轮盘榫齿高低周复合疲劳寿命试验研究

某二级涡轮盘榫齿在外场使用中断裂失效严重,连续发生数起二级涡轮盘甩出及叶片脱榫飞出事故.断口分析表明属疲劳和腐蚀交互作用所致,为确保发动机在外场使用的安全,对这种轮盘榫齿在高温状态下,分轻、重腐蚀2种类型进行了高、低周复合疲劳寿命对比试验研究.试验较成功地模拟了实际使用中造成榫齿损坏的主要因素,试验断口表现出明显的疲劳破坏特征,实现了盘齿故障再现,其试验成果为该发动机安全飞行提供了科学依据.      

卫星用热控涂层喷涂方式研究

热控涂层是保证卫星正常工作、延长卫星在轨工作寿命的重要温控手段。传统的喷涂方式虽能满足质量要求,但存在一定的问题。文章结合卫星常用热控涂层的性能和特殊性要求,首先分析了涂层与基底材料的热学性能、力学性能,进而对各种常用喷涂方式进行适用性试验研究,最终确定无气喷涂是较适用于卫星热控涂层的喷涂方式。     

Fouling corrosion in aluminum heat exchangers

Fouling deposits on aluminum heat exchanger reduce the heat transfer efficiency and cause corrosion to the apparatus.This study focuses on the corrosive behavior of aluminum coupons covered with a layer of artificial fouling in a humid atmosphere by their weight loss,Tafel plots,electrochemical impedance spectroscopy(EIS),and scanning electron microscope(SEM)observations.The results reveal that chloride is one of the major elements found in the fouling which damages the passive film and initiates corrosion.The galvanic corrosion between the metal and the adjacent carbon particles accelerates the corrosive process.Furthermore,the black carbon favors the moisture uptake,and gives the dissolved oxygen greater chance to migrate through the fouling layer and form a continuous diffusive path.The corrosion rate decreasing over time is conformed to electrochemistry measurements and can be verified by Faraday’s law.The EIS results indicate that the mechanism of corrosion can be interpreted by the pitting corrosion evolution mechanism,and that pitting was observed on the coupons by SEM after corrosive exposure.     

三坐标测量机上自由型曲面的精确测量

提出自适应扫描测量法和自由型曲面的单有序测量方法,用双三次参数Ｂ样条和最小二乘法建立测头中心轨迹曲面的数学描述,实现测头半径的三维补偿和被测曲面的生成重建。测量步长自动选择,测量过程简便,曲面生成准确度高,适用于三坐标测量机上自由曲面的快速、精确测量和重建。     

GAP/AN推进剂安全性能研究

利用冲击感度和摩擦感度测试研究了聚叠氮缩水甘油醚／硝酸铵（ＧＡＰ／ＡＮ）推进剂及其常用组分的安全性能,指出了影响ＧＡＰ／ＡＮ推进剂冲击感度和摩擦感度的主要因素为硝酸酯（ＢＴＴＮ／ＮＧ）,ＡＰ,ＨＭＸ等添加剂。硝酸铵具有非常低的冲击感度和摩擦感度,是理想的低易损性推进剂的氧化剂。硝酸酯增塑的ＧＡＰ／ＡＮ推进剂不仅具有较高的能量,而且安全性能显著优于ＧＡＰ／ＡＰ,ＧＡＰ／ＨＭＸ,ＧＡＰ／ＨＮＦ推进剂。     

Multi-objective optimal formation reconfiguration with scalarization and stochastic boundaries

