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581.
582.
本文进行了间接性选区激光烧结铁粉成型粉末的实验,结果表明以环氧树脂作为粘结剂的铁粉成型粉末制备简单、成型性好、成本低,并对工艺参数进行了优化。用此种材料在优化的工艺参数下制作出了复杂的三维零件且误差稳定在 0.3 mm左右。 相似文献
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584.
为了研究激光冲击强化(LSP)后加力燃烧室火焰探测器焊缝位置异常开裂原因,采用X射线衍射方法和金相方法对激光冲击强化效果进行分析,并利用扫描电子显微镜对断口进行了观察。在Abaqus有限元分析软件中建立了与观察到的焊缝缺陷相似的有限元模型,对焊缝缺陷的LSP处理及冲击波传播过程进行了模拟分析。试验结果表明:具有较好材料完整性的区域经LSP处理后,表面会预置较大残余压应力,同时表面金属晶粒得到细化,疲劳裂纹会在焊缝缺陷位置萌生和扩展。有限元分析结果表明:存在分层缺陷的焊缝经LSP强化后,冲击波会在分层缺陷处产生反射,造成分层位置发生开裂,形成裂纹源造成疲劳开裂。根据试验和仿真分析结果,为提升火焰探测器焊缝激光冲击抗疲劳效果,建议优化焊接工艺,提高焊接质量。 相似文献
585.
钣金件快速精确加工中的激光切割工艺分析 总被引:2,自引:1,他引:1
针对δ0.5mm~δ6mm钣金件的结构特点,通过比较常用加工工艺和激光切割过程工艺.选出适合实际的优化方案。验证了不同切割参数对切割质量的影响。在工艺参数为:脉冲功率2.4kW、脉冲宽度约10ms、功率密度10^7W/cm^2的情况下,激光切割δ0.5mm~δ6mm钣金件获得了良好的切割质量,尺寸精度控制在误差(±100μm)范围内。工艺方案合理,生产率高。 相似文献
586.
《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(5):1333-1343
This paper investigates the motion control system of an optical telescope system used for precision satellite tracking and ranging applications. The system uses direct-drive permanent magnet synchronous motors (PMSMs) for high precision positioning. To overcome the performance limitations due to system dynamics and position dependent plant variations, a disturbance observer based control system is utilized. This paper contributes the detailed analysis, design and implementation of such an advanced control concept for the performance improvement of precision satellite tracking systems. Satellite tracking experiments are conducted to verify the performance of the proposed system. Utilizing the proposed control concept, the RMS servo error is reduced by a factor of 3.8 to well below the arcsecond range, achieving seeing limited tracking. 相似文献
587.
潜艇只在必要时刻才浮出水面,对实时通信和导航定位造成极大制约。蓝绿激光具有深水穿透性高、衰减系数低等优势,已在机载和星载平台对潜艇通信中得到验证。借鉴GNSS导航信号产生原理,结合蓝绿激光通信测距一体化与低轨卫星自身精密定轨,提出了基于蓝绿激光通信的低轨卫星对潜定位算法。通过在激光通信中增加载波相位调制,实现潜艇激光接收器的伪距测量,联合其高程测量信息实现水下定位。以一带一路海域,特别是中国南海区域为服务对象,优化星座参数设计了3颗卫星组成的低轨稀疏星座。潜艇在星座覆盖区域内保持静态,间隔1~3min完成至少两次通信测距和导航电文接收,联合两组观测数据、精密星历及高程测量信息进行定位解算。仿真结果显示,在卫星过境期间,考虑卫星定轨精度,激光在空气、水下传播误差等因素,潜艇可在水下实现X、Z方向定位误差优于100m,Y方向误差约100~150m的高精度定位,对提升潜艇的战场作战能力具有意义。 相似文献
588.
Ernst Schrama 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(1):235-247
In this paper we discuss our efforts to perform precision orbit determination (POD) of CryoSat-2 which depends on Doppler and satellite laser ranging tracking data. A dynamic orbit model is set-up and the residuals between the model and the tracking data is evaluated. The average r.m.s. of the 10?s averaged Doppler tracking pass residuals is approximately 0.39?mm/s; and the average of the laser tracking pass residuals becomes 1.42?cm. There are a number of other tests to verify the quality of the orbit solution, we compare our computed orbits against three independent external trajectories provided by the CNES. The CNES products are part of the CryoSat-2 products distributed by ESA. The radial differences of our solution relative to the CNES precision orbits shows an average r.m.s. of 1.25?cm between Jun-2010 and Apr-2017. The SIRAL altimeter crossover difference statistics demonstrate that the quality of our orbit solution is comparable to that of the POE solution computed by the CNES. In this paper we will discuss three important changes in our POD activities that have brought the orbit performance to this level. The improvements concern the way we implement temporal gravity accelerations observed by GRACE; the implementation of ITRF2014 coordinates and velocities for the DORIS beacons and the SLR tracking sites. We also discuss an adjustment of the SLR retroreflector position within the satellite reference frame. An unexpected result is that we find a systematic difference between the median of the 10 s Doppler tracking residuals which displays a statistically significant pattern in the South Atlantic Anomaly (SSA) area where the median of the velocity residuals varies in the range of ?0.15 to +0.15?mm/s. 相似文献
589.
《中国航空学报》2021,34(4):375-386
Laser welding of dissimilar titanium/aluminum alloys has been employed at an increasing rate, particularly in the aerospace industry, owing to its advantages in terms of current design flexibility and fuel/cost savings. The major problem with dissimilar Ti/Al welds arises from the difference in the thermal expansion and contraction of the two metals, which leads to hot-cracking susceptibility and the mitigation of the mechanical property after welding. In the present study, pulsed Nd:YAG laser welding of Ti6Al4V and AA6060 has been addressed. Hot-cracking susceptibility in the heat affected zone and the shear fracture behavior of the lap joints were investigated through microstructural characterization and mechanical tests. The results indicate that the hot cracking tendency can be reduced by increasing the pulse peak power (7.5–8.5 kW) and the laser point diameter (0.8–1.0 mm) with specific pulse duration and overlap. An alternative control strategy for less hot cracks in the Ti/Al lap joint can be to increase the weld width and decrease the cooling rate during solidification. The shear fracture of the Ti/Al lap joint is likely to occur along the lower side path of the weld interface with decreasing weld surface collapsed amount and increasing aluminum base metal melt depth. 相似文献
590.