卫星用蜂窝板常温胶接工艺

对J-133常温胶接蜂窝板的工艺特性进行对比分析,优选出合适的工艺方法,通过正交试验研究刷胶量、均压板厚度、打压压力对胶接质量的影响,优选出最佳的工艺参数,成功制备验证件。研究表明:最佳涂胶方式为“在面板胶接面依次涂胶,垫一层30g/m²碳毡,再刷上剩余胶液”;热压罐打压方式优于真空袋加压;在一定范围内的均压板厚度对蜂窝板的90°剥离强度影响最大,刷胶量的影响次之,打压压力影响最小;最优的工艺参数组合为:刷胶量350g/m²,均压板厚度为1.5mm,打压压力0.15MPa。根据最佳工艺参数制备出的J-133常温胶接蜂窝板,其胶接质量和力学性能与J78B胶膜中温固化的蜂窝板相近,满足航天设计要求。     

有机硅凝胶离心脱泡工艺研究

为解决传感器类产品使用有机硅凝胶灌封时易产生气泡的问题，同时提高箭上传感器灌封效率和灌封质量，本文采用离心脱泡工艺对有机硅凝胶进行脱泡研究，采用双因素优选试验的设计方法来确定最佳离心脱泡参数范围及最优的离心脱泡工艺参数，并进行脱泡及固化效果检查。实验表明，当采用离心脱泡参数为740 r/min 、12 min时，脱泡效果最佳。固化后胶液切片内的气泡最小直径约24 μm，最大直径约54 μm，且无桥接情况，测其绝缘均大于200 MΩ，无导通或短路情况符合NASA标准及且两个相邻气泡之间不能形成导通短路的要求。通过批量生产与试验验证，采用离心脱泡的工艺方法效果理想、稳定、有效可行，易于批量生产，满足箭上传感器类产品的使用要求。     

不同几何结构对燃油喷嘴热防护特性的影响

试验研究了不同管路结构对燃油结焦性能的影响,结果表明,在1 000 K、150 m/s来流条件和400 K、05 m/s燃油条件下,减小弯管角度和突扩管路的突扩尺寸可以降低结焦附着,且在对管路加热的初始阶段中,结焦量随时间增加会出现波动,在加热15 min时管壁结焦量达到最大,壁面上部分结焦的脱落使结焦量降低。随后,采用试验与数值模拟相结合的方法研究了喷嘴和喷嘴帽罩结构对热防护特性的影响。结果表明,主、副油路同心布置的喷嘴具有最好的热防护效果,在所试验工况下最高可降低湿壁温度近50%,甚至优于带空气隔热层的模型。而喷嘴帽罩对喷嘴出口油温的降低有限,但减小帽罩与喷嘴体的接触或在接触面处填充低热导率的材料仍是有效的改进措施,可降低出口油温约5 K。研究结果对喷嘴的热防护设计具有指导作用。     

基于微分几何纤维缠绕回转壳封头的厚度计算

应用微分几何理论,建立了纤维复合材料在回转壳封头上稳定缠绕的数学模型,推导出了缠绕角、中心角与轴向坐标之间的微分方程。结合缠绕轨迹在封头上叠带的几何关系,给出了厚度的计算方法。算例表明该计算方法反映了纤维缠绕回转壳封头上厚度的分布规律,可直接应用于结构的初步设计。     

