An improved real-time cycle slip correction algorithm based on Doppler-aided signals for BDS triple-frequency measurements

Doppler, which is an instantaneous GNSS observable signal, has been proven effective in determining velocity and acceleration due to its high availability and accuracy. We propose a real-time triple-frequency cycle slip correction (CSC) method based on Doppler-aided signals because Doppler shift is time-independent and immune to cycle slips. When the sampling interval is less than 1 s, cycle slips on triple-frequency can be detected and repaired using pure Doppler data with high reliability; however, this method cannot be used when the sampling interval exceeds 1 s because the integral cumulative error of Doppler increases significantly. For such cases, a modified triple-frequency CSC approach has been developed based on the raw phase and smoothed code data that was refined using the Doppler signal. To suppress the effect of the integral Doppler error, a balance factor is introduced to adjust the contributions of the raw code and Doppler observables. After the refinement of the GNSS data, three independent combinations need be selected to detect and repair cycle slips with triple-frequency observations. Four constrained criteria have been proposed to select optimal combinations that can reduce the residual ionospheric delay (RID) and measurement noise to a low level. Finally, experiments were carried out to test the performance of the new method using real triple-frequency BDS observations (GPST: 3:15:00–5:55:00, March 23, 2018). The results show that pure Doppler can detect and repair cycle slips effectively with small intervals, and modified Hatch-Melbourne-Wübbena (HMW) method based on Doppler-aided signals can achieve 99.7% success rate in cycle slip correction with large intervals (up to 30 s).     

CICC型超导导体外壳制作工艺研究

通过焊接参数的选定(焊接电流 I=150A,电压U=8.8V,焊接速度0.7～1m/min),保证单根导体长度不小于300m,焊缝无气孔,裂纹等焊接缺陷.使焊接后的CICC超导导体内部最接近焊缝位置的温度低于183℃,确保导体导电性能,导体焊缝耐压试验不低于5MPa,且氦气密性能良好,研制出的产品满足相关技术标准的质量...     

2A14铝合金返修焊技术

根据2A14铝合金的冶金特点，针对对接接头和锁底焊缝的不同要求，提出了相应的采用缺陷槽的补焊工艺。分析了焊接位置、补焊层数及两面补焊、预热和缓冷、补焊的收／起弧及长度、电源选择、环境控制、补焊顺序和方向，以及装配等因素的影响。由不同运载贮箱补焊的结果可知，该工艺措施有效，补焊质量较好，提高了补焊的一次合格率。     

Mechanical behavior of the metal parts welded with extraterrestrial regolith simulant by the solar concentrator in ISRU & ISRF application

The use of in-situ resources plays an important role on future extraterrestrial human activities for the facility repair and habitat construction, especially in sustainable space exploration of Moon and Mars. A method of the metal welded with extraterrestrial regolith simulant using solar processing under ambient conditions is presented. Metal parts are made of Q235B ferroalloy and TA2 titanium alloy into standard tensile members according to the ASTM code. They are disconnected from the middle in advance, and then welded together with lunar and Martian regolith simulant under ambient conditions, respectively. The entire welding process and precautions are detailed. Additionally, the mechanical behavior of weldments is characterized regarding their tensile strength. Furthermore, the fusion zone of weldments is studied by Scanning electron microscopy (SEM), energy dispersive X-ray spectroscopy (EDS) and X-ray diffraction (XRD) measurements. The results show that it is possible to weld metal parts together with extraterrestrial regolith simulant by the solar concentrator. The average ultimate tensile strength of ferroalloy specimens welded with lunar and Martian regolith simulant is 2.94 MPa and 1.66 MPa; The average ultimate tensile strength of titanium alloy specimens welded with lunar and Martian regolith simulant is 4.95 MPa and 2.59 MPa. Moreover, the failure mode of all weldments was brittle failure. The welding joints strength derives from the phases that the regolith as the solder fusing into ferroalloys in a homogeneous way and titanium alloys in an inhomogeneous way. The presented method may provide a new thought for astronaut assistance associating with repairing and fabricating in subsequent Moon and Mars missions.     

