全文获取类型
收费全文 | 306篇 |
免费 | 99篇 |
国内免费 | 52篇 |
专业分类
航空 | 228篇 |
航天技术 | 68篇 |
综合类 | 30篇 |
航天 | 131篇 |
出版年
2023年 | 8篇 |
2022年 | 23篇 |
2021年 | 23篇 |
2020年 | 22篇 |
2019年 | 14篇 |
2018年 | 7篇 |
2017年 | 6篇 |
2016年 | 9篇 |
2015年 | 13篇 |
2014年 | 18篇 |
2013年 | 15篇 |
2012年 | 15篇 |
2011年 | 21篇 |
2010年 | 13篇 |
2009年 | 14篇 |
2008年 | 17篇 |
2007年 | 23篇 |
2006年 | 14篇 |
2005年 | 12篇 |
2004年 | 9篇 |
2003年 | 12篇 |
2002年 | 11篇 |
2001年 | 17篇 |
2000年 | 10篇 |
1999年 | 13篇 |
1998年 | 22篇 |
1997年 | 18篇 |
1996年 | 13篇 |
1995年 | 12篇 |
1994年 | 11篇 |
1993年 | 6篇 |
1992年 | 4篇 |
1991年 | 3篇 |
1990年 | 4篇 |
1989年 | 4篇 |
1987年 | 1篇 |
排序方式: 共有457条查询结果,搜索用时 46 毫秒
71.
72.
73.
在飞机部件装配过程中,CFRP/钛合金叠层结构的连接十分常见,而由于两种材料迥然不同的材料性能,导致制孔后存在孔径阶差,严重影响了CFRP/钛合金结构的疲劳强度。本文开展了低频轴向振动辅助钻削的正交实验,分析了低频振动辅助钻削工艺参数与切削力和切屑形态的关系以及工艺参数对CFRP/钛合金孔径阶差的影响。结果表明,由于低频振动辅助钻削刀具的周期性进给,钛合金切屑由连续长切屑变为扇形短屑,减少了对CFRP的扩孔效应,钻削区域切削热降低,平均轴向力降低;另外,振幅和进给量对孔径阶差的影响较为显著,而主轴转速的影响较小,且孔径阶差随着振幅的增大先减小后增大,随着进给量的增大而增大。通过试验验证和分析,确定面向孔径控制的最优工艺参数组合方案:主轴转速为600 r/min、进给量为0.02 mm/r、振幅为150μm。 相似文献
74.
75.
《中国航空学报》2021,34(5):27-38
Studies show that different geometries of a Variable Cycle Engine (VCE) can be adjusted during the transient stage of the engine operation to improve the engine performance. However, this improvement increases the complexity of the acceleration and deceleration control schedule. In order to resolve this problem, the Transient-state Reverse Method (TRM) is established in the present study based on the Steady-state Reverse Method (SRM) and the Virtual Power Extraction Method (VPEM). The state factors in the component-based engine performance models are replaced by variable geometry parameters to establish the TRM for a double bypass VCE. Obtained results are compared with the conventional component-based model from different aspects, including the accuracy and the convergence rate. The TRM is then employed to optimize the control schedule of a VCE. Obtained results show that the accuracy and the convergence rate of the proposed method are consistent with that of the conventional model. On the other hand, it is found that the new-model-optimized control schedules reduce the acceleration and deceleration time by 45% and 54%, respectively. Meanwhile, the surge margin of compressors, fuel–air ratio and the turbine inlet temperature maintained are within the acceptable criteria. It is concluded that the proposed TRM is a powerful method to design the acceleration and deceleration control schedule of the VCE. 相似文献
76.
《中国航空学报》2020,33(1):244-254
Vibration monitoring by virtual sensing methods has been well developed for linear time-invariant structures with limited sensors. However, few methods are proposed for Time-Varying (TV) structures which are inevitable in aerospace engineering. The core of vibration monitoring for TV structures is to describe the TV structural dynamic characteristics with accuracy and efficiency. This paper propose a new method using the Long Short-Term Memory (LSTM) networks for Continuously Variable Configuration Structures (CVCSs), which is an important subclass of TV structures. The configuration parameters are used to represent the time-varying dynamic characteristics by the “freezing” method. The relationship between TV dynamic characteristics and vibration responses is established by LSTM, and can be generalized to estimate the responses with unknown TV processes benefiting from the time translation invariance of LSTM. A numerical example and a liquid-filled pipe experiment are used to test the performance of the proposed method. The results demonstrate that the proposed method can accurately estimate the unmeasured responses for CVCSs to reveal the actual characteristics in time-domain and modal-domain. Besides, the average one-step estimation time of responses is less than the sampling interval. Thus, the proposed method is promising to on-line estimate the important responses of TV structures. 相似文献
77.
本文依据系统响应与其特征结构的关系,提出了振动控制的最优反馈特征结构配置方法,它针对结构承受的载荷,利用多目标优化理论,确定系统的理想特征结构,并文献的方法配置初始反馈,为了达到最优控制,文中建立了满足理想特征结构配置的目标函数,并且将保证最优控制的Lyapunov方程作为约束条件,使得反馈在满意的控制品质下,消耗的控制能最小。 相似文献
78.
《中国航空学报》2023,36(1):444-455
The vibration characteristics of composite vertical stabilizer skin structures play a critical role in damping effects designed for overcoming the air disturbances experienced by aircraft structural components during flight. The first-order fundamental frequencies and their corresponding damping characteristics of the vertical stabilizer skin structure tow-steered by automatic fiber placement technique were optimized with the parameterized trajectories and plies as design variables. Firstly, the vibration and damping numerical models were derived based on Kirchhoff laminate theory, the Rayleigh-Ritz method, and the Strain Energy Method. Then the optimization model was developed by adopting the self-adaptive Differential Evolution Multi-objective optimization algorithm and incorporating the solution method of Pareto Front. The constraints of this optimization model considered the experimentally obtained minimum turning radius of prepregs tow-steered in automatic fiber placement process obtained from experimental tests. Finally, the comparison of numerical simulation results was conducted for the optimized trajectories and the conventional straight trajectories under various boundary conditions, and the numerical results were partially validated through damping and frequency tests. The results indicate the vibration characteristics of the composite vertical stabilizer skin structure can be enhanced to a large extent by optimizing fiber trajectories, and the enhancement percentage is affected by the boundary conditions of the actual structure. 相似文献
79.
80.
磁悬浮控制力矩陀螺高速转子高频自激振动的抑制 总被引:3,自引:0,他引:3
磁悬浮控制力矩陀螺(CMG)中转子一阶弹性模态自激振动是影响磁悬浮高速转子系统稳定性的关键因素之一.自激振动通常可以采用陷波器(NF)进行抑制,然而引入NF或改变其参数以及转子转速的变化均会改变模态自激频率,因而难以直接准确地确定NF参数.本文提出一种仿真确定NF参数的方法,通过转子弹性模态缩减建模和模态参数确定得到准确的弹性转子动力学模型,进而采用闭环仿真优化确定NF中心频率和极点阻尼.采用该方法设计的NF有效抑制了转子的高频弹性模态自激振动,使得磁悬浮CMG转子可以稳定升速到24000r/min.实验结果验证了该方法的实用性和有效性. 相似文献