Design and analysis of an advanced thermal management system for the solar close observations and proximity experiments spacecraft

In this paper,the mission and the thermal environment of the Solar Close Observations and Proximity Experiments(SCOPE)spacecraft are analyzed,and an advanced thermal management system(ATMS)is designed for it.The relationship and functions of the integrated database,the intelligent thermal control system and the efficient liquid cooling system in the ATMS are elaborated upon.For the complex thermal field regulation system and extreme space thermal environment,a modular simulation and thermal field planning method are proposed,and the feasibility of the planning algorithm is verified by numerical simulation.A solar array liquid cooling system is developed,and the system simulation results indicate that the temperatures of the solar arrays meet the requirements as the spacecraft flies by perihelion and aphelion.The advanced thermal management study supports the development of the SCOPE program and provides a reference for the thermal management in other deep-space exploration programs.

Research on Performance Optimization of Liquid Cooling and Composite Phase Change Material Coupling Cooling Thermal Management System for Vehicle Power Battery

The serpentine tube liquid cooling and composite PCM coupled cooling thermal management system is designed for 18650 cylindrical power batteries,with the maximum temperature and temperature difference of the power pack within the optimal temperature operating range as the target.The initial analysis of the battery pack at a 5C discharge rate,the influence of the single cell to cooling tube distance,the number of cooling tubes,inlet coolant temperature,the coolant flow rate,and other factors on the heat dissipation performance of the battery pack,initially determined a reasonable value for each design parameter.A control strategy is used to regulate the inlet flow rate and coolant temperature of the liquid cooling system in order to make full use of the latent heat of the composite PCM and reduce the pump’s energy consumption.The simulation results show that the maximum battery pack temperature of 309.8 K and the temperature difference of 4.6 K between individual cells with the control strategy are in the optimal temperature operating range of the power battery,and the utilization rate of the composite PCM is up to 90%.

Design and validation of real-time dynamic spectrum management in OFDM-based HNPLC systems

Time-varying frequency selective attenuation and colored noises are unfavorable characteristics of power line communication(PLC) channels of the low voltage networks.To overcome these disadvantages,a novel real-time dynamic spectrum management(DSM) algorithm in orthogonal frequency division multiplexing(OFDM)-based high-speed narrow-band power line communication(HNPLC) systems is proposed,and the corresponding FPGA circuit is designed and realized.Performance of the proposed DSM is validated with a large amount of network experiments under practical PLC circumstance.As the noise in each narrow subcarrier is approximately Gaussian,the proposed DSM adopts the BER/SER expression formulized via the AWGN channel to provide a handy and universal strategy for power allocation.The real-time requirement is guaranteed by choosing subcarriers in group and employing the same modulation scheme within each transmission.These measures are suitable for any modulation scheme no matter the system criterion is to maximize data rate or minimize power/BER.Algorithm design and hardware implementation of the proposed DSM are given with some flexible and efficient conversions.The DSM circuit is carried out with Xilinx KC705.Simulation and practical experiments validate that the proposed real-time DSM significantly improves system performance.

A power and thermal management system for long endurance hypersonic vehicle

Due to the pneumatic heating and combustion effect,the scramjet engine of hypersonic vehicle faces high temperature challenge.It is necessary to comprehensively consider its thermal management and power generation together.A new Power and Thermal Management System(PTMS)combined with Supercritical Carbon Dioxide(SCO_(2))closed Brayton cycle and fuel vapor turbine is proposed and discussed in this paper.The new PTMS can meet the cooling requirement of hypersonic vehicle at Mach number 6–7,and avoid the coking and scrapping in the scramjet cooling channels.Compared with the PTMS only based on fuel vapor turbine,the new PTMS utilizes the waste heat of scramjet to generate more electricity.In addition,it can reduce the use of fuel sink for cooling,and the additional weight penalty can be compensated for long endurance hypersonic flight.

