排序方式: 共有12条查询结果,搜索用时 218 毫秒
1.
介绍了稳定裕度试飞流程和稳定裕度实时数据处理软件的设计思路,讨论了稳定裕度实时数据处理系统的数据流程和如何建立飞行试验数据库,最后给出了系统经过试飞验证后的几点结论。 相似文献
2.
研究了新型TMC-2复合材料的叶片小余量锻造工艺。结果表明,采用小余量锻造工艺研制的叶片锻件组织均匀,金属变形流线分布合理,因而,叶片的疲劳性能和抗腐蚀能力得到提高,同时,使用寿命得以延长。采用TMC-2复合材料研制的小余量叶片,在高温下具有优良的蠕变和热稳定性能。 相似文献
3.
雷变宁 《西安航空技术高等专科学校学报》2011,29(1):31-33
介绍现代飞机维修理念,分析国内飞机维修工作的基本情况,结合国际上飞机维修理念及其发展趋势,针对自身条件和生产现状,提出目前国内飞机应用的维修策略及方法。 相似文献
4.
刀具半径补偿功能在数控加工中的一种应用 总被引:2,自引:0,他引:2
焦满囤 《华北航天工业学院学报》2002,12(3):1-2
介绍了在数控机床中使用刀具半径补偿功能(G41、G42),实现利用同一段数控程序完成对余量较大的工件进行多次走刀加工的方法。 相似文献
5.
《中国航空学报》2020,33(12):3495-3508
Deformation resulting from residual stress has been a significant issue in machining. As allowance allocation can directly impact the residual stress on part deformation, it is essential for deformation control. However, it is difficult to adjust allowance allocation by traditional simulation methods based on residual stress, as the residual stress cannot be accurately measured or predicted, and many unexpected factors during machining process cannot be simulated accurately. Different from traditional methods, this paper proposes an allowance allocation method based on dynamic approximation via online inspection data for deformation control of structural parts. An Autoregressive Integrated Moving Average (ARIMA) model for dynamic allowance allocation is established so as to approach the minimum deformation, which is based on the in-process deformation inspection data during the alternative machining process of upside and downside. The effectiveness of the method is verified both by simulation cases and real machining experiments of aircraft structural parts, and the results show that part deformation can be significantly reduced. 相似文献
6.
7.
离心式恒加速度试验系统基本参数研究 总被引:1,自引:0,他引:1
通过对离心机加速度方向、加速度数值、速度波纹、加速度梯度等基本参数特性的分析,得出离心机设计、使用及测量等方面的有效方法.以常见的2种100 kg转臂式恒加速度离心试验机SY31-100型与SY31-100A型为例进行比较,分析试品在某一设定加速度试验时,不同的点可能承受的最大和最小加速度,得出减少试验样品上各点试验加速度误差的处理方式. 相似文献
8.
为研究汽蚀管在火箭发动机供应系统中的自激振荡特性,采用全尺寸的发动机泵后供应系统,并模拟供应系统在发动机中的边界条件,开展了汽蚀管动态液流试验。在不同的汽蚀管相对压力损失下,获得了不同位置处的压力振荡数据。试验结果表明,当汽蚀管处于汽蚀工作状态,汽蚀管下游脉动压力存在220~310 Hz范围的振荡,下游压力的自激振荡对汽蚀管上游系统无明显影响。随着汽蚀管相对压力损失的增大,汽蚀管下游的汽蚀振荡频率减小,汽蚀振荡幅值增大。在汽蚀管与主阀之间,振荡幅值沿流向逐步增大,从主阀至推力室头腔,振荡幅值逐步衰减。当汽蚀裕度过大时,汽蚀管下游出现大幅值的压力脉冲尖峰,并导致导管结构产生高幅值的脉冲形振动响应。 相似文献
9.
《中国航空学报》2020,33(9):2434-2444
Owing to reliability and high strength-to-weight ratio, large thin-walled components are widely used in the aviation and aerospace industry. Due to the complex features and sequence involved in the machining process of large thin-walled components, machining deformation of component is easy to exceed the specification. In order to address the problem, it is important to retain the appropriate finishing allowance. To find the overall machining deformation, finishing allowance-induced deformation (web finishing allowance, sidewall finishing allowance) and initial residual stress-induced deformation were considered as major factors. Meanwhile, machined surface residual stress-induced deformation, clamping stress-induced deformation, thermal deformation, gravity-induced deformation and inertial force-induced deformation were neglected in the optimization model. Six-peak Gaussian function was introduced to fit the initial residual stress. Based upon the obtained function of initial residual stress, a deformation prediction model between initial residual stress and finishing allowance was established to attain the finishing allowance-induced deformation. In addition, linear programming optimization model based on the simplex algorithm was developed to optimize the overall machining deformation. Results have concluded that the overall machining deformation reached the minimum value when sidewall finishing allowance and web finishing allowance varied between 1 and 2 mm. Additionally, web finishing allowance-induced deformation and sidewall finishing allowance-induced deformation were 1.05 mm and 0.7 mm. Furthermore, the machining deformation decreased to 0.3–0.38 mm with the application of optimized finishing allowance allocation strategy, which made 39–56% reduction of the overall machining deformation compared to that in conventional method. 相似文献
10.
陈杰 《郑州航空工业管理学院学报(管理科学版)》2004,22(3):41-43
文章不仅首次系统完整地提出了适用于任意条件的存货跌价准备的抵销方法,还首次提出并验证了存货跌价准备的两种抵销方法即分析抵销法和综合抵销法. 相似文献