注气离心喷嘴喷注过程稳定性试验

为了解管路注气对补燃循环液氧煤油发动机预燃室煤油离心喷嘴喷注过程稳定性的影响，在大气环境下开展了敞口型离心喷嘴注气时喷注过程稳定性试验。使用注气装置在离心喷嘴的上游供应管路中注入空气，通过高速相机记录管路内的两相流特征和喷嘴喷注过程的振荡特征，采用图像区域亮度分析方法定量评估喷注过程的振荡强度。研究发现：注气能显著改变敞口型离心喷嘴的喷注雾化过程及稳定性特征；注气后雾化液膜破碎距离缩短且喷雾角减小，喷注过程出现明显的振荡并伴随Klystron效应；管路内两相流的气泡尺度较大且切向孔较小时，喷注过程的振荡幅值较大；随着注气量增加，喷注过程的振荡频率降低；气泡尺度及两相流型对离心喷嘴喷注振荡过程的影响与普通气泡雾化喷嘴的显著不同，柱状流型时离心喷嘴喷注过程出现1~3 Hz流量振荡且可能间歇性断流。气泡对切向孔的间歇性堵塞作用可能是喷注过程振荡及Klystron效应的原因。     

高模量碳纤维复合材料薄壁管件成型工艺优化研究

为了获得高模量碳纤维复合材料薄壁管件最佳成型工艺参数组合,通过正交试验确定了缠绕工艺参数的大小顺序,经过进一步优化试验及对孔隙率和管件性能分析,得到挤胶装置间隙为0.1~0.12 mm,胶液温度为(40±2)℃,纤维缠绕张力为(10±2)N,加压带缠绕张力为40 N时,管件综合性能最优。     

大厚度复合材料制件(内埋金属)的超声检测分析

采用超声波无损检测及金相试验方法研究了内埋金属件的大厚度复合材料实心部位的微观结构,发现采取0o纤维在金属件周围进行缠绕铺层时容易引起超声波的衰减,分析了超声波衰减的机理,首先预浸料中夹杂微小气泡引起孔隙率较低,形成了复合材料内部的疏松缺陷;其次由固化过程时内应力引起的微裂纹,导致超声波信号发生衰减;另外,纤维屈曲或局部树脂分布不均匀对超声波也有一定影响。     

吸波复合材料回转体构件的缠绕工艺

对吸波复合材料构件的缠绕工艺特性及存在的问题进行了分析,综合现代复合材料缠绕成型工艺,针对含有吸收剂的缠绕层,提出了"双辊同槽、双线夹芯复合"的浸胶工艺制备预浸纱带,以湿法缠绕工艺制备回转体吸波复合材料构件的工艺方法。工艺特性分析表明,选用相应的缠绕规律和工艺参数能够满足不同形态的回转体构件绕制,使吸收剂在各缠绕层中均匀分布、含量可控,保证了制件的吸波性能稳定、质量可靠。     

预浸带缠绕过程缠绕层温度场变化研究

为了研究工艺参数对复合材料缠绕层的温度分布的影响,采用经典热力学理论针对预浸带缠绕过程中的传热机制进行分析;基于缠绕过程中的周期性变化规律,同时以变化的旧层初始温度为传热模型的初始边界条件,构建预浸带缠绕温度分布模型,并通过Matlab编程获得一维热传递模型的精确数值解。理论分析了缠绕初始温度、缠绕速度及芯模温度对缠绕层温度变化的影响。结果表明,对缠绕层温度影响程度依次为芯模温度＞缠绕速度＞缠绕初始温度;而且无论影响参数如何变化,缠绕层的温度分布始终为内层温度较低,并随着径向位置增大,缠绕层温度也在逐渐升高,直到外层最高温度。此外,通过实验对比分析,说明该温度分布模型满足工程要求,可为缠绕工艺研究提供指导。     

影响胶粘剂剪切强度因素的探讨

分析了在胶粘剂剪切强度检测过程中,胶接材料表面处理方法、胶层的厚度、测试时加的垫片厚度和试样的夹距距离、涂胶时的晾置时间等因素对检测结果影响。研究结果表明,上述因素不仅直接影响了胶粘剂粘接强度的大小,而且关系到胶粘剂剪切强度检测试验的测试结果。     

The effect of inlet conditions on the flow and heat transfer in multiple rotating cavity with axial throughflow

