航空发动机高速球轴承动态特性分析

 高速滚动轴承的动态特性对航空发动机转子系统的性能有重要的影响,为尽可能真实模拟轴承实际运转情况,建立轴承零件相互作用模型得到各零件之间力和力矩,使用较精确的弹流模型计算拖动力,采用拟动力学法建立任意受载的球轴承动力学分析模型,提出了工程中非线性方程组的高效解法。编制调试了计算程序READ ( Rolling Element bearing Advanced Dynamics tool),以276927NK1W1(H)航空轴承为算例分析了工况参数和结构参数对滚动轴承动态特性的影响规律,最后通过Gupta的动力学程序算例验证了程序的准确性。轴承动态特性的研究为研究航空发动机转子轴承集成系统动态性能分析奠定了基础。     

旋转式机械故障诊断的一种方法

探讨一种利用噪声频谱对旋转式机械故障进行诊断的方法。介绍动静摩擦故障对噪声频谱影响的模拟试验 ,并探讨这种方法的应用     

More on a possible modulation barrier in the outer heliosphere

The new concept of a possible modulation barrier in the outer heliosphere is discussed further. It is argued that since barrier-type modulation is characterized by large radial gradients in the outskirts of the heliosphere, while they remain almost constant in the rest of the heliosphere, it is already contained in drift and in terminal shock acceleration models. Combined with the expected coalescence of transients at large radial distances this may contribute to a very effective modulation barrier at large radial distances.     

Posterior Cramer-Rao bounds for multi-target tracking

This study is concerned with multi-target tracking (MTT). The Cramer-Rao lower bound (CRB) is the basic tool for investigating estimation performance. Though basically defined for estimation of deterministic parameters, it has been extended to stochastic ones in a Bayesian setting. In the target tracking area, we have thus to deal with the estimation of the whole trajectory, itself described by a Markovian model. This leads up to the recursive formulation of the posterior CRB (PCRB). The aim of the work presented here is to extend this calculation of the PCRB to MTT under various assumptions.     

单个RP-3航空煤油液滴的超临界蒸发实验研究

目前以航空发动机为背景的针对液态碳氢燃料的超临界蒸发研究很少,鉴于未来高性能航空发动机的研制需求,选取国产RP-3航空煤油为研究对象,对液滴的超临界蒸发进行了研究。分析了蒸发过程中不同环境参数下液滴无量纲直径的平方随时间的变化规律,实验结果表明超临界蒸发与常规亚临界蒸发特性存在很大的差异;根据实验结果绘制了液滴蒸发时间随环境参数变化的曲线图,并分析了蒸发过程中不稳定度的变化规律,发现在不同的温度范围内环境压力对液滴蒸发时间的影响规律是截然不同的,同时不稳定度Bi随环境温度及压力的升高而增大;对不同工况下液滴的瞬态蒸发常数以及平均蒸发常数进行了定量计算,分析认为影响液滴蒸发常数的两个主要因素是环境温度和环境压力,且后者占主导地位。     

探针支杆对压气机转子性能及流场影响的数值模拟研究

为了研究探针支杆对压气机转子性能及流场的影响,以低速轴流压气机单转子为研究对象,利用定常和非定常计算方法分析了在转子叶片上游50%弦长位置处安装探针支杆后转子整体性能及流场结构的变化。结果表明:支杆的存在会使压气机转子设计点静压升下降1.09%,损失增大8%;近失速点静压升下降0.8%,损失增大4.2%。同时支杆尾迹会周期性改变泄漏涡的形态与强度,不会改变泄漏涡破碎导致的泄漏涡脱落频率。支杆尾迹造成的非定常效应使叶尖区域局部总压升有所升高,在近失速工况下,总压升提高更显著。     

Cardiovascular deconditioning during weightlessness simulation and the use of lower body negative pressure as a countermeasure to orthostatic intolerance

The cardiovascular function is one of the main disturbed by weightlessness: it is particularly affected by the astronaut's return to Earth, where symptoms linked to the cardiovascular deconditioning syndrom appear in the following forms: (1) orthostatic intolerance with its risk of syncope: (2) higher submaximal oxygen consumption for an equivalent work load. Lower Body Negative Pressure (LBNP) is intended to stimulate the venous system of the lower limbs; however, the specific effects of periodical LBNP sessions on the orthostatic intolerance have never been studied. With this objective in mind, 5 volunteers took part in two recent antiorthostatic bedrest experiments for 30 days. In the first experiment 3 subjects were submitted to several sessions of LBNP experiment per day and 2 others were controls; in the second experiment the LBNP group of the 1st one became controls and vice-versa. Two orthostatic investigations were performed: (1) 5 days before the bedrest; (2) at the end of the 30 day bedrest period. The results showed: (1) when the subjects were control, a high orthostatic intolerance post bedrest with 3 syncopes and one presyncopal state during the first minutes of the tilt test; (2) when the subjects were submitted to LBNP sessions, no orthostatic intolerance.     

火箭垂直发射系统燃气流场的计算

本文报导了火箭垂直发射系统燃气流场的数值计算结果，在计算中采用二阶精度的ＭＵＳＣＬ格式。为了将三维问题转化为二维问题，对数值流量作了校正。处理了弹体运动引起的动边界，分析了计算结果，与实验测量结果比较表明，数值精度是满意的。。     

In-situ photopolarimetric measurements of dust and gas in the coma of Halley''s comet

The Halley Optical Probe Experiment (HOPE) on board the Giotto spacecraft has provided the first in-situ measurements, both of the dust and of some gaseous species, from inside the coma of the comet. The instrument has already been described /1/, together with first results /2/. The purpose of this note is to show how optical measurements can lead to in-situ information, how those were obtained during the 13–14 march 1986 Halley fly-by, and what is the status of the data analysis.     

Time variations of the total electron content in the Southeast Asian equatorial ionization anomaly for the period 2006–2011

This study presents the time variations of the total electron content in the South East Asian equatorial ionization anomaly. The time variation of the TEC is analyzed through the period 2006–2011 by using a latitudinal chain of GPS stations extending in the northern and southern hemisphere. The data shows that the shape of the diurnal variation of the TEC depends on the latitude: a plateau is observed at the stations near the equator and a Gaussian at the station distant from the equator. We observe a semiannual pattern in all the stations with maxima at equinox. In both hemispheres, the amplitude of the crest is larger in spring than autumn from 2006 to 2008 and smaller in spring than in autumn from 2009 to 2011. We also observe an asymmetry between the amplitude and the position of the two crests of ionization. There is a very high level of correlation between the amplitude of the TEC at the two crests and the sunspot number: ∼0.88. During the deep solar minimum 2008–2009, the amplitude of crests of ionization becomes small during several months in summer and winter. The results show that both crests move significantly equatorward in winter than other seasons and there is a tendency for both crests to appear earlier in winter and later in summer.