面向型面精度一致性的整体叶盘砂带磨削新方法及实验研究

由于整体叶盘由多个叶片组成,根据"木桶定律",整体叶盘的性能和寿命取决于型面精度(型线精度和表面质量)最差的叶片。因此,在满足整体叶盘型面精度的前提下,提高各叶片型面精度一致性对其性能和寿命具有重要的影响。提出一种面向型面精度一致性的砂带磨削新方法,一方面通过砂带周期性的往复运动结合自锐式磨削原理,实现型面铣削残差层的高效去除;另一方面通过砂带周期性的自动更新,保证各叶片的型面精度在同一截面具有高一致性。阐述并建立了面向型面精度一致性的砂带磨削新方法及其磨削控制方程。在此基础上,对某航空发动机整体叶盘的11个叶片进行了砂带磨削实验,并且运用标准差对整体叶盘型面精度一致性进行定量分析。研究结果表明:整体叶盘磨削后,表面粗糙度小于0.25 μm,型线精度小于0.05 mm,同时型面精度一致性显著提高,证明了该方法的有效性。     

叶片型面砂带磨削技术的现状和发展趋势

叙述了国内外叶片型面砂带磨削的各种技术,分析了一些叶片材料的砂带磨削性能,并介绍了一些典型的叶片砂带磨床.     

双带法快速凝固1050Al薄的成形试验研究

运用具有我国自主知识产权的双带法快速凝固技术将液态 1 0 5 0 Al直接制备成厚度为 1 mm左右的薄带。介绍了这一方法的基本原理、特点等。在可控冷却钢带线速度分别为 1 m/ s、2 m/ s条件下 ,制备了厚度相同的1 0 5 0 Al薄带 ,对所制备的带材进行了金相组织观察 ,可以明显看出 :可控线速度越大 ,组织越精细     

金属氟塑料衬套的研制

聚四氟乙烯金属带材具有极高承载和超长使用寿命等特点，因此，在飞机上得到广泛的应用，以满足高、低温，高负荷，长寿命等苛刻条件下对润滑材料的要求。本文介绍了这种材料的研制过程，并提出了材料的验证试验方法。     

Occurrence features of simultaneous H+- and He+-band EMIC emissions in the outer radiation belt

As an important loss mechanism of radiation belt electrons, electromagnetic ion cyclotron (EMIC) waves show up as three distinct frequency bands below the hydrogen (H⁺), helium (He⁺), and oxygen (O⁺) ion gyrofrequencies. Compared to O⁺-band EMIC waves, H⁺- and He⁺-band emissions generally occur more frequently and result in more efficient scattering removal of <～5?MeV relativistic electrons. Therefore, knowledge about the occurrence of these two bands is important for understanding the evolution of the relativistic electron population. To evaluate the occurrence pattern and wave properties of H⁺- and He⁺-band EMIC waves when they occur concurrently, we investigate 64 events of multi-band EMIC emissions identified from high quality Van Allen Probes wave data. Our quantitative results demonstrate a strong occurrence dependence of the multi-band EMIC emissions on magnetic local time (MLT) and L-shell to mainly concentrate on the dayside region of L?=?～4–6. We also find that the average magnetic field amplitude of H⁺-band waves is larger than that of He⁺-band waves only when L?<?4.5 and AE¹?<?300?nT, and He⁺-band emissions are more intense under all other conditions. In contrast to 5 events that have average H⁺-band amplitude over 2 nT, 19 events exhibit >2 nT He⁺-band amplitude, indicating that the He⁺-band waves can be more easily amplified than the H⁺-band waves under the same circumstances. For simultaneous occurrences of the two EMIC wave bands, their frequencies vary with L-shell and geomagnetic activity: the peak wave frequency of H⁺-band emissions varies between 0.25 and 0.8 f_cp with the average between 0.25 and 0.6 f_cp, while that of He⁺-band emissions varies between 0.03 and 0.23 f_cp with the average between 0.05 and 0.15 f_cp. These newly observed occurrence features of simultaneous H⁺- and He⁺-band EMIC emissions provide improved information to quantify the overall contribution of multi-band EMIC waves to the loss processes of radiation belt electrons.     

On the spatial extent of the proton radiation belt from solar cell output variation of the Akebono satellite

Output current of silicon solar cells of Akebono satellite orbiting in the inner magnetosphere decreased from 13 A in 1989 to about 7 A in 2009, due to accumulated damage by energetic particles. A fair correlation between the monthly decrease rate of solar cell output current and trapped proton flux was found between 1989 and 1992, indicating that trapped energetic protons are responsible for the solar cell degradation. Simple variation from month to month was dominated by a fluctuation with one-year period and the correlation was not discernible after 1993. On the other hand, during orbiting the earth, another kind of decrease of output current emerged at low altitude above the sub-solar point, i.e., in the midst of sunlit condition. The decrease was larger in later years. The fact indicates more prominent temperature effect in the later years because of progress of the degradation. By removing data affected by the orbit condition above, variation from the same month in the previous year shows a clear oscillation due to orbit precession correlated with trapped energetic proton flux up to 1996. The amplitude of the annual variation oscillation tends to be larger than that expected from a degradation model based on energetic proton distribution of the NASA’s AP8 model. The larger oscillation amplitude suggests that the proton radiation belt was more sharply localized than given by the AP8 model throughout the early half of 1990s.     

Solar wind-driven electron radiation belt response functions at 100-min time scales

We present a simple yet numerically robust technique, using autoregressive linear filters, to remove unwanted “colored noise” from solar wind and radiation belt electron data at sub-daily resolution. The remaining signal is then studied using finite impulse response linear prediction filters to represent the driven portion of the linear dynamics that describe the coupling between solar wind speed and electron flux. Sub-daily resolution response profiles covering magnetic L-shells between 1.1 and 8.0 R_E are presented which are consistent with daily resolution response functions. Namely, while there is strong global coherence governing electron flux dynamics, there are at least two distinct responses. The first response is an immediate dropout of electrons between L = 4 and L = 7 that is at least a partly adiabatic effect associated with enhancements in the ring current. This is followed by a 1–2 day delayed enhancement across the same L-shells that is likely a result of increased radial diffusion. The second response is an immediate enhancement seen between L = 3 and L = 4 with a typical duration of less than one day. Plausible explanations for this second response are briefly discussed, but neither empirical nor theoretical evidence can establish conclusively a definite physical cause. Finally, the response profiles show significant solar cycle and seasonal dependencies, indicating that better model output might be achieved with: (1) additional simultaneous solar wind inputs; (2) more sophisticated dynamical model structures capable of incorporating non-linear feedback; and/or (3) time-adaptive linear filters that can track non-stationary dynamics in time.     

网带炉温度及运行时间的测量方法

介绍网带炉在静态不充气、充气及动态充气等状态下，温场的测量方法；并就冷态空载、负载运行时间及加热空载、负载运行时间的测量进行了讨论和分析。     

农林5A型飞机驾驶员座椅FAA适航验证强度分析

介绍了农5A飞机驾驶员座椅在FAA适航取证中的强度验证计算方法。先对农5A飞机驾驶员座椅验证试验假件作用在安全带和肩带上载荷进行了分析,然后施加到座椅强度有限元计算模型上进行计算。座椅经参考强度计算结果设计改进后,顺利完成了强度验证试验,满足了FAA适航要求。本文为小型飞机座椅适航取证提供了思路和方法。