全文获取类型
收费全文 | 251篇 |
免费 | 66篇 |
国内免费 | 32篇 |
专业分类
航空 | 231篇 |
航天技术 | 39篇 |
综合类 | 23篇 |
航天 | 56篇 |
出版年
2024年 | 1篇 |
2023年 | 5篇 |
2022年 | 8篇 |
2021年 | 12篇 |
2020年 | 22篇 |
2019年 | 17篇 |
2018年 | 15篇 |
2017年 | 13篇 |
2016年 | 15篇 |
2015年 | 20篇 |
2014年 | 22篇 |
2013年 | 14篇 |
2012年 | 15篇 |
2011年 | 16篇 |
2010年 | 11篇 |
2009年 | 10篇 |
2008年 | 11篇 |
2007年 | 19篇 |
2006年 | 10篇 |
2005年 | 10篇 |
2004年 | 6篇 |
2003年 | 11篇 |
2002年 | 8篇 |
2001年 | 11篇 |
2000年 | 9篇 |
1999年 | 12篇 |
1998年 | 5篇 |
1997年 | 7篇 |
1996年 | 2篇 |
1995年 | 4篇 |
1994年 | 2篇 |
1992年 | 1篇 |
1990年 | 2篇 |
1989年 | 1篇 |
1986年 | 2篇 |
排序方式: 共有349条查询结果,搜索用时 15 毫秒
11.
Rotating experimental investigations were carried out to study the oil sealing capability of two different floating ring seals in cold/hot state for aero-engine. High-speed Floating Ring Seal(HFRS) is a seal with the inner diameter of 83.72 mm and maximum speed of 38000 r/min, and Low-speed Floating Ring Seal(LFRS) is another seal with the inner diameter of 40.01 mm and maximum speed of 18000 r/min. In hot state, sealing air with the temperature of 371 K and oil with the temperature of 343 K was employed to model the working conditions of an aero-engine. Comparisons between floating ring seal and labyrinth seal were done to inspect the leakage performance.More attention was paid to the critical pressure ratio where the oil leakage began. Results show that the critical pressure ratio in cold state is obviously larger than that in hot state for both seals. An underlying sealing mechanism for floating ring seal is clarified by the fluid film, which closely associates with the dimensionless parameter of clearance over rotating diameter(2 c/Dr). Another fantastic phenomenon is that the leakage coefficient in hot state, not the leakage magnitude, is unexpectedly larger than that in cold state. Overall, the leakage performance of the floating ring seal is better than the labyrinth seal. 相似文献
12.
Yihua Zheng Anthony T.Y. Lui Mei-Ching Fok Brian J. Anderson Pontus C. Brandt Donald G. Mitchell 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(8):1234-1242
One essential component of magnetosphere and ionosphere coupling is the closure of the ring current through Region 2 field-aligned current (FAC). Using the Comprehensive Ring Current Model (CRCM), which includes magnetosphere and ionosphere coupling by solving the kinetic equation of ring current particles and the closure of the electric currents between the two regions, we have investigated the effects of high latitude potential, ionospheric conductivity, plasma sheet density and different magnetic field models on the development of Region 2 field-aligned currents, and the relationship between R2 FACs and the ring current. It is shown that an increase in high latitude potential, ionospheric conductivity or plasma sheet density generally results in an increase in Region 2 FACs’ intensity, but R2 FACs display different local time and latitudinal distributions for changes in each parameter due to the different mechanisms involved. Our simulation results show that the magnetic field configuration of the inner magnetosphere is also an important factor in the development of Region 2 field-aligned current. More numerical experiments and observational results are needed in further our understanding of the complex relationship of the two current systems. 相似文献
13.
It is urgent to carry out detailed research on storage performance of rubber sealing ring to get the criterion for its storage life. This paper acquires material ageing regularity by theoretical analysis and experimental confirmation. On this condition, failure mode and failure criterion of typical sealing structure is studied, and the failure mechanism is found. Thus by analyzing the stress distribution, the relationship between ageing state and sealing condition is established. Rationalization proposal is put forward and storage life of sealing ring is evaluated. The research mentionedabove has special reference to the design of sealing structures and can provide reference for prolonging their service life. 相似文献
14.
航空发动机中介机匣组件因各种故障而需修理或导致报废的现象时有发生。针对发动机中介机匣分流环裂纹掉块、上部衬套磨损松动、弹性环磨损、同心度检测不合格等故障进行分析研究,提出解决措施,制定满足发动机使用要求的合理技术标准和修理方法。在修理技术方法中,采用挖补补焊方法解决分流环裂纹掉块故障;采用极坐标定位与专用模板衬套相结合的方法提高新品衬套加工精度以解决上部衬套更换新品后装配准确性难题;采用装配过盈销钉和扩口工艺以保证零件的堵孔质量等。结果表明:这些修理措施提高了中介机匣零部件的利用率,延长了其使用寿命,降低了发动机修理成本。 相似文献
15.
某型号节流圈,其结构特点是壁薄,壁厚仅2.5mm,轴向尺寸小,精度高,刚性差;加工难点为装夹时容易变形,尺寸精度难以保证。通过设计、制作专用夹具,优化加工参数,解决了这一加工难题。这样既保证了产品质量,降低了加工难度又显著提高了生产效率。 相似文献
16.
在生产中大直径薄壁结构齿圈加工变形是经常遇到的问题。本文以某产品齿圈制齿后出现严重锥度变形问题为例,分析引起变形的原因,通过反复实验,找到了避免变形的有效措施。 相似文献
17.
李安 《南昌航空工业学院学报》2001,15(2):44-48
心电信号的数据采集是体表标测系统中关键技术之一。文中提出了128通道高性能体表标测系统中心电信号数据采集的VxD算法,在Wind9x系统下利用VxD技术、锁定内存和临界资源互斥访问算法相结合,实现了心电数据高速实时采集。该软件充分利用了硬件的等待时间,具有实时性高,运行速度快占内存少的特点。该软件在VtoolsD开发平台上用VisualC++开发。 相似文献
18.
19.
20.
某型飞机起落架作动筒发生漏油故障,分解后发现作动筒橡胶密封圈断裂,直接影响了飞行安全。通过对断裂的密封圈断口及表面进行观察和硬度测定,分析密封圈的失效性质及断裂产生的原因,确定了橡胶密封圈失效模式,并提出了纠正措施。 相似文献