基于BICMOS电流控制型多路输出电源的研制

介绍一种适用于低压、宽范围供电的多路输出DC/DC变换器,在功率电路中使用无损耗箝位电路实现了变压器磁芯的复位,控制电路使用第三代BICOMS电流控制型PWM,简化了电路设计、降低了噪声敏感度,给出了多路输出电源中变压器和耦合电感的工程设计的详细过程,同时分析了多路输出耦合电感对负载交叉调节性能的影响.研制的变换器输入电压范围8V-40VDC,输出5V/3A、±15V/0.5A、 10V/0.5A.     

功率MOSFET并联主动均流设计与仿真

功率MOSFET并联在低压大电流领域是一种常见而且有效的解决方案。但是，由于MOSFET器件参数、回路寄生参数以及栅极驱动参数的差异性等因素，功率MOSFET器件并联时常常出现电流不均衡现象。通过Multisim 仿真，分析了MOSFET器件参数因素以及外围电路特性对并联支路静态和动态电流的影响；根据法拉第电磁感应定律以及磁通约束原理，采用耦合电感的均流方法，在并联的各支路中串入共磁芯耦合线圈，实现了各并联支路的电流平衡；然后，通过建立耦合电感的电路以及数学模型，揭示了串入耦合电感实现均流的数学原理。最后，通过仿真验证了串入耦合电感实现并联功率MOSFET均流方法的有效性与可行性。     

快变换交流方波埋弧焊电源研制

设计了一种双逆变电路结构的快变换交流方波埋弧焊电源,该电源由全桥型一次逆变电路和半桥型二次逆变电路组成.二次逆变电路由续流耦合电感、小功率电压尖峰吸收保护逆变回馈电路、IGBT半桥电路构成.一次逆变电路采用了电压、电流双闭环控制,二次逆变电路采用“临界共同导通”的控制策略,并对其电路换向过程进行了分析.试验结果表明,这种交流方波埋弧焊电源在电流换向过程中换向速度快且无过零死区时间,保证了电弧稳定性,具有良好的工程应用前景.     

面向航空结构低频振动的力电耦合超材料板设计

针对航空结构低频振动控制难的问题，提出将负电容与电感电路结合设计具有优异低频振动特性的力电耦合超材料板结构。该超材料板包含作为基底的普通板结构、周期分布在板表面的压电单元及与压电单元相连的包含电感和负电容的分流电路。首先通过有效介质理论，得到了超材料板等效抗弯刚度解析表达式并进行了修正。在此基础上，通过分析负电容对等效抗弯刚度的影响阐明了负电容拓宽禁带的机制。进一步推导了禁带范围的解析表达式，研究了负电容对禁带范围和位置的影响规律，理论结果表明负电容与电感并联可以将禁带宽度拓宽至原来的20倍以上。最后，通过数值算例验证了引入负电容后力电耦合超材料板能够在目标低频范围实现很好的振动抑制效果。     

交直流共用主电路及其控制方法在双输出航空静变电源中的应用

详细介绍一种通过交直流变换共用主电路实现同一电源双路分时输出的方法,给出了交直流共用主电路的拓扑结构及其工作原理,分析了交流变换五电平载波移相及直流变换级联移相控制策略。为了在三相交流变换电路的基础上实现大功率直流输出,并兼顾各相功率均衡,提出了一种相位角同步的均流控制策略。最后通过试验实现了同一电源分时输出交流115 V/400 Hz/100 kVA和直流270 V/80 kW,验证了所述拓扑结构和控制策略的合理性与可行性。     

离子推力器高效高可靠性屏栅电源设计

为了进一步提高离子推力器的可靠性和使用寿命,采用6个电源模块串联输出的方法设计了高效高可靠性的屏栅电源试验样机,每个模块采用全桥LLC谐振变换器,并对屏栅电源模块的性能、打火时开关管的瞬态电流应力分别进行了测试研究。结果表明：屏栅电源模块采用全桥LLC谐振变换器,可以实现零电压开通零电流关断（ZVSZCS）,整个电源的转换效率提高到96.9%;单个电源模块输出电压为210V,电源模块内部没有大于250V 的交流电压峰值,简化了高压绝缘设计的难度;变换器初级较大谐振电感的限流作用使得推力器出现打火时,开关器件瞬态电流仅为40A。该设计可以有效提高屏栅电源的效率和可靠性,可以应用于小行星探测等深空探测航天器的电推进系统。     

某型飞机电源组件多路交流电压输出偏低故障分析与排除

针对电源组件在供电电压18V应急状态下工作时多路交流电压输出偏低故障,对电源组件工作原理进行分析并建立故障树,实现了故障的准确定位和排除,为类似故障排查提供参考。     