Design and Simulation of High-power LED Array Packaging

Thermal management is one of the key technologies for high-power Light emitting diode(LED)entering into the general illuminating field.Successful thermal management depends on optimal packaging structure and selected packaging materials.In this paper,the aluminum is employed as a substrate of LED,3×3 array chips are placed on the substrate,heat dissipation performance is simulated using finite element analysis(FEA)software,analyzed are the influences on the temperature of the chip with different convection coefficient,and optical properties are simulated using optical analysis software.The results show that the packaging structure can not only effectually improve the thermal performance of high-power LED array but also increase the light extraction efficiency.

Thermal Design for 5 Watt Power LED

With the consideration of the thermal management and heat sink requirements,a cooling device is designed and the thermal resistance of this device is calculated with a single 5 W power LED.The thermal design of a single 5 W power LED is reasonable,effective and the result has been simulated.This design also instruct other power LEDs' thermal design.Provided is a reliable and effective method for the design of power LED illumination lamps and lanterns.

基于集合经验模态分解和多目标遗传算法的火-多储系统调频功率双层优化

针对分布于区域电网不同网络节点的多座储能电站参与电网调频功率调度问题,该文提出一种基于集合经验模态分解(EEMD)和多目标遗传算法(MOGA)的火-多储系统调频功率双层优化策略。该策略包含火-储调频功率优化层和多储能电站调频功率优化层:上层计及火-储调配资源各自优势及剩余调频能力,构建火-储调频功率优化分配模型,完成火-储调频功率的分配;下层引入关于调频成本和荷电状态(SOC)的自适应权重系数,以调频成本最低和SOC均衡为优化目标,完成调频功率在多储能电站之间的分配。仿真结果表明,所提策略可以提升区域电网调频效果并降低调频成本,均衡控制多个储能电站的调频成本和SOC,可以防止经济性较好的储能电站长期处于SOC越限边缘状态,提升储能电站参与调频的积极性和可持续性。

电动汽车电池组冷媒直冷系统工作特性的试验

针对一种利用电动汽车空调制冷剂直接冷却电池组的锂离子电池热管理系统,设计了基于口琴管式冷板的电池模组.进行了直冷和液冷的比较,研究了环境温度、压缩机转速、阀门开度及放电倍率对制冷剂流量和蒸发温度的影响,以及对电池组散热特性的影响.结果表明:采用直冷方式在控制电池组平均温度上比液冷具有更好的冷却效果;压缩机转速增加对电池组有明显的控温效果,在3500 r/min的转速下即使是2.0 C的高倍率放电也能控制温度在40.00℃以下;阀门开度增大有利于电池组平均温度的下降,但不利于电池组温差的降低;在电池组温差较大的情况下,单体电池温差能占到电池组温差的88%.

基于多目标协调的混合储能功率自适应分配方法

混合储能具有良好的功率可控特性,在孤岛微网中常被用作功率缓冲器,补偿分布式电源和负荷多变的功率潮流.围绕储能的功率响应问题,本文设计了混合储能的功率控制方案,并提出了一种基于多目标协调的子单元功率自适应分配方法.首先基于对母线功率供求平衡关系的分析,设计了主从并联型储能功率控制方案.其次利用积分器的“时空调零”特性,实现了子单元的功率自主分配;基于此,考虑了不同荷电状态(SOC)下储能最大充放电功率的差异,设计了子单元的SOC分层管理和多目标功率协调策略.仿真结果表明,所提策略实现的功率分配效果满足子单元的功率响应特性;随着超级电容SOCscn偏移加深,所提策略对SOCscn的优化能力越强,初始SOCscn为97%时能提高10.10%的优化性能,这保障了超级电容作为电压源的功率输出能力;所提策略降低了超级电容常态下的蓄电池的输出深度,蓄电池的最大功率深度降低了46.70%,这提高了蓄电池的使用寿命.