This paper discusses experimental results from two different build configurations of a heated multiple rotating cavity test rig.Measurements of heat transfer from the discs and tangential velocities are presented.The test rig is a 70% full scale version of a high pressure compressor stack of an axial gas turbine engine.Of particular interest are the internal cylindrical cavities formed by adjacent discs and the interaction of these with a central axial throughflow of cooling air.Tests were carried out for a range of non-dimensional parameters representative of high pressure compressor internal air system flows(Re up to 5×106 and Rez up to 2×105).Two different builds have been tested.The most significant difference between these two build configurations is the size of the annular gap between the(non-rotating) drive shaft and the bores of the discs.The heat transfer data were obtained from thermocouple measurements of surface temperature and a conduction solution method.The velocity measurements were made using a two component,LDA system.The heat transfer results from the discs show differences between the two builds.This is attributed to the wider annular gap allowing more of the throughflow to penetrate into the cavity.There are also significant differences between the radial distributions of tangential velocity in the two builds of the test rig.For the narrow annular gap,there is an increase of non-dimensional tangential velocity V/Ωr with radial location to solid body rotation V/Ωr=1.For the wider annular gap,the non-dimensional velocities show a decrease with radial location to solid body rotation.      

Research on Auto-detection for Remainder Particles of Aerospace Relay Based on Wavelet Analysis

Aerospace relay is one kind of electronic components which is used widely in national defense system and aerospace system. The existence of remainder particles induces the reliability declining, which has become a severe problem in the development of aerospace relay. Traditional particle impact noise detection (PIND) method for remainder detection is ineffective for small particles, due to its low precision and involvement of subjective factors. An auto-detection method for PIND output signals is proposed in this paper, which is based on direct wavelet de-noising (DWD), cross-correlation analysis (CCA) and homo-filtering (HF), the method enhances the affectiv-ity of PIND test about the small particles. In the end, some practical PIND output signals are analysed, and the validity of this new method is proved.     

Preparation of Highly Dispersed Antimony-doped Tin Oxide Nano-powder via Ion-exchange Hydrolysis of SnCl4 and SbCl3 and Azeotropic Drying

Antimony-doped tin hydroxide colloid precipitates have been synthesized by hydrolysis of SnCl4 and SbCl3 using: (1) an ion-exchange hydrolysis to remove chlorine ions, and (2) isoamyl acetate as an azeotropic solvent to obviate water. The obtained dried powder is of high dispersivity without any need for further grinding. The size and dispersivity of the final particles are investigated with the aid of TG-DTA, BET, XRD and TEM. After having calcined, the antimony-doped tin oxide nanopowder possesses a tetragonal rutile structure with high dispersivity, uniform particles and low hard agglomeration.     

Effects of Mo on the Microstructure and Hydrogen Sorption Properties of Ti-Mo Getters

The effects of Mo on the microstructure evolution, porosity and hydrogen sorption properties of Ti-Mo getters are investigated in this work. The results show that the addition of Mo prolongs the densification process of Ti-Mo getters and results in a significant amount of sintered pores. With the Mo content increasing, the porosity of getters firstly increases reaching the maximum value as it at- tains about 7.5wt.%, and then drops. At the room temperature, the hydrogen sorption property of getters increases progressively with the Mo content increasing, but the tendency is not very clear before its content lies below 2.5wt.%. When the Mo content achieves about 7.5wt.%, the hydrogen sorption property proves to be the best. The discussion is made about the above mentioned phenomena inclusive of hydrogen sorption properties of getters under different activation conditions (from 500-750 ℃).     

超声速燃烧数值模拟中的湍流与化学反应相互作用模型

高精度数值模拟有助于理解超声速湍流燃烧中湍流与化学反应的相互作用,可为发动机燃烧室等工程应用设计提供可靠的预测模型。除直接数值模拟外,目前在湍流燃烧应用中使用的大涡模拟和雷诺平均Navier-Stokes模拟均需要借助模型模化发生在湍流小尺度上的流动与化学反应过程对湍流大尺度运动的影响。现有的湍流与化学反应相互作用模型大致可分为:火焰面类模型和概率密度函数类模型,2类模型在不同的应用中各自具有优势和局限性。此外,现有模型大都基于低马赫数燃烧,而超声速燃烧中通常会伴随快速混合、局部熄火和再着火以及激波等复杂过程,这为发展其中的湍流与化学反应相互作用模型提出了更多的挑战。     

