全文获取类型
收费全文 | 143篇 |
免费 | 48篇 |
国内免费 | 3篇 |
出版年
2023年 | 2篇 |
2022年 | 6篇 |
2021年 | 7篇 |
2020年 | 1篇 |
2019年 | 7篇 |
2018年 | 5篇 |
2017年 | 5篇 |
2016年 | 5篇 |
2015年 | 6篇 |
2014年 | 6篇 |
2013年 | 4篇 |
2012年 | 7篇 |
2011年 | 14篇 |
2010年 | 12篇 |
2009年 | 15篇 |
2008年 | 10篇 |
2007年 | 6篇 |
2006年 | 11篇 |
2005年 | 10篇 |
2004年 | 5篇 |
2003年 | 6篇 |
2002年 | 1篇 |
2001年 | 10篇 |
2000年 | 4篇 |
1999年 | 1篇 |
1998年 | 5篇 |
1997年 | 5篇 |
1996年 | 2篇 |
1994年 | 3篇 |
1993年 | 1篇 |
1992年 | 4篇 |
1991年 | 2篇 |
1990年 | 4篇 |
1989年 | 1篇 |
1987年 | 1篇 |
排序方式: 共有194条查询结果,搜索用时 109 毫秒
51.
本文从柴油机燃油压力波的特征出发,建立ARI(Auto—Regressive Integra—ted)时序参数模型.通过对不同故障下的燃油压力波基于ARI时序参数的现代谱分析,说明ARI时序参数模型较好地揭示了燃油压力波蕴含的故障信息.通过燃油压力波的ARI时序参数构造故障诊断模式向量,根据几何距离与信息距离的测度来诊断故障,具有一定的实践意义. 相似文献
52.
53.
54.
氧气体积分数对油气爆炸特性的影响 总被引:1,自引:0,他引:1
作为燃烧和爆炸三要素之一,氧气体积分数的控制对于爆炸事故的防治具有重要意义。实验研究了氧气体积分数对汽油蒸气-空气混合物(简称油气)爆炸极限和爆炸压力的影响。结果表明:随着氧气体积分数的降低,油气爆炸下限呈一阶指数规律缓慢增大,油气爆炸上限呈线性规律迅速减小;爆炸极限范围由0.92%~3.76%缩小为1点,该爆炸极限临界点为1.22%,对应的临界氧气体积分数为11.4%;油气的最大爆炸压力和最大压力上升速率随着氧气体积分数的降低而减小,油气体积分数越大,氧气体积分数影响越显著。 相似文献
55.
舰艇滑油系统插装式减压阀的设计 总被引:1,自引:0,他引:1
介绍了为某型舰艇滑油系统而设计的控制压力低、流通能力大和稳定性好的插装式减压阀;建立了插装式减压阀的数学模型,通过Matlab仿真分析了插装式减压阀的稳态特性,并与试验测试结果进行了比较,验证了设计的结果是准确的. 相似文献
56.
针对目前市场上热气溶胶灭火装置"爆炸"及存在安全隐患,阐述了其发生原理,并提出了热气溶胶灭火装置应严格控制的一些安全性能指标和结构方式。 相似文献
57.
针对外卡压力传感器存在的测试信号重复性差、信噪比低、安装局限性大的问题,设计了一种新型卡持结构——人字形结构,并从理论上分析了该结构相对于"匚"形夹块和环形夹块的优势。实验数据表明:采用人字形卡持结构的外卡压力传感器具有测试可靠、信噪比高、通用性好的特点。 相似文献
58.
In this paper, the kerosene/air rotating detonation engines(RDE) are numerically investigated, and the emphasis is laid on the effects of total pressures and equivalence ratios on the operation characteristics of RDE including the initiation, instabilities, and propulsive performance. A hybrid MPI + OpenMP parallel computing model is applied and it is proved to be able to obtain a more effective parallel performance on high performance computing(HPC) systems. A series of cases with the total pressure of 1 MPa, 1.5 MPa, 2 MPa, and the equivalence ratio of 0.9, 1, 1.4 are simulated. On one hand, the total pressure shows a significant impact on the instabilities of rotating detonation waves. The instability phenomenon is observed in cases with low total pressure (1 MPa) and weakened with the increase of the total pressure. The total pressure has a small impact on the detonation wave velocity and the specific impulse. On the other hand, the equivalence ratio shows a negligible influence on the instabilities, while it affects the ignition process and accounts for the detonation velocity deficit. It is more difficult to initiate rotating detonation waves directly in the lean fuel operation condition. Little difference was observed in the thrust with different equivalence ratios of 0.9, 1, and 1.4. The highest specific impulse was obtained in the lean fuel cases, which is around 2700 s. The findings could provide insights into the understanding of the operation characteristics of kerosene/air RDE. 相似文献
59.
Xing-liang Wu Sen Xu Ai-min Pang Wei-guo Cao Da-bin Liu Xin-yu Zhu Fei-yang Xu Xu Wang 《防务技术》2021,17(4):1262-1268
MgH2, TiH2, and ZrH2 are three typical metal hydrides that have been gradually applied to composite explosives and propellants as additives in recent years. To evaluate ignition sensitivity and explosion severity, the Hartmann device and spherical pressure vessel were used to test ignition energy and ex-plosion pressure, respectively. The results showed that the ignition sensitivity of ZrH2, TiH2 and MgH2 gradually increased. When the concentration of MgH2 is 83.0 g/m3 in Hartmann device, the ignition energy attained a minimum of 10.0 mJ. The explosion pressure of MgH2 were 1.44 times and 1.76 times that of TiH2 and ZrH2, respectively, and the explosion pressure rising rate were 3.97 times and 9.96 times that of TiH2 and ZrH2, respectively, through the spherical pressure vessel. It indicated that the reaction reactivity and reaction rate of MgH2 were higher than that of TiH2 and ZrH2. In addition, to conduct in-depth theoretical analysis of ignition sensitivity and explosion severity, gas production and combus-tion heat per unit mass of ZrH2, TiH2 and MgH2 were tested by mercury manometer and oxygen bomb calorimetry. The experimental results revealed that MgH2 had a relatively high gas production per unit mass (5.15 mL/g), while TiH2 and ZrH2 both had a gas production of less than 2.0 mL/g. Their thermal stability gradually increased, leading to a gradual increase in ignition energy. Furthermore, compared with theoretical combustion heat, the combustion ratio of MgH2, TiH2 and ZrH2 was more than 96.0%, with combustion heat value of 29.96, 20.94 and 12.22 MJ/kg, respectively, which was consistent with the explosion pressure and explosion severity test results. 相似文献
60.
发动机汽缸压缩压力是检测发动机机密封性的重要参数.发动机密封性降低,会造成发动机经济性、动力性下降及废气排放指标恶化,因此对各缸压缩压力的检测具有重要意义.现提出一种利用曲轴瞬时转速,进行不解体检测坦克发动机汽缸压缩压力的方法.通过实车测量获得缸压及转速的特征参数,利用灰色理论模型的方法建立了发动机转速脉动与汽缸压缩压力的数学关系.试验结果表明,利用这种方法进行缸内压缩压力测量是可行的. 相似文献