轻质耐高温隔热材料及成型技术

针对型号更高的热环境要求,开展新型轻质耐高温隔热材料研究。采用耐高温酚醛树脂作为基体树脂,添加纤维、功能性填料,通过预混料片材进行低压固化成型,对所制备的隔热材料试片进行密度、热性能以及力学性能等的测试。结果表明:该材料体系密度为0.6~0.9 g/cm^3,初始分解温度大于450℃,拉伸强度大于12MPa,200℃拉伸强度大于10 MPa,热导率低于0.25 W/(m·K),并可根据实际应用需求,实现对材料各方面性能的调控。所制备的隔热材料试片通过某型号风洞考核验证,采用该材料体系制备的大尺寸异形结构舱体通过力热联合试验考核,满足总体设计要求。     

增材制造异形波导管内腔的磨粒流抛光方法研究

针对磨粒流抛光异形波导管内球面欠抛的问题,通过设置仿形芯模引导磨料流经内球面,完成内球面的抛光.利用Fluent对不同仿形芯模与波导管内腔形成的流道模型进行流体仿真,对比分析等效壁面的流速、压力以及壁面剪切应力.仿真结果表明,芯模球径越大,越有利于改善内球面的加工质量.采用球径9mm的仿形芯模进行磨粒流抛光试验,波导管...     

Satellite capture as a restricted 2 + 2 body problem

A restricted 2?+?2 body problem is proposed as a possible mechanism to explain the capture of small bodies by a planet. In particular, we consider two primaries revolving in a circular mutual orbit and two small bodies of equal mass, neither of which affects the motion of the primaries. If the small bodies are temporarily captured in the Hill sphere of the smaller primary, they may get close enough to each other to exchange energy in such a way that one of them becomes permanently captured. Numerical simulations show that capture is possible for both prograde and retrograde orbits.     

非规则构件转动惯量的测定

介绍了一般（不对称）三线摆的结构原理，并根据动量矩原理推导了其微角及大角摆动周期的近似表达式，同时说明了一般三线摆的性质及优点。利用此摆可测量不规则小型物体绕指定轴的转动惯量，而且可不需要任何夹具。     

不规则地形条件下的双向抛物方程模型研究

在传统SSFT抛物方程模型基础上,针对传统算法忽略电波后向传播与散射,造成不规则地表边界条件下电波传播预测误差较大的问题,提出了可计算任意不规则地形剖面下前向和后向传播场的递归双向抛物方程模型,并给出了具体实现步骤,提高精度的同时弥补了传统算法的不足。仿真分析了双向抛物方程模型计算标准大气条件下单刃峰、双刃峰及实际地形的电波传播场分布特性,并与传统宽角抛物方程与几何绕射理论进行比较,验证了算法及模型的正确性与有效性。     

On tethered sample and mooring systems near irregular asteroids

A tethered asteroid sample and mooring system is investigated in this paper. In this system the spacecraft is moored to the surface of an irregular asteroid such as 216 Kleopatra by using a rocket-propelled anchor with a cable. The rocket-propelled anchor is a kind of space penetrator, which can inject into asteroids at high speeds generated by its own rocket engine. It can be used to explore the interior structure of asteroids, and it can also be used as a sample collector. When the sampling mission is done, the sample can be pulled back to the spacecraft with the anchor. Using this method, the spacecraft can be kept in a safe region in which it cannot be trapped by the gravitational field of the asteroid. This work is concerned with the dynamics of the tethered system near irregular asteroids. First, a shape model and gravitational field model of irregular asteroids are built. Then, the configuration and the stability of the tethered system are investigated, and the quasi-periodic motion near the equilibrium point of the tethered system is analyzed. Finally, the non-uniform density distribution of the asteroids is considered. The deployment process and the oscillation of the tethered system in the uncertain asteroid gravity field are simulated using the Monte Carlo method. The feasibility of the tethered asteroid sample and mooring system is proved.     

Inner wrinkling control in hydrodynamic deep drawing of an irregular surface part using drawbeads

Inner wrinkling phenomenon is more likely to develop during hydrodynamic deep drawing （HDD） of complicated component-forms due to the higher demand for controlling deformation sequences. Aiming at the problems in control of inner wrinkling for an irregular surface part featured with both concavity and convex, this research proposes an optimal design method of drawbead parameters to change the material flow. According to theoretical analysis of the mechanism of inner wrinkling, optimizing cavity pressure only is unreasonable to form a wrinkle-free deep-drawn part, so semi-circular drawbeads are employed. The effects of layout and height of drawbeads on forming results are discussed, and a process window is established based on evaluation indicators including the anti-wrinkle coefficient and the minimum wall thickness. Experiments are carried out to validate the process window, and the wall thickness and the wrinkle height are measured and compared with numerical findings. The results show that the anti-wrinkle ability of drawbeads weakens with increasing oblique angle and distance from the die center, while the wall thickness increases with increasing oblique angle and distance, and the inner wrinkling can be completely suppressed by drawbeads arranged in zones I and II with optimum penetration.     

Orbital maneuver strategy design based on piecewise linear optimization for spacecraft soft landing on irregular asteroids

Recently, asteroid exploration becomes an important branch of human’s deep space activities. In this paper, a piecewise linear optimal orbital maneuver strategy is designed for a spacecraft soft landing on irregular-shaped asteroids. First, the space around an irregular asteroid is converted into several grid units, and the gravitational field of the asteroid is linearly fitted in each unit. Then, the soft-landing orbital maneuver strategy design problem is formulated as a piecewise linear optimal problem, and further transferred into a family of two-point boundary value problems, which can be solved using collocation method. Finally, a corresponding algorithm is developed to obtain the piecewise linear optimal maneuver strategy, which is proved to be able to achieve the soft-landing mission well. Simulation results show that the error of the model linearization is small enough, while the calculation efficiency is remarkably improved, and the robustness of maneuver strategy is also improved.     

具有孔洞和不规则边界的网格参数化技术

针对凸组合参数化方法难以处理具有孔洞的网格模型,以及对不规则边界的网格模型参数化的边界处变形较大的问题,提出了一种新的参数化方法,首先通过拟合变分隐式曲面修补网格上的孔洞,并构造出较规则的附加边界,最后采用凸组合参数化方法进行参数化.通过曲面拟合实验表明,该方法引入的附加数据作为曲面拟合数据,最终的拟合曲面在孔洞以及边界处具有较好的光顺性,且该方法已应用于复合材料成型模具快速设计中的参数化曲面构建.     

用图像模板测量技术检测零件不规则薄圆孔的研究

针对零件的不规则薄孔,常规的方法无法对其精确测量,提出了一种基于数字图像处理的模板匹配检测方法,运用数字图像处理技术对采集的圆孔网像进行截取、降噪、分割、边缘检测等处理,再把提取出的圆与标定模饭上的标准阋进行比较,实现对不规则网孔尺寸的检测,并通过实验证明了陔方法的可行性和实用性.