟工程塑料实际服役工作环境的试验装置,在多型自然环境中,构建兼具环境因素侵蚀与载荷应力耦合作用的试验条件。方法 研制工程塑料环境因素与载荷应力协同作用试验装置,采用包括拉伸加载、弯曲加载、控制系统等组件的模块化设计,实现0.01~16 Hz加载频率的拉伸及弯曲载荷,最大1 550 kg的拉伸载荷,最大375 kg的弯曲载荷。结果 将研制完成的试验装置置于多型自然环境下对试验施加恒定和交变载荷,以真实模拟工程塑料实际服役中的环境因素与载荷应力协同作用。结论 试验装置制造加工难度小,结构稳定可靠,可用于评价和研究工程塑料等系列类型材料的环境损伤性能演变。 相似文献
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目的考核某型飞机全尺寸雷达罩的静强度,验证其计算模型的准确性。方法采用有限元计算和静力试验相结合的方法,对某型飞机全尺寸雷达罩的承载能力进行研究与试验验证。根据雷达罩的结构特点和载荷分布情况建立有限元计算模型,进行应力应变计算与强度校核,得到了雷达罩的应力应变云图。在此基础上,选用最严重载荷工况对雷达罩的承载能力进行试验验证。通过试验总体方案设计及加载实施方案优化设计,采用矢量加载技术和软硬结合的加载方式对雷达罩施加拉压载荷,保证各加载点的载荷均与所在表面的法向相同,与雷达罩实际受载情况一致。结果雷达罩的应力水平较低,承载能力较高;试验实测应力结果与理论计算结果有偏差,但应力分布规律合理,与理论分析计算结果的趋势基本一致;静力试验结果证明雷达罩及其与机身连接结构能够满足静强度设计要求。结论雷达罩静力试验测得的应变数据与有限元计算结果吻合较好,雷达罩本体及其与机身的连接结构满足强度设计要求。 相似文献
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目的 模拟飞机结构承受静压载荷与噪声载荷时的真实情况,为飞机设计初期阶段设计选型提供试验数据支持。方法 使用压缩空气进行静压加载,模拟噪声与正压、噪声与负压联合加载,并以静压载荷0.06 MPa、噪声载荷151 dB为例,进行了试验验证。结果 在噪声与静压载荷同时作用下,若静压载荷过大,结构会发生塑性变形。结论 提出的飞机选型阶段噪声与静压载荷联合加载的试验方法,实现了噪声与静压(正压与负压)联合加载,并通过飞机壁板声静联合试验,验证了飞机壁板结构的噪声与静压联合试验方法。 相似文献
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本文介绍一座新型氧化塘的研究和设计.该塘污水停留仅一天,表面负荷140g/m~2·d.当原污水BOD_5为100mg/L、SS为120mg/L时,经初沉池分别去除30%和50%,至氧化塘出水BOD_5和SS均为30—40mg/L.经过各阶段试验和120m~2/d中间试验均达到预期效果.现已用于广州大坦沙15×10m/d污水处理厂设计. 相似文献
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《Journal of Manufacturing Processes》2002,4(1):77-85
Reconfigurable tooling is an attractive prospect for aerospace sheet metal forming because many different part shapes must be produced in small numbers. This paper describes the design and test of a particular type of “discrete-die” reconfigurable tool. The discrete-die concept involves using the ends of densely packed rod-shaped elements as the working surface of the die. The rod-shaped elements are reconfigured manually or automatically to change the shape of the die. Numerous mechanical schemes can be employed to move the elements: this paper describes the use of a shaft-driven lead screw concept. The input shaft turns continuously, and each pin's position is controlled by the engagement of an individual clutch. The required design parameters were developed using a combination of theory and experiment, and a laboratory-scale working prototype device was built and tested. The design parameters included an evaluation of the suitability of open-loop pin-position control based only on time, an evaluation of the torque capacity, engagement time, and reliability of the clutches, and the development of design loads. Experience in construction of the prototype showed that the design concept was sound but that significant enhancements to the control system would be required in a full-scale device. 相似文献
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Joseph F. Wilson Brad L. Kinsey Yannis P. Korkolis 《Journal of Manufacturing Processes》2013,15(4):580-585
Characterization of the evolving yield loci and forming limit diagrams for sheet materials under biaxial loading is necessary for the development of accurate sheet metal forming process simulations. Biaxial tension testing has been shown to have significant advantages over the current computational and experimental methods for such material characterization; however, the few commercially available loading frames are far too large and expensive to be practical for most metal forming research laboratories. In this paper, the design of a practical servohydraulic biaxial loading frame is presented. The design, control, and operation of the loading frame are discussed in detail, and experimental data is provided to validate the effectiveness of the control system with respect to specimen center shifting. 相似文献