Thermal insulation and anti-vibration properties of MoSi2-based coating on mullite fiber insulation tiles

Thermal protection materials with excellent thermal insulation properties and high reliability are crucial for aerospace vehicle. Mullite fiber insulation tiles coated with MoSi₂-borosilicate glass (MFIT@MoSi₂) were prepared by a simple slurry method. Results shown that the surface temperature rapidly reached 1043.1 °C under the heat flux of 450 kW/m², while the cold-surface remained at room temperature. The adjusting effects of MoSi₂-based coating on the thermal response and transfer properties of MFIT were investigated systematically. Compared with MFIT, the surface and internal temperatures of MFIT@MoSi₂ were obviously suppressed, due to the existence of MoSi₂-based coating with high emissivity, which effectively enhanced the thermal radiation of the surfaces. Finally, the structural reliability under coupled environment of heating (q₀ = 450 kW/m²) and random vibration with high magnitude (20–2000 Hz, Grms = 20 g) was also investigated. Destructive cracking and peeling of the coating were not observed, due to the excellent bonding strength between the coating and the substrate. The results provided an important basis for the potential application of insulation tiles with mullite fibers in aerospace vehicles and the design of lightweight thermal protection systems.     

The culture at work: cultural ergonomics

Abstract

With the subject matter of ergonomics increasingly broadly conceived, a need is suggested for the systematization and codification of cultural influences on the wide-ranging elements of the field. Pertinent types of systematic analysis, basic and applied research, and training are viewed as necessary, both (a) to generate new knowledge, and (b) to develop culturally appropriate user applications that are important for varied work environments world-wide.     

Design of deployable bistable structures for morphing skin and its structural optimization

The morphing skin is the surface of a deployable frame which can change its shape to present optimal performance in all stages of a task for an aerospace vehicle. This article proposes a deployable frame with low kinematic error and high stability. Mechanical design and optimization of the deployable mechanism are developed, and specifically the analysis model of the deployable mechanism is established by the use of extendable units. The genetic algorithm is employed to find the optimal geometric parameters of the foldable structure. Furthermore, the design method of a bistable compliant mechanism is investigated to achieve the bistability. An example of a morphing leading edge (MLE) is analysed using the proposed method. The results show that the position errors converge to the optimal solution which supplies the minimum value. Numerical analysis indicates that the mechanism can provide two bistable positions for the actual use of the MLE.     

先进材料在高端装备的应用进展

就航天、航空、大型海水淡化装置和深海采油平台所需的关键先进材料及其部件的发展趋势和应用进展作概要的介绍。表明高端装备特别是航空航天和海洋开发利用,是一项复杂的系统工程,需要各种高技术、新材料部件、传感器和大量资金的支撑。指出高性能纤维及其复合材料在高端装备制造中不仅能满足高性能和轻量化要求,对节能减排也有重要贡献,对发展现代国防有极其重要的意义和作用,国家应予大力支持。     

Numerical simulation of rime ice accretion process on an airfoil

To simulate the ice accretion on an airfoil, a boundary moving technique is proposed to deal with the distortion of the airfoil surface due to ice accretion on the leading edge. Incorporating the two‐phase model of air‐supercooled droplets in the Eulerian coordinate system, this technique is applied to simulate the process of the rime ice accretion (the droplets freeze at the instant impinging on the airfoil) on the NACA 0012 airfoil, and the ice profile after ice accretion is achieved successfully. A brief comparison between the results of this paper and the experiment data indicates that the current method is applicable and effective. © 2005 Wiley Periodicals, Inc. Heat Trans Asian Res, 34(4): 226–234, 2005; Published online in Wiley InterScience ( www.interscience.wiley.com ). DOI 10.1002/htj.20064     

航天轴承新贵:60NiTi合金

在NiTi系合金大家族中,等原子比的NiTi合金具有形状记忆效应和超弹性。相比于等原子比NiTi合金,60NiTi合金不会发生热弹性马氏体相变,不具有形状记忆效应和超弹性,但是它在硬度、耐腐蚀性和弹性性能等方面具有出众的潜能,在航天领域上展现了良好的应用前景。固溶态60NiTi合金同时具备结构稳定性、超强的耐腐蚀性、出色的耐磨性,已成为航天轴承候选新材料。     

基于Wiener过程的航天继电器可靠性评估方法

提出了一种利用Wiener过程进行航天继电器可靠性评估的方法。从失效物理的角度判定退化数据是否符合Wiener过程,根据随机过程理论建立了失效概率、失效概率密度以及可靠度的退化模型,并利用极大似然理论对模型中的未知参量进行似然估计,实现可靠性评估。最后对某型号航天继电器进行可靠性寿命试验,验证了所提方法的合理性与有效性。     

MPLS-VPN在跨场区航天数据网中的应用

对分布在不同城市的跨场区航天数据网而言,依托航天骨干网构建各分站内部私有专用网络是迫切所需。将MPLS-VPN(多协议标签交换虚拟专用网),多层标签技术应用到航天数据网中,达到高速转发业务数据和增强其稳定性及安全性。介绍MPLS-VPN的原理及关键技术,结合跨场区航天数据网建设的现状提出一组MPLS-VPN航天数据网结构,分析使用MPLS-VPN实现组网的部署情况,并且实验仿真跨场区航天数据网的组网环境。用2种常用的用户业务数据为场景,通过测试网络的性能指标,验证了采用MPLS-VPN架构方案的优点。     

航天高稳激光源温控电路设计

从航天实际应用角度出发,提出了基于MAX1968芯片的高稳激光源自动温控系统设计方法,介绍设计电路工作原理和组成的同时,给出了关键使用技术优化方案.结合某型号航天项目的具体测试,结果表明该温控电路在实际应用中能够达到双向无死区温控和0.01℃温度稳定性的要求.     

基于供应商关系系数的航天型号供应商过程激励模型

航天型号供应商是一个庞大的网络体系,涉及到国民经济所有的生产部门和技术领域,对如此庞大复杂的供应商系统进行激励是航天型号管理的主要问题之一.在深入研究航天型号供应商激励难点与重点的基础上,本文提炼了航天型号复杂性、长期性与必要性的供应商激励特征.根据项目组与供应商的关系强度提出了航天型号供应商关系系数的概念及其数学模型,构建了基于供应商关系系数的航天型号供应商过程激励模型,并详细阐述了该激励模型的供应商管理功能.