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.

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.

Design Methods for Improving the Performance and Thermal Stability of Radar

The radar power supplies exhibit a complex electronics. The development of more and more compact systems leads to master the interaction between different parts of the power supply while reducing electronic circuits, magnetic and thermal couplings from the constitutive circuitry. The consideration of these phenomena is very difficult at the design of the power supply. This paper presents two complementary methods based first on a circuitry model for the quantification of heat sources and secondly on finite element model for heat diffusion. This approach can help a designer in the goal of improving the performances and thermal stability of radar tied to the supply circuit subset.

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.

Integrated power electronics module based on chip scale packaged power devices

High performance can be obtained for the integrated power electronics module（IPEM） by using a three-dimensional packaging structure instead of a planar structure. A three- dimensional packaged half bridge-IPEM （HB-IPEM）, consisting of two chip scale packaged MOSFETs and the corresponding gate driver and protection circuits, is fabricated at the laboratory. The reliability of the IPEM is controlled from the shape design of solder joints and the control of assembly process parameters. The parasitic parameters are extracted using Agilent 4395A impedance analyzer for building the parasitic parameter model of the HB- IPEM. A 12 V/3 A output synchronous rectifier Buck converter using the HB-IPEM is built to test the electrical performance of the HB-IPEM. Low voltage spikes on two MOSFETs illustrate that the three-dimensional package of the HB-IPEM can decrease parasitic inductance. Temperature distribution simulation results of the HB-IPEM using FLOTHERM are given. Heat dissipation of the solder joints makes the peak junction temperature of the chip drop obviously. The package realizes three-dimensional heat dissipation and has better thermal management.

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.

Challenges and recent progress in thermal management with heat pipes for lithium-ion power batteries in electric vehicles

Electric vehicles(EVs)are globally undergoing rapid developments,and have great potentials to replace the traditional vehicles based on fossil fuels.Power-type lithium-ion batteries(LIBs)have been widely used for EVs,owing to high power densities,good charge/discharge stability,and long cycle life.The driving ranges and acceleration performances are gaining increasing concerns from customers,which depend highly on the power level of LIBs.With the increase in power outputs,rising heat generation significantly affects the battery performances,and in particular operation safety.Meanwhile,the cold-start performance is still an intractable problem under extreme conditions.These challenges put forward higher requirements for a dedicated battery thermal management system(BTMS).Compared to traditional BTMSs in EVs,the heat pipe-based BTMS has great application prospects owing to its compact structure,flexibility,low cost,and especially high thermal conductivity.Encompassing this topic,this review first introduces heat generation phenomena and temperature characteristics of LIBs.Multiple abuse conditions and thermal runaway issues are described afterward.Typical cooling and preheating methods for designing a BTMS are also discussed.More emphasis on this review is put on the use of various heat pipes for BTMSs to enhance the thermal performances of LIBs.For lack of wide application in actual EVs,more efforts should be made to extend the use of heat pipes for constructing an energy-efficient,cost-effective,and reliable BTMS to improve the performances and safety of EVs.

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。

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。

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%.

功率分配方式对船用双堆燃料电池热管理效果分析

为研究船用双堆质子交换膜燃料电池(PEMFC)功率分配方式、热管理系统布置形式对热管理系统性能影响,基于AMESim软件建立了船用双堆PEMFC系统仿真模型,根据试验数据验证了仿真模型的可靠性。在此基础上,以串联式、并联式与旁通式热管理系统模型为研究对象,研究在变载工况下采用功率平均分配、逐级分配策略对电堆进出口冷却水温差的影响规律,最后比较在功率平均分配策略下3种热管理系统布置形式的性能。结果表明,3种热管理系统中电堆进出口冷却水温差均会在不同程度上受到功率分配策略的影响,在功率平均分配策略下,采用串联式热管理系统布置形式更有利于提高电堆内部温度一致性。

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。

电动汽车大功率直流充电热管理系统设计

为提高动力电池在大功率直流充电状况下的充电效率,提出一种基于充电桩热泵系统的电池热管理系统。以某款电动汽车的动力电池为例,研究该热管理系统在-20,-10,0,20和40℃工况下大功率直流充电的温度特性和充电时长问题。使用数值仿真软件对系统进行建模并分析,结果表明,电桩式电池热管理系统响应快、效率高,且最高温度可控制在50℃以下。在低温0,-10和-20℃工况下,相较于原车载式电池热管理系统,可分别为动力电池节约10.6%,17.9%和24.6%的充电时间;在20和40℃工况下可节省1.4%和6.0%的充电时间;对比动力电池各阶段所用的充电时间,所提出的系统主要比原系统减少了电量0~20%范围内的充电时间。

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。

基于温度传感器的通信电源热管理策略研究

文章概述温度传感器的发展现状,分析通信电源热管理当前面临的挑战与需求。通过比较不同类型温度传感器的性能,优化传感器的选择与布局设计,并构建高效的数据采集与处理系统。详细阐述通信电源热管理系统的架构设计、监测预警机制及热管理策略的制定,提出热管理策略的具体实施步骤,强调软硬件协同工作的重要性,并讨论系统的维护与调整方法。

电动汽车动力电池热管理系统设计

针对电动汽车各系统温度调控体系,设计一套电动汽车动力电池热管理系统,包含电机冷却回路、乘员舱热管理回路以及电池热管理回路。在计算系统热量、确定电池温度采用逻辑门限值控制、乘员舱温度采用模糊控制的基础上,利用Comsol和Simulink分别建立动力电池模型和乘员舱及控制系统模型,利用二者进行联合仿真。结果表明:基于标准城市路况条件及大连气候,模拟环境温度35℃下,系统运行3276s时,电池单体最高温度可由40.00℃降至29.05℃,且乘员舱温度维持在25℃左右;模拟环境温度-10℃下,系统运行3276s时,电池单体最低温度可由-10.00℃升至23.19℃,且乘员舱温度满足模糊控制器设定的控制需求。