适于低轨卫星IP网络的单核共享树组播算法(英文)

为了解决低轨卫星IP网络中现有典型源组播算法的信道资源浪费问题,本文提出了一套单核共享树组播算法,即核心群合并共享树(CCST)和加权核心群合并共享树(w-CCST)算法。CCST 算法包括动态近似中心(DAC)选核方法和核心群合并组播路径构建方法。DAC方法专为周期、规律运动的低轨卫星网络提出,不需要复杂的星上计算。在核心群合并方法中,以核节点作为初始核心群,通过核心群和剩余组成员的最短路径方法逐步扩展直至整棵组播树构建完成,从而使得组播树的树代价最小,大大提高了网络的带宽利用率和组播传输效率。w-CCST 算法中所提出的加权因子可以调整树代价和端到端传播时延之间的折衷程度,因此,可以通过调整加权因子来适度增大树代价、降低端到端传播时延以支持某些端到端时延要求苛刻的实时组播业务。最后,与低轨卫星 IP 网络中典型算法进行了性能比较,仿真结果说明,CCST 算法的平均树代价比其它算法显著降低,w-CCST 算法的平均端到端传播时延小于 CCST 算法。     

Jet Vectoring Control Using a Novel Synthetic Jet Actuator

A primary air jet vectoring control system with a novel synthetic jet actuator (SJA) is presented and simulated numerically. The results show that, in comparison with an existing traditional synthetic jet actuator, which is able to perform the duty of either “push” or “pull”, one novel synthetic jet actuator can fulfill both “push” and “pull” functions to vector the primary jet by shifting a slide block inside it. Therefore, because the new actuator possesses greater efficiency, it has potentiality to replace the existing one in various appli- cations, such as thrust vectoring and the reduction of thermal signature. Moreover, as the novel actuator can fulfill those functions that the existing one can not, it may well be expected to popularize it into more flow control systems.     

Nonlinear Adaptive Slewing Motion Control of Spacecraft Truss Driven by Synchronous V-gimbaled CMG Precession

The slewing motion control of a truss arm driven by a V-gimbaled control-moment-gyro (CMG) is a nonlinear control problem. The V-gimbaled CMG consists of a pair of gyros that must precess synchronously. The moment of inertia of the system, the angular momentum of the gyros and the external disturbances are not exactly known. With the help of feedback linearization and recursive Lyapunov design method, an adaptive nonlinear controller is designed to deal with the unknown items. Performance of the proposed controller is verified by simulation.     

An SOR Implicit Time-accurate Scheme in Calculating Unsteady Flows

A new time-accurate marching scheme for unsteady flow calculations is proposed in the present work. This method is the combination of classical Successive Over-Relaxation (SOR) iteration method and Jacobian matrix diagonally dominant splitting method of LUSGS. One advantage of this algorithm is the second-order accuracy because of no factorization error. Another advantage is the low computational cost because the Jacobian matrices and fluxes are only calculated once in each physical time step. And, the SOR algorithm has better convergence property than Gauss-Seidel. To investigate its accuracy and convergency, several unsteady flow computa- tional tests are carried out by using the proposed SOR algorithm. Roe’s FDS scheme is used to discritize the inviscid flux terms. Un- steady computational results of SOR are compared with the experiment results and those of Gauss-Seidel. Results reveal that the numerical results agree well with the experimental data and the second-order accuracy can be obtained as the Gauss-Seidel for unsteady flow computations. The impact of SOR factor is investigated for unsteady computations by using different SOR factors in this algorithm to simulate each computational test. Different numbers of inner iterations are needed to converge to the same criterion for different SOR factors and optimal choice of SOR factor can improve the computational efficiency greatly.