动力电池温度集成控制系统设计与研究

本文以非公路机械动力锂电池为研究对象,围绕动力电池低温加热与高温散热两大关键环节,开展动力电池温度集成控制系统设计与研究。鉴于温度对电池性能及寿命的影响,本文采用挤压成型的铝制型材液冷板,长圆形冷却液道截面,并行布置于模组底部与侧面的方式,实现电池模组的多方向冷却。同时,在电池模组两侧加装电阻式加热片,可使低温下的电池快速升温至适宜温度,确保动力电池发挥良好的充放电性能。动力电池温度集成控制系统能够有效解决电池模组单体电芯温差过大等问题,为动力电池安全高效工作提供强有力保障。

含整体煤气化燃料电池-碳捕集电厂的风火储系统分布鲁棒调度方法

整体煤气化燃料电池(integrated gasification fuel cell,IGFC)是与碳捕集技术高度适配的清洁、高效、稳定的绿色煤电技术,有望克服传统碳捕集技术在低浓度CO_(2)环境下产生的高成本、高能耗问题。该文构建含IGFC碳捕集电厂的风火储发电系统。研究IGFC碳捕集电厂的运行机理,对IGFC内部各环节建立数学模型,提出工况匹配时燃烧利用率和阴极空气利用率需要满足的运行条件,并针对该型碳捕集电厂的电碳特性进行分析。为计及风电出力的不确定性,构建风火储系统的两阶段分布鲁棒经济调度模型,引入k阶适应性理论,提出基于正交支撑子集策略的求解方法来获得鲁棒对等式。最后,在改进IEEE-30节点系统中进行算例分析,结果表明,该型碳捕集电厂可利用阳极碳富集的优势,实现系统低碳经济调度的目标,并验证所提优化方法能为可行解提供可解释性。

计及驾驶风格的氢燃料电池有轨电车自适应能量管理策略

半独立路权运行模式下,氢燃料电池混合动力有轨电车驾驶员的驾驶风格影响锂电池荷电状态,从而对整车运行经济性有较大影响。提出一种结合驾驶员驾驶风格的自适应能量管理策略,以提高能量管理策略对工况和驾驶风格的适应性。首先,考虑不同的道路工况对驾驶员驾驶风格的影响,通过K-均值聚类算法对行驶工况进行识别,将行驶工况分为低速、中速、高速3类;引入冲击度和加速度标准差构建基于模糊逻辑的算法,对驾驶风格进行识别,将驾驶风格分为迟钝型、标准型、激进型3类。其次,建立系统瞬时氢耗量最优的目标函数,在满足约束条件的前提下,引入锂电池荷电状态等效因子修正系数,针对不同驾驶风格调整传统等效氢耗最小策略中相应的等效因子,以实现等效因子随驾驶风格的改变实时变化。最后,将该策略与传统等效氢耗最小策略、庞特里亚金极小值策略进行仿真对比分析,结果表明:该策略能实现3个动力源功率分配最优;锂电池和超级电容荷电状态波动曲线相较于其他2种策略最为平滑;在续驶里程结束时混合动力系统氢耗量为1.39 kg,具有最为优越的燃油经济性;母线电压最大偏移率最小;能使3个动力源平稳出力,具有较强的系统稳定性。研究结果为进一步提高有轨电车实际运行中对驾驶风格的适应性提供参考。

高寒地区纯电动汽车电池热管理系统实用技术探究

新能源汽车动力电池在低温环境下的能量衰减,制约了纯电动汽车的发展。针对电池热管理系统寒冷天气的技术性能,主要基于保温、预热、电池热管理系统管控策略等测试进行分析与研究,为改善动力电池低温性能和对动力电池低温热管理技术的进一步研究提供指导。