A new method is proposed for multi-objective optimal control of satellite formation reconfiguration. First, necessary optimality conditions of single-objective fuel-optimal reconfiguration are studied. Problem of initial guess of the costate and control discontinuity are addressed by using a new developed stochastic based method. Terminal conditions of Two Point Boundary Value Problem (TPBVP) of the optimal control equations are relaxed using augmented Gaussian. Variances or bandwidths of the terminal conditions are set to decision variables to be optimized. Responses of varied initial costate are modeled and propagated using Riccati equation. Using quadratic convolution of relaxed terminal conditions, objective function of the fuel-optimal problem is reformulated into a quadratic equation, and a gradient based optimizer is used to search the optimal initial guess. In the second part of the paper, optimal control of format flying reconfiguration with two competitive objectives:fuel and time of flight (ToF) is studied. With Pascoletti-Serafini scalarization, the Multi-objective Optimal Control Problem (MOCP) is scalarized into a set of weighted Single-objective Optimal Control Problems (SOCP). Hamiltonian and switch function for the weighted SOCP are developed and constructed. New developed stochastic based approach is then used to search the optimal Pareto solutions. Verification and performances of proposed algorithms are demonstrated through numerical simulations of single-objective and multi-objective optimal control of low-thrust elliptical orbit formation reconfiguration. Potential applications of the algorithms to some other preliminary space mission designs are also discussed.     

Long-term time-varying characteristics of UPD products generated by a global and regional network and their interoperable application in PPP

The quality and availability of Uncalibrated Phase Delay (UPD) solutions are crucial to the Precise Point Positioning (PPP) service, and the long-term temporal variability and its contributing factors should be better understood. In this paper, we comprehensively investigate the long-term time-varying characteristics of each UPD product respectively generated by a global and regional network and their interoperable application in PPP-AR (ambiguity resolution), the sampling of the WL and NL UPDs are daily and 30 s, respectively. Firstly, in terms of our 30 day Wide-Lane (WL) UPD products of 31 satellites, the Standard Deviation (STD) of each satellite WL UPDs ranges from 0.04 to 0.06 cycles, indicating that the long-term prediction accuracy of satellite WL UPD is sufficient for fixing Wide-Lane ambiguities. Secondly, when a satellite in eclipsing the discontinulity may corrupt the determination of Narrow-Lane (NL) UPD in form of offset, as a result of lacking or poor satellite attitude dynamic modeling. When the influence of discontinuity is removed, the STD of our estimated satellite NL UPDs is less than 0.05 cycles. Thirdly, the STD of our estimated receiver WL UPDs is mainly below 0.2 cycles, which implies that its stability is one order poorer that of the satellite. In addition, if they are used for stations in and around the network covered region, the stability of the UPD products from the CMONOC (Crustal Movement Observation Network of China) is better than that from a global network, benefit from the fact that all the CMONOC stations are equipped with the same receiver type. Finally, the PPP-AR results show that a rate of 82.9% for stations with a WL-ambiguity-fixed rate of over 90% while 69.5% for stations with an NL-ambiguity-fixed rate of over 80% can be achieved when using UPD from the global network, which is worse than that of using UPD from the CMONOC (85.7% for stations with a WL-ambiguity-fixed rate of over 90% while 75% for stations with an NL-ambiguity-fixed rate of over 80%). The results of the experiment on the UPD interoperable application in PPP show that the global network UPD products can provide a fast AR at any single station, and the convergence time is well below 25 min. Particularly, when the location of a station is in and around the regional network, our results show that the PPP results obtained using regional UPDs enable the consistent use of global UPDs. When the location of a station is far away from the regional network, using the regional UPDs can not achieve PPP-AR. Finally, the WL UPDs of the previous day is used for forecasting to estimate the NL UPDs, the stability analysis results of NL UPDs solution and positioning results are demonstrate the validity of forecasted UPD products.     

含间隙球轴承-转子系统的主共振研究

 为了深刻揭示球轴承-转子系统的共振机理,考虑了重力、装配等因素引起的非对称轴承间隙以及滚珠与滚道之间的Hertz接触,建立了球轴承-转子系统的运动方程,首次应用平均法求得了系统在主共振情况下的解析解,并讨论了系统参数对主共振的影响。根据奇异性理论方法计算得到了系统参数平面上的转迁集,研究了不同参数域内共振解的分岔模式,最后通过数值仿真验证了理论分析的正确性,从而为球轴承-转子系统的振动控制提供了理论依据。