排序方式: 共有55条查询结果,搜索用时 31 毫秒
41.
Effects of RRA Treatments on Microstructures and Properties of a New High-strength Aluminum-Lithium Alloy-2A97 总被引:1,自引:0,他引:1
YUAN Zhi-shan LU Zheng XIE You-hua DAI Sheng-long LIU Chang-sheng 《中国航空学报》2007,20(2):187-192
A new high strength 2A97 Al-Cu-Li-X alloy was subjected to triple-aging of retrogression and re-aging treatments (RRA). Transmission electron microscopy (TEM), differential scanning calorimetry (DSC), and tensile tests were used to investigate the effects of RRA treatment on the microstructures and properties. DSC test reveals the reversion temperature range of the strengthening δ' (Al3Li)phase. The results show that the microstructure consists of δ' (Al3Li) phase, T1 (Al2CuLi) phase and θ"/θ'(Al2Cu) phase for 2A97 alloy treated by a triple-aging ora retrogression and re-aging treatment in the following order: (1) at 165 ℃×30 min, (2) at 220 ℃ or 240 ℃×15 min, (3) at 165 ℃×24 h. The plastic deformation, incorporated into the treatment after secondary high temperature aging, promotes the T1 precipitation during final re-aging. The tensile properties of the alloy treated by the retrogression and re-aging treatment reach the peak level of alloy single-aged at 165 ℃ in T6 temper. 相似文献
42.
飞机扭转敏捷性与飞行品质关系研究 总被引:1,自引:0,他引:1
借鉴模拟或试飞获得飞机绕飞行速度滚转且截获 90°倾斜角所需时间 TRC90 的技术,设计数字仿真用的飞机扭转敏捷性机动动作及其相应的舵面操纵规律。具体计算某机不同 H,Ma和 ny 下的 TRC90 和 TA尺度,以及定常水平盘旋飞行时的模态特性。讨论和分析飞机扭转敏捷性指标与飞行品质之间的关系 相似文献
43.
44.
45.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(4):1210-1224
This work develops an autonomous trajectory planning algorithm for 6-DOF asteroid landing. The trajectory planning problem is formulated as a nonconvex time-optimal optimization problem with two-phase free final time, while the cost is regularized by augmenting a fuel consumption penalty. The nonconvex optimization problem is solved in successive solution method, and successive convexification is used to convert the original nonconvex problem into a sequence of convex subproblems, where each subproblem is obtained by linearizing the nonconvex dynamics and state constraints and using the velocity increment to give a convex expression of the fuel consumption penalty in cost function. Specifically, in the linearization, we divide the flight time interval into two parts and normalize each part using a time dilation coefficient to solve the problem that both the final times for the two flight phases are unknown, so that the original free final time problem turns to a fixed-time problem by minimizing the sum of the two time dilation coefficients and fuel consumption penalty. Besides, trust regions and virtual control are used to increase robustness of the algorithm. A convergence analysis is presented which indicates the successive solution will recover the local optimality of the original problem. Then the validity of the proposed algorithm and effects of different factors on flight time and fuel consumption are examined by simulations of landing on an irregular asteroid. 相似文献
46.
47.
船用发电机的转子绕组因通过电压低、电流小、结构比定子简单等原因,在日常电机制造及检验过程中,匝间绝缘的监测容易忽视,而且IEC 60034以及IEC 60092等国际电工委员会颁布的标准中也没有对此提出明确要求。但是, 基于对产品质量及性能的可靠性保障,转子匝间耐压测试是有必要的,特别对高压电机产品的转子匝间绝缘监测,以验证匝间绝缘对陡峭前沿的操作过电压的承受能力。以制造厂进行的高压发电机转子匝间试验为例,介绍了测试方法、故障现象及异常分析三部分内容,包含了以脉冲波形判断发电机转子部分的绝缘异常,以及制造过程中接地电阻的问题。 相似文献
48.
针对IE4电机开发过程中采用不等匝绕组设计存在的问题,在原三相异步电动机电磁设计软件V2.0版的基础上,开发了能够采用不等匝绕组进行设计计算的新版本软件MEMC V3.0。通过MEMC V3.0在YE4系列、YZTE4系列电机设计中应用。结果表明取得了预期效果。 相似文献
49.
50.