振动处理对铝合金焊接结构变形与内应力的影响

铝合金的焊后延迟变形是生产中影响产品质量的重要问题，本文研究一种投资少、见效快的解决方法－振动处理。实验证明振动处理能降低铝合金焊接结构残余应力峰值，使内应力均匀化，对于控制焊接延迟变形有明显效果。振动后对焊缝组织的微观结构分析显示，振动处理降低了位错密度，因为位错密度是内应力的直接表征，因此振动处理的作用效果可以用振动前后微观结构的变化来解释。     

公路隔离网专用焊机微机控制系统研制

介绍了公路隔离网专用焊机微机控制系统的功能、系统的硬件结构和软件设计。控制系统具有手动、半自动、全自动等工作方式，可自动补偿网压波动对焊接电流的影响。批量生产应用表明：控制系统操作方便，性能可靠，焊接质量稳定。     

机务维修系统非例行维修平台的设计研究

非例行维修是航空公司机务维修方案的重要组成部分。由于非例行维修的不确定性,需要调研航空公司的业务流程和运行特点,分析具体的设计需求,开发出有效的现代化非例行维修管理平台。运用Delphi工具及Oracle数据库开发出航空公司非例行机务维修平台,以非单生命周期数据流转为核心,建立起航空公司对于非例行维修的管理平台,并介绍实现平台功能的几项关键技术。实际情况表明平台能够对航空公司的维修管理进行有效的控制,缩短维修时间,降低维修成本。     

LY12CZ铝合金随焊锤击碾压工艺规范研究

针对生产现场大尺寸LY12CZ铝合金薄板(2500mm×6000mm×2mm)的拼焊成形,采用动态随焊锤击碾压焊接新技术,有效防止了LY12CZ铝合金焊接热裂纹的产生,并基本消除了薄板焊接变形。通过调整随焊锤击工艺参数和焊接线能量,使锤击碾压行为与焊接熔池的凝固过程相匹配,从而实现了LY12CZ铝合金焊接无裂纹、小变形的目的。     

部件三维仿真模型与发动机循环参数分析的耦合方法研究

为了将基于部件三维仿真模型获取的部件工作特性耦合于发动机循环参数分析、提高整机性能预估的可信度,本文提出了改进完全耦合方法,结合核心机驱动风扇级(Core Driven Fan Stage,CDFS)三维仿真模型和变循环发动机(Variable Cycle Engine,VCE)零维仿真模型,使用迭代耦合和改进完全耦合方法建立了VCE多维度仿真模型,研究了修正因子计算方法及边界参数松弛处理方法对VCE多维度仿真模型的影响,对比了迭代耦合与改进完全耦合方法的差异。结果表明,采用改进完全耦合方法时,直接将基于部件高保真度仿真模型得到的压比和等熵效率应用于发动机循环参数分析,可避免非线性方程组线性化过程对部件高保真度仿真模型的重复调用,同时计算过程不依赖于部件通用特性图。采用优化方法计算修正因子或者对边界参数进行松弛处理均可以抑制改进完全耦合方法中迭代残差的震荡,加速收敛。改进完全耦合方法与迭代耦合方法计算结果无明显差异,且在使用优化方法计算修正因子时收敛速度基本一致。超声速巡航状态下,与VCE零维仿真模型的计算结果相比,多维度仿真模型中CDFS压比升高了2.73%,由此导致VCE推力降低了3.48%。     

粉末高温合金FGH96惯性摩擦焊接头室温CTOD测试与分析

FGH96是采用损伤容限设计思想研制的新型粉末高温合金,是满足高推比、高燃效发动机使用要求的涡轮盘、环形件和其他热端部件的理想材料。FGH96惯性摩擦焊接头的CTOD值小于母材,其断口的韧窝小于母材。母材和接头断裂路径均为穿晶断裂。