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841.
基于Fokker F27机群载荷谱损伤分散性计算分析 总被引:3,自引:2,他引:1
为考虑机群载荷谱分散性进行机群可靠性寿命评估,以56架Fokker F27飞机每次飞行的载荷因子-超越数曲线族为基础,编制得到56架飞机的载荷谱,选取SWT公式和线性累积损伤理论计算得到每架飞机的飞行载荷损伤、地-空-地载荷损伤和每次飞行载荷损伤,采用概率坐标回归方法进行拟合优度检验.结果表明,飞行载荷损伤服从威布尔分布、地-空-地载荷损伤服从对数正态分布,综合飞行载荷和地-空-地载荷损伤的每次飞行损伤服从对数正态分布,每次飞行损伤的对数标准差为0.073 7. 相似文献
842.
针对高速转子柔片式密封系统,建立了密封区域流场的数学模型,采用一种修正的压力耦合方程组的半隐式方法(Semi-Implicit Method for Pressure-Linked Equations Revised, SIMPLER)算法和有限差分法对数学模型进行数值求解,构建了柔片式密封性能分析程序,得到密封系统的压力场分布、速度场分布及泄漏量等,研究了不同结构参数和工况参数对密封性能的影响.分析结果表明:泄漏量随密封压差的增大呈线性增长趋势,而随转子转速的增大略有减小;增加柔片宽度、减小柔片长度、减小前/背板-转子间距均对降低密封系统的泄漏量有益,而柔片安装角度的变化则对密封系统的泄漏量影响不明显.基于流场的结果,柔片和转子的动力学响应将被研究. 相似文献
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846.
煤油/空气三管气动阀式脉冲爆震发动机 总被引:3,自引:0,他引:3
在煤油/空气单管气动阀式脉冲爆震发动机(PDE)研究基础上,建立了煤油/空气三管气动阀式PDE实验系统。在进气加温的条件下,以煤油为燃料,低污染空气为氧化剂,在内径为100 mm、长为2 000 mm的3个爆震管组成的三管气动阀式PDE中进行了多循环爆震实验,成功实现总工作频率30 Hz情况下,保证三管正常时序工作,在每个爆震管中均获得稳定发展的Chapman Jouguet(CJ)爆震波,研究了共用进气道对爆震室充填混气的影响和不同工作频率下三管气动阀式PDE的爆震波压力特性。研究结果为进一步研究多管PDE提供了基础,为探索脉冲爆震 涡扇组合发动机(PDTE)的可行性提供了初步的理论依据。 相似文献
847.
电磁探测卫星自治(AEDS)是一类对地观测卫星,其搜集的信息对工业、科研和军事等领域有着重要的意义。针对电磁探测卫星有效载荷特点,建立了基于动态拓扑结构无环路有向图的星上自主规划数学模型,提出了基于标记更新最短路径搜索的星上自主规划精确算法,对其完备性和时间复杂度进行了分析。并对精确算法时间复杂度较高的缺点,将近似支配概念引入到模型中,提出了标记更新最短路径搜索近似算法,分析了算法的近似程度和时间复杂度。最后,根据模拟的数据进行实验及分析,表明该方法能有效解决电磁探测卫星自主任务规划问题。 相似文献
848.
Yongkang Tang Shuangsheng Guo Wenping Dong Lifeng Qin Weidang Ai Shan Lin 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
The objectives of this research were to determine photosynthesis, evapotranspiration and growth of lettuce at long-term low atmospheric pressure. Lettuce (Lactuca sativa L. cv. Youmaicai) plants were grown at 40 kPa total pressure (8.4 kPa pO2) or 101 kPa total pressure (20.9 kPa pO2) from seed to harvest for 35 days. Germination rate of lettuce seeds decreased by 7.6% at low pressure, although this was not significant. There was no significant difference in crop photosynthetic rate between hypobaria and ambient pressure during the 35-day study. The crop evapotranspiration rate was significantly lower at low pressure than that at ambient pressure from 20 to 30 days after planting (DAP), but it had no significant difference before 20 DAP or after 30 DAP. The growth cycle of lettuce plants at low pressure was delayed. At low pressure, lettuce leaves were curly at the seedling stage and this disappeared gradually as the plants grew. Ambient lettuce plants were yellow and had an epinastic growth at harvest. The shoot height, leaf number, leaf length and shoot/root ratio were lower at low pressure than those at ambient pressure, while leaf area and root growth increased. Total biomass of lettuce plants grown at two pressures had no significant difference. Ethylene production at low pressure decreased significantly by 38.8% compared with ambient pressure. There was no significant difference in microelements, nutritional phytochemicals and nitrate concentrations at the two treatments. This research shows that lettuce can be grown at long-term low pressure (40 kPa) without significant adverse effects on seed germination, gas exchange and plant growth. Furthermore, ethylene release was reduced in hypobaria. 相似文献
849.
Yunan Yang Liman Tang Ling Tong Yang Liu Hong Liu Xiaomin Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2010
Silkworm could be an alternative to provide edible animal protein in Controlled Ecological Life Support System (CELSS) for long-term manned space missions. Silkworms can consume non-edible plant residue and convert plant nutrients to high quality edible animal protein for astronauts. The preliminary investigation of silkworm culture was carried out in earth environment. The silkworms were fed with artificial silkworm diet and the leaves of stem lettuce (Lactuca sativa L. var. angustana Irish) separately and the nutritional structure of silkworm was investigated and compared, The culture experiments showed that: (1) Stem lettuce leaves could be used as food of silkworm. The protein content of silkworm fed with lettuce leaves can reach 70% of dry mass. (2) The protein content of silkworm powder produced by the fifth instar silkworm larvae was 70%, which was similar to the protein content of silkworm pupae. The powder of the fifth instar silkworm larvae can be utilized by astronaut. (3) The biotransformation rate of silkworm larvae between the third instar and the fifth instar could reach above 70%. The biotransformation cycle of silkworm was determined as 24 days. (4) Using the stem lettuce leaves to raise silkworm, the coarse fiber content of silkworm excrements reached about 33%. The requirements of space silkworm culture equipment, feeding approaches and feeding conditions were also preliminarily designed and calculated. It is estimated that 2.2 m3 of culture space could satisfy daily animal protein demand for seven astronauts. 相似文献
850.
考虑日月引力对卫星轨道的扰动影响,分析了大椭圆轨道(HEO)倾角漂移规律,推导了小倾角HEO轨道的倾角长期漂移解析公式。结合HEO轨道倾角保持要求,给出了相应倾角控制策略。以STK为比较验证软件平台,经仿真分析与比较可知:文中推导的小倾角HEO轨道的轨道倾角解析公式较STK计算偏差在5%以内,验证了解析公式正确性;基于推导的倾角长期漂移解析公式,进行了倾角控制仿真,仿真结果表明了控制策略的有效性,并同时体现了倾角长期漂移解析计算公式在工程中的作用。 相似文献