Excellent electromagnetic wave absorption of MOF/SiBCN nanomaterials at high temperature

Electromagnetic wave absorbing materials at high-temperature are urgently needed for stealth aircrafts or aero-engines worked in harsh environments. In this contribution, cobalt-containing siliconboron carbonitride (MOF/SiBCN) nanomaterials were prepared by pyrolyzing metal–organic framework, i.e. cobalt 2-methylimidazole (ZIF-67), and hyperbranched polyborosilazane. The rhombic dodecahedral ZIF-67 and cobalt element promoted in situ formation of dielectric loss phases, including SiC nanocrystals, CoSi nanocrystals and turbostratic carbons. The ZIF-67/SiBCN nanomaterials showed excellent microwave absorption both at room and elevated temperature. The minimum reflection coefficient (RC_min) was −51.6 dB and effective absorption bandwidth (EAB) is 3.93 GHz at room temperature. At an elevated temperature of 600 °C, the RC_min reached −30.29 dB and EAB covered almost the whole X-band (3.95 GHz, 8.45–12.4 GHz). The ZIF-67/SiBCN nanocomposites are promising and useful platform for microwave absorbing materials at high-temperature. It may shed light on the downstream applications in designing next generation areo-engines and stealth aircrafts.     

Transient thermal behavior of stratospheric balloons at float conditions

The prediction of the thermal behavior of stratospheric balloons under varying environmental conditions is one of the key issues in the design and flight test of balloons. In this paper, a three-dimensional transient thermal model is developed to predict the thermal behavior of spherical stratospheric balloons. The diurnal variations of the skin and lifting gas temperatures at float conditions are discussed in detail. The further studies on the thermal behavior of stratospheric balloons are presented also.     

基于RBF神经网络的自适应PID星钟热控制

星钟的频率稳定性决定了星钟提供时间信息的精度,而频率稳定性取决于星钟物理核心温度的稳定程度.基于RBF神经网络逼近星钟热模型,设计自适应PID控制方法实现星钟物理核心的温度控制.仿真验证了算法的有效性.     

月面载荷被动热控技术

由于月面温度环境变化幅度较大,月面载荷需要通过被动热控装置有效控制其与外部环境的换热量,使其本体温度维持在工作或储存温度范围内。文章分析了月面载荷与外部空间环境换热方式;论述了低当量发射率多层隔热组件设计与结构组成;讨论了月面载荷最外表面辐射屏ε和α_s特殊设计及对其表面辐射平衡温度影响;指出利用月壤恒温层及其特性,展开式外多层隔热组件可以在载荷所在月面处形成一个温度相对稳定的月面小环境,其平均温度与当地月壤恒温层温度相当。     

影响气冷式个体热防护装备致冷力的因素分析

个体气冷系统是一种致冷有效、穿着舒适的热防护装备,在设计和使用中 提高其致冷效率是至关重要的。从工程和生理上分析了影响个体气冷系统致冷力的多种 因素,包括供气温度、湿度、流量以及它们之间的相互关系、致冷面积、流量分配、隔热性 能等。得出了提高蒸发性和对流性两类通风服致冷力和舒适性的方法。为不同工况下合理设 计和选用气冷式个体热防护装备,使之具有更高的人机工效和更好的舒适性提供了参考和借 鉴作用。〖JP〗     

帆板驱动影响下的卫星姿态高精度高稳定度控制

受步进电机驱动作用,太阳帆板对日定向时卫星姿态受到影响。本文针对帆板驱动不平稳引起的同卫星姿态耦合干扰,提出了一种卫星姿态稳定和太阳帆板对日定向的复合控制方法。卫星姿态稳定采用自抗扰控制器,以估计补偿由帆板驱动和系统不确定性引起的干扰,并在此基础上,设计了步进电机自适应电流补偿驱动器,以克服帆板驱动机构摩擦力矩和谐波力矩影响。仿真结果表明,该方法能大大提高卫星姿态控制精度和稳定度,同时还改善了帆板对日定向的精度。
     

FOX-7的热分解机理

采用热原位红外、热裂解色谱-质谱、热重分析(TG)、差示扫描量热法(DSC)研究了FOX-7的热分解过程,通过测定程序升温过程中凝聚相的化学结构变化和生成的气相产物,研究了FOX-7的热分解机理。研究结果表明,FOX-7在转晶后可能发生了缩合反应,使其处于缩合产物的平衡状态,随着温度的升高该平衡被打破,FOX-7开始分解成一些小官能团产物和小分子产物;气相产物中首先检测到NO,说明热分解的"脱硝"过程存在硝基与亚硝基互变反应过程。     

Heat Absorbing and Releasing Experiments with Improved Phase-change Thermal Storage Canisters

This article, based on authors' long-term study, proposes an improved foamed-Ni-packed phase-change thermal storage canister, which takes advantage of the foamed-Ni characteristic of instinctive porous structure and excellent properties to ameliorate its void distribution and thermal conductivity. The improved canister and the unimproved one without foamed-Ni package, are put to heat absorbing and releasing tests to investigate the effects of heat absorbing temperature upon the phase-change materials (PCM) melting time under three temperature schemes by using platinum resistance thermometers (PT100) and data acquisition modules (ADAM-4000) to gather the data of varying temperature. Afterwards, the computerized tomography (CT) is employed to scan the void distribution in both canisters. Compared to the unimproved canister, the experimental results evidence the superiority of the improved one in higher uniformity in void and temperature distribution as well as faster thermal responses.     

空间站集成全局热数学模型的建模和分析

为了分析某空间站的综合热性能,建立了该空间站的集成全局热数学模型（IOTMM）。文章介绍了该空间站的物理模型、工作模式、热节点网络模型和流体网络模型,其中流体网络模型主要由氨外回路、低温水回路、中温水回路、舱内通风回路和舱间通风回路组成,最后利用IOTMM分析了空间站在载人飞行模式下各种设备的温度变化情况。     

基于DSP和CAN总线的热功率模拟系统

热功率模拟系统用于测试整星热平衡试验时模拟星上各设备热量分布情况,以检测整星的热控系统性能。本系统采用数字信号处理（DSP）组成单元处理系统,采用控制器局部网（CAN）总线组成通信网络,通过计算机对每一路功率按照预先设定好的功率曲线进行调控、巡检、记录。