质子交换膜燃料电池性能优化控制

质子交换膜燃料电池(proton exchange membrane fuel cell,PEMFC)的热管理,是影响PEMFC安全、稳定、高效运行的核心关键因素。该文在分析PEMFC热管理子系统的结构,以及关键组成部件(包括空气压缩机、冷却液循环泵和冷却风扇)的工作原理基础上,首先搭建耦合热管理子系统的PEMFC非线性仿真模型,进一步将其简化处理得到用于控制的线性模型;在此基础上,设计基于卡尔曼滤波的状态观测器,以实现对状态和不可测量扰动的估计,从而消除模型稳态误差;随后设计目标计算器,以净输出功率跟踪误差最小化和系统效率最大化为目标,对PEMFC系统工作状态进行优化;进而基于线性控制模型,设计无偏显式模型预测控制(offset-free explicit model predictive control,offset-free EMPC),对优化工作状态进行跟踪控制;最后,搭建一个软件在环(softwareintheloop,Si L)测试平台,通过与传统MPC控制策略的仿真结果对比可得,无偏EMPC控制策略可以显著将净输出功率的平均跟踪误差绝对值从344.29W减小到82.19W,系统效率从40.32%提升到46.56%,算法平均单步计算耗时从26ms降低到11.8ms,并且可以约束PEMFC系统运行在稳定和安全的工况。

Analysis and comparison of potential power and thermal management systems for high-speed aircraft with an optimization method

Under the dual effects of aerodynamic heating and high-power electronic equipment heating,the heat sink and power demand of advanced high-speed aircraft have been exponentially rising,which seriously restricts the aircraft performance.To improve system cooling and power supply performance and reduce engine performance loss,a power and thermal management system(PTMS)with high performance,low energy consumption,and light weight urgently needs to be developed.In this paper,three modes of a potential PTMS with different heat sinks and bleed air sources are further discussed to analyze and compare the optimal matching with the flight mission at Mach 1-4.4.The equivalent mass method is used to uniformly assess the costs of the fixed weight,bleed,resistance,etc.as a function of the fuel weight penalty,which is chosen as the optimization objective.The optimization variables consist of the compressor outlet temperature,cooling air flow rate,and fan duct heat exchanger structure size.The results show that the intermediate-stage bleed air and fan duct heat sink are more suitable when the Mach number is less than 2,but the ram air bleed is highly suitable for flight missions at a high Mach number.Especially at Mach 3.4-4.4,the ram air bleed mode can respond to the cooling and power demands with a simple architecture.

分布式电池系统热平衡控制设计

为实现电池系统的温度平衡,提出一种基于分布式的独立输入并联输出(IIPO)电池系统架构的热平衡控制方案。在该系统中,热平衡系统、输出电压控制系统相互结合。在放电操作阶段,通过调节功率转换器的占空比,将调节后的总线电压保持在期望值,并引入电流控制回路来调节每只电池的放电速率,将调节后的电池放电电流保持在期望值,从源头上控制电池产热,以实现热平衡。所提出的热平衡控制器不需要额外的平衡元器件,电池的热平衡会在系统运行期间实现。提出并讨论了控制方案及可行性,并给出概念验证实验样机的理论基础和结果分析,评估和验证热平衡控制器的操作性。

动力电池低温热管理系统评价技术研究

电动汽车的普及对动力电池相关的技术提出了更高的要求,使电池保持在合适温度区间工作的动力电池热管理系统已经成为各大厂商的核心技术需求。由于锂离子电池在冬季低温环境下性能下降、寿命衰减尤为明显,低温热管理技术更是近年来动力电池研究的重点。从锂离子电池在低温环境中的性能劣化机理出发,对低温热管理系统的发展现状进行了综述,并结合最新研究进展,归纳了一套电动汽车低温热管理评价方法。

面向月球基地的自循环热管理及发电系统研究

针对月球基地热管理需求,根据月面热环境特点,设计了一种面向月球基地的新型自循环热管理及发电系统。系统将有机朗肯循环(ORC)和喷射制冷循环(ERC)相结合,以仪器设备散热和太阳能或核能废热为热源,以外部冷背景为冷源,系统内一部分的工质吸收热源,通过有机朗肯循环发电,另一部分工质通过蒸发器吸收航天员日常工作环境中的热量,为航天服和科学研究提供冷量。系统不需要外部电力,可以独立运行,实现发电与制冷。经分析模型计算,在满足月球基地热量收集、传输和排散的基础上,可以实现最大废热制冷率40%以上,总废热利用效率50%以上.