航空发动机地面保障车电源系统设计

简述了电源系统的组成及供给能力,并制定了电源系统方案。根据航空发动机地面起动及地面保障车的用电要求,分析了系统的用电功率及设计要求。针对航空发动机在使用中易出现起动机输出轴薄弱环节处断裂现象,采用了合适的限流匹配设计技术。同时,在电源中引入超级电容设计技术,解决了蓄电池等在高原、负温环境条件下性能下降明显的问题,并提高了系统响应特性,增加了发动机瞬间所需功率。最后,通过试验对设计进行了验证。     

基于DSC整流器和双闭环PR逆变器的模块化中频静变电源

与传统中频电源相比,模块化中频静变电源具有选用灵活、可靠性高、冗余性好、便于系统维护等优点。中频静变电源整流器在控制母线电压稳定的同时还要实现单位功率因数控制。为此,具体分析了双电流环控制策略,给出了双电流环控制器中电压电流正负序分离原理和双dq锁相环的具体实现方法,即延时信号抵消(DSC)和双闭环准比例谐振(PR)。针对逆变器输出电压基波无差跟踪困难、谐波含量高等问题,采用双闭环多重准PR控制策略,实现中频电压的稳定输出。仿真和试验结果表明,双电流环控制器能同时实现母线电压稳定和单位功率因数控制,采用双闭环多重准PR控制策略的中频逆变器能够输出稳定的中频交流电压。     

直流稳流电源输出纹波和噪声的测试方法

如何准确测量出直流稳流电源输出纹波和噪声是电源检定／校准工作中需要解决的问题。通过具体事例分析了用不同的测量设备测量同一台电源的纹波电压其结果不同的原因,提出了在测量稳流电源的纹波电压的过程中如何选择负载类型,为实际电源纹波测量工作提供了一些参考。     

Magnetically inflatable SPS with energy storage capability

A new approach to superconductive magnetic energy storage (SMES) for solar power satellite (SPS) with inherent rigidity is introduced in this paper. The rigidity of this SMES originating from the electromagnetic forces within it, can eliminate the need for mechanical building blocks for support structure. This force can also be used for the deployment of the system in space. In addition, the storage capability of the system allows its use in low Earth orbit (LEO) which reduces the launching and transmission costs. The paper also discusses the basic design and the operation of the proposed SPS system     

Porous Alumina Ceramics Fabricated by Spark Plasma Sintering

Porous alumina of regular spherical particles was fabricated with the spark plasma sintering (SPS) and then compared to those ob-tained through conventional hot pressing (HP). The effects of the parameters of the heating process on porosity were also investigated. Microstructural studies suggest that porous ingots including regular pores be made out of regular spherical alumina particles due to the close sphere packages. A comparative study on the relative necks of the specimens produced by SPS and HP indicates an enhancement of neck growth with SPS. Contrasting the theoretical values to the experimental results over the relative necks indicates that a proper relationship between the relative necks and the porosity can be established by a sintering model.     

Influence of SPS casing treatment on axial flow compressor subjected to radial pressure distortion

The present work is about the stall margin enhancement ability of a kind of stall precursor-suppressed (SPS) casing treatment when fan/compressor suffers from a radial total pres-sure inlet distortion. Experimental researches are conducted on a low-speed compressor with and without SPS casing treatment under radial distorted inlet flow of different levels as well as uniform inlet flow. The distorted flow fields of different levels are generated by annular distortion flow gen-erators of different heights. The characteristic curves under these conditions are measured and ana-lyzed. The results show that the radial inlet distortion could cause a stall margin loss from 2% to 30% under different distorted levels. The SPS casing treatment could remedy this stall margin loss under small distortion level and only partly make up the stall margin loss caused by distortion in large level without leading to perceptible additional efficiency loss and obvious change of charac-teristic curves. The pre-stall behavior of the compressor is investigated to reveal the mechanism of this stall margin improvement ability of the SPS casing treatment. The results do show that this casing treatment delays the occurrence of rotating stall by weakening the pressure perturbations and suppressing the nonlinear amplification of the stall precursor waves in the compression system.     

