Simulated microgravity inhibits cell wall regeneration of Penicillium decumbens protoplasts

This work compares cell wall regeneration from protoplasts of the fungus Penicillium decumbens under rotary culture (simulated microgravity) and stationary cultures. Using an optimized lytic enzyme mixture, protoplasts were successfully released with a yield of 5.3 × 10⁵ cells/mL. Under simulated microgravity conditions, the protoplast regeneration efficiency was 33.8%, lower than 44.9% under stationary conditions. Laser scanning confocal microscopy gave direct evidence for reduced formation of polysaccharides under simulated conditions. Scanning electron microscopy showed the delayed process of cell wall regeneration by simulated microgravity. The delayed regeneration of P. decumbens cell wall under simulated microgravity was likely caused by the inhibition of polysaccharide synthesis. This research contributes to the understanding of how gravitational loads affect morphological and physiological processes of fungi.     

分布式卫星嵌入式计算机系统结构设计方法

针对分布式卫星的运行环境和任务特点,综合考虑分布式卫星嵌入式计算机系统在可靠性、安全性和实时性方面的要求,提出了一种基于三级容错的主辅式双系统体系结构设计方法。论文分析了分布式卫星的特点和星上嵌入式计算机系统的设计要求,对三级容错设计、主辅式双系统安全设计以及基于可信平台模块(TPM)的辅系统设计进行了详细的阐述。该设计方法已成功应用于地面原理验证系统中,结果表明其可以很好地解决分布式卫星嵌入式计算机系统的可靠性、安全性和实时性问题。     

月球探测器软着陆机构

综述了月球探测器软着陆机构的应用与发展现状。介绍了软着陆机构的性能要求和组成,并根据着陆腿结构和缓冲器种类对软着陆机构进行了分类。讨论了着陆器主体设计、着陆腿结构和缓冲器的模块化设计。阐述了着陆器发射、在轨飞行、着陆和着陆后阶段的动力学研究内容。分析了缓冲器设计、着陆机构基本构型设计,以及缓冲器与基本构型主要参数配置等关键技术,对月球探测器软着陆机构设计有一定的参考意义。     

MD110数字程控交换机维护管理和常见故障处理

随着全国民航空管运行调度电话交换通信网的建立与运行,MD110数字程控交换机的日常维护和故障排除变得日趋紧要.论文结合实际工作中的运行维护管理经验,总结出一些MD110数字程控交换机的维护管理和常见故障处理的实用方法.     

浅谈工程项目管理中的过程控制

分析了在工程项目管理中做好工程设计、设备采购、工程施工与合同、工程进度、工程试车及竣工验收等方面的过程控制,从而达到工程项目管理的要求和期望目标。     

Inhibition Effect of Water Injection on Afterburning of Rocket Motor Exhaust Plume

 One of the most important characteristic signatures of the exhaust plume from rocket motor is the afterburning phenomenon, and the injected water into the plume could inhibit the afterburning. The calculation model for the gas-liquid multiphase flow field with chemical reaction in the plume is built. By inducing the energy source terms caused by the vaporization of liquid water, condensation of the vapor and chemical reaction in the energy equation, the gas-liquid multiphase flow field and the afterburning phenomenon are calculated in a coupling way. Mixture multiphase flow model is used to calculate the gas-liquid flow field, and the vaporization mechanism is used to investigate the water vaporization process. The temperature contours are obtained and accord well with the experimental photos. The mass fraction contours of primary species are obtained, which can indicate the extent of inhibition effect of water injection on the afterburning phenomenon in the plume. When water is injected into the plume, the region of afterburning reduces a lot, and temperature on the ground wall declines rapidly, which can de-crease the ablation of the combustion gas to the launch ground.     

贫氧推进剂热值标准装置不确定度评定

介绍了贫氧推进剂热值标准装置的工作原理,并对该装置进行了不确定度分析评定。     

基于串口通信的虚拟仪器平台的设计与测试

设计了一套基于串口通信的虚拟仪器平台。系统硬件采用DSP平台和PC平台协同工作的模式,其中DSP芯片为协处理器,负责信号采集和预处理。PC平台负责信号分析与工作状态控制,用户可以通过开发好的PC平台软件完成对系统的控制,PC机与DSP的通信采用串口实现。分析了串口通信质量对信号测量的影响,实验结果显示串口通信稳定可靠,通信误码对信号分析影响不大,能够满足串口通信虚拟仪器平台的需求。     

利用PLC实现动中通的集中控制

本文针对动中通的集中控制需求,设计了一种基于PLC 的控制系统,目的在于解决当前控制系统的可靠性不高、不便操控、性能不稳定等问题。介绍了以松下的FPX系列晶体管输出型的可编程控制器（PLC）为核心的动中通集中控制系统,详细描述了系统的硬件组成及软件结构,包括PLC 与人机界面（HMI）联机通信,实现人机对话,全方位管理和监控动中通系统的工作状态, 对出现的故障实时报警。     

地形提示与告警系统试飞研究

对地形防撞系统的试飞技术和试飞风险规避进行研究。首先介绍了TAWS子模式功能。然后详细分析了各子模式的试飞技术。阐述了TAWS系统试飞的主要风险源,并分析相应风险源的规避措施。最后,通过实例论证了TAWS试飞技术的应用性,为新型号飞机TAWS试飞工作安全、有效的开展提供了参考。