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排序方式: 共有1105条查询结果,搜索用时 485 毫秒
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D. Bortoluzzi D. Vignotto A. Zambotti M. Armano H. Audley J. Baird P. Binetruy M. Born E. Castelli A. Cavalleri A. Cesarini A.M. Cruise K. Danzmann M. de Deus Silva I. Diepholz G. Dixon R. Dolesi L. Ferraioli Carlo Zanoni 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(1):504-520
LISA Pathfinder is a technology demonstrator space mission, aimed at testing key technologies for detecting gravitational waves in space. The mission is the precursor of LISA, the first space gravitational waves observatory, whose launch is scheduled for 2034. The LISA Pathfinder scientific payload includes two gravitational reference sensors (GRSs), each one containing a test mass (TM), which is the sensing body of the experiment. A mission critical task is to set each TM into a pure geodesic motion, i.e. guaranteeing an extremely low acceleration noise in the sub-Hertz frequency bandwidth. The grabbing positioning and release mechanism (GPRM), responsible for the injection of the TM into a geodesic trajectory, was widely tested on ground, with the limitations imposed by the 1-g environment. The experiments showed that the mechanism, working in its nominal conditions, is capable of releasing the TM into free-fall fulfilling the very strict constraint imposed on the TM residual velocity, in order to allow its capture on behalf of the electrostatic actuation.However, the first in-flight releases produced unexpected residual velocity components, for both the TMs. Moreover, all the residual velocity components were greater than maximum value set by the requirements. The main suspect is that unexpected contacts took place between the TM and the surroundings bodies. As a consequence, ad hoc manual release procedures had to be adopted for the few following injections performed during the nominal mission. These procedures still resulted in non compliant TM states which were captured only after impacts. However, such procedures seem not practicable for LISA, both for the limited repeatability of the system and for the unmanageable time lag of the telemetry/telecommand signals (about 4400 s). For this reason, at the end of the mission, the GPRM was deeply tested in-flight, performing a large number of releases, according to different strategies. The tests were carried out in order to understand the unexpected dynamics and limit its effects on the final injection. Some risk mitigation maneuvers have been tested aimed at minimizing the vibration of the system at the release and improving the alignment between the mechanism and the TM. However, no overall optimal release strategy to be implemented in LISA could be found, because the two GPRMs behaved differently. 相似文献
884.
对含有不同隐形损伤的40Cr焊板进行射线检测、疲劳试验和正交磁记忆信号测量,探索试件在疲劳应力作用下磁记忆信号的变化特征。试验结果表明:单一测量方式下的磁特征值不能表征焊板在疲劳循环载荷下的变化特征,所得结论存在偶然性;研究发现,可用磁场矢量梯度积分特征和磁场矢量合成梯度特征来评价焊板的疲劳损伤过程,并建立了以磁场矢量梯度特征为损伤参量的疲劳损伤模型,从而可以对含有隐形损伤焊接构件的疲劳寿命进行定量评估,为金属磁记忆技术在焊接缺陷定量评价上的进一步研究提供参考依据。 相似文献
885.
《中国航空学报》2020,33(3):771-791
Composite materials are increasingly used in the aerospace industry. To fully realise the weight saving potential along with superior mechanical properties that composites offer in safety critical applications, reliable Non-Destructive Testing (NDT) methods are required to prevent catastrophic failures. This paper will review the state of the art in the field and point to highlight the success and challenges that different NDT methods are faced to evaluate the integrity of critical aerospace composites. The focus will be on advanced certificated NDT methods for damage detection and characterization in composite laminates for use in the aircraft primary and secondary structures. 相似文献
886.
纵-扭复合超声钻削TC4钛合金振动系统设计与试验 总被引:1,自引:1,他引:0
螺旋沟槽变幅杆能够实现超声振动模式的转换,对单激励纵-扭复合振动的实现具有结构简单和操作可行的优点。基于弹性波场论对超声波在复合变幅杆中发生模式转换的原因及振动特性进行分析,并从超声波的入射角入手,分析入射角对振动模态的影响。在圆锥复合变幅杆的圆锥段开设螺旋沟槽,建立三维模型,并进行有限元仿真和试验验证,结果表明超声波入射角的改变对纵-扭复合变幅杆的扭-纵比影响显著。当入射角为46.5°和67.2°时,在变幅杆的输出端纵振模态和扭振模态发生明显的变化,实测的扭-纵比前者较后者提高约5.1倍。通过普通钻削与超声钻削实验对比,在不同的入射角条件下,超声钻削的平均钻削力均低于普通钻削力。与入射角为67.2°时对比,当入射角为46.5°时,平均钻削力降低约46%,并提高了制孔的质量,从而为模态转换的纵-扭复合变幅杆设计提供一定的理论依据。 相似文献
887.
陶瓷材料由于具有高熔点、高硬度、高耐磨性、耐氧化、良好的绝缘性等优点,使得其在航天领域得到广泛的应用。针对陶瓷材料在常规机械加工过程中易引入微裂纹等非本征缺陷和残余应力等加工缺陷,通过对陶瓷材料特性的理论分析,引入超声振动加工方法。同时,对陶瓷材料超声振动加工的机理进行了分析,对比验证了普通磨削加工和超声辅助铣磨削加工的效果。采用仿真分析了超声加工过程中工件所受的切削压力和内应力云图,并从理论的角度进行了验证,实现了陶瓷材料产品表观质量的大幅提升,其表面粗糙度达到Ra0.56μm。 相似文献
888.
利用超声波焊接技术实现大平面超薄铜箔与多股双层镀银编织铜的焊接,该技术服役于将来的中国空间站。分析了不同参数对连接力学性能的影响,利用扫描电子显微镜对典型接头界面处的微观组织特征进行了分析,并采用有限元仿真的方式对连接行为进行了仿真。结果表明:采用超声波焊接实现了薄壁铜层与镀银编织铜的焊接,焊点连接面处组织致密,无明显缺陷;焊点连接处由Ag和Cu元素组成,焊接温度远未达到熔点,为低温连接行为,其连接机理为扩散连接;在焊接能量为120 J、0.276 MPa参数下,母材拉脱力可达到90 N。 相似文献
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890.