作动器输出机构刚度优化设计与仿真分析

作动器输出机构的变形可以看作是输出轴体扭转变形与摇臂变截面悬臂梁变形的综合。从材料力学的角度出发,详细推导了作动器输出机构机械刚度的理论计算方法,并以此理论为依据对作动器输出机构的结构进行优化设计。通过仿真对比确定优化设计的正确性,为工程应用提供了有力的理论支撑。     

飞机电源系统模拟器的设计

介绍某型号飞机电源系统模拟器的结构和设计原理,详细介绍了C8051F005单片机及其外围的模拟量输入输出电路、数字量输入输出电路、通讯电路和供电电路,并对系统的软件设计进行了阐述。     

Recent development of casing treatments for aero-engine compressors

Casing treatment is a mature stabilization technique which has been widely applied on aero-engines for modern aircrafts and turbo-chargers for automobiles. After the investigations of half century since the 1960s, this technique has been well developed for various configurations with different effectiveness. From the perspective of stabilization mechanism, this paper roughly categorizes the configurations of casing treatment into two types: traditional ones which work by affecting the flow structure of blade tip region; a novel one named as Stall Precursor-Suppressed (SPS) casing treatment. The effectiveness of both types will be demonstrated for their applications on axial compressors and centrifugal compressors with uniform or distorted inlet. And the stabilization mechanism of casing treatments for regular types and SPS one will also be explained respectively. In addition, this review will summarize the methodologies of casing treatments with the numerical simulations for regular grooved configurations and the eigenvalue approach for SPS casing treatment. Looking forward to the future of compressor stabilization, casing treatment technique will still exist as a general and inexpensive option, and the exploration for its effectiveness and mechanism will be deeper with the development of computational fluid dynamics and advanced measurement techniques.     

信号仿真系统离散信号发送功能研究

离散量信号是民用飞机地面模拟试验中不可缺少的信号之一。基于某型号飞机地面模拟试验的需求,提出了简单可靠的离散信号电路设计方案,利用CMOS管和光电耦合器作为输入输出隔离器件,将TTL电平转换成离散量信号。采用电路仿真软件Multisim进行仿真分析,并结合某型号铁鸟试验验证。仿真分析及试验结果表明,该电路满足某型号飞机地面模拟试验对离散量信号的要求。     

航空减压器输出特性回归分析及参数优化

为研究某型航空双级气体减压器设计参数对输出特性的影响规律,建立减压器AMESim模型并与测试结果对比验证;采用响应面法获得减压器设计参数与输出特性的二次回归模型,分析减压器设计参数的影响;利用带精英策略的快速非支配排序遗传算法(NSGA-Ⅱ)对二次回归模型进行优化,得到最优设计参数。响应面结果显示:反馈孔面积是影响输出压力超调量的关键因素,与阀芯密封处动泄漏面积的交互作用对超调量影响显著;阀芯质量是影响输出压力脉动强度的关键因素,与弹簧刚度、膜片刚度的交互作用对脉动强度影响显著。优化结果表明:减压器二级结构的阀芯质量、反馈孔面积、主弹簧刚度、副弹簧刚度、阀芯密封处动泄漏面积和膜片刚度分别为52.26 g、9.06 mm2、67.27 N/mm、10.68 N/mm、0.64 mm2和89.49 N/mm时输出特性达到最优,优化后输出压力超调量降低了28.72%,脉动强度降低了40.63%。      

Experimental investigation on SPS casing treatment with bias flow

Generally, casing treatment（CT） is a passivity method to enhance the stall margin of fan/compressor. A novel casing treatment based on the small disturbance theory and vortex and wave interaction suggestion is a method combining passive control and active control, which has been proved effective at enhancing the stall margin of fan/compressor in experiment. In order to investigate the mechanism of this kind of casing treatment, an experimental investigation of a stall precursor-suppressed（SPS） casing treatment with air suction or blowing air is conducted in the present paper. The SPS casing treatment is designed to suppressing stall precursors to realize stall margin enhancement in turbomachinery. The experimental results show that the casing treatment with blowing air of small quantity can improve the stall margin by about 8% with about 1% efficiency loss. By contrast, the SPS casing treatment with micro-bias flow does not improve the stall margin much more than that without bias flow, even worse. Meanwhile, the present investigation has also attempted to reveal the mechanism of stall margin improvement with the casing treatment.It is found that the stall margin improvements vary with the modification of the unsteady shedding flow and the unsteady wall boundary impedance. The experimental results agree fairly well with the theoretical prediction using a flow stability model of rotating stall.     

Neural controllers for systems with unknown dynamics

This study presents a methodology for specifying a neural controller for a system about which no a priori model information is available. The neural design presumes that a finite duration input/output (I/O) histogram on the system is available. The design procedure extracts from the histogram sufficient information to specify the neural feedback controller. The resultant controller will drive the system along a general output reference profile (unknown during the design). The resultant controller also exhibits the capability of disturbance rejection and the capacity to stabilize unstable plants