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981.
针对某型弹用涡扇发动机结构特点,建立了一种转子-支承-机匣整机模型,对转子与机匣采用有限元梁模型,支承采用集总质量模型,引入支承松动故障模型,利用数值积分方法求解耦合系统的响应.基于机匣加速度信号,研究了对称刚度以及不对称刚度模型下松动故障的冲击特征分析.结果表明:①松动故障所引发的机匣加速度时域波形具有上下不对称性冲击特征以及频谱中出现倍频特征;②仿真计算结果与实际弹用涡扇发动机试车数据时域波形特征以及频谱特征非常一致,而且验证了不对称刚度松动故障模型更适合弹用涡扇发动机的松动故障建模.   相似文献   
982.
本文阐述了直升机综合保障工程中一项重要要素即保障设备在提高部队战斗力方面的重要意义,介绍了直升机保障设备的现状并提出了一些关于应用的建议。  相似文献   
983.
对于现代的军用飞机,都要求它们具有高的效费比。为此必须大力推行综合后勤保障,以提高军机的后勤保障的效能和降低军机寿命周期内的使用保障费用。提出要实现综合后勤保障,就应在军机的整个寿命周期内以综合后勤保障计划作为贯穿全过程的管理手段,协调军机的保障性设计和其他专业设计工作,并保证各种后勤保障资源的落实。在实现综合后勤保障的过程中,进行后勤保障分析则是必不可少的基础工作。  相似文献   
984.
本文对NH90型直升机的发动机安装形式进行剖析,并为其在直升机上的应用提供理论依据。  相似文献   
985.
With notably few exceptions, the existing satellite mission operations cannot provide the ability of schedulability prediction, including the latest satellite planning service (SPS) standard-Sensor Planning Service Interface Standard 2.0 Earth Observation Satellite Tasking Extension (EO SPS) approved by Open Geospatial Consortium (OGC). The requestor can do nothing but waiting for the results of time consuming batch scheduling. It is often too late to adjust the request when receiving scheduling failures. A supervised learning algorithm based on robust decision tree and bagging support vector machine (Bagging SVM) is proposed to solve the problem above. The Bagging SVM is applied to improve the accuracy of classification and robust decision tree is utilized to reduce the error mean and error variation. The simulations and analysis show that a prediction action can be accomplished in near real-time with high accuracy. This means the decision makers can maximize the probability of successful scheduling through changing request parameters or take action to accommodate the scheduling failures in time.  相似文献   
986.
王胜男  李运泽  周航  周国栋 《航空学报》2013,34(6):1285-1292
 基于质子膜燃料电池(PEMFC)和热驱制冷,提出一种舱外航天服冷电联储方法,根据热力学总能理论,通过能量的梯级利用和不同形式的能量联产来实现舱外航天服生命保障系统冷电联储、能源转化和环境控制一体化。对舱外航天服生命保障冷电联储系统进行了热力学分析,表明本文舱外航天服生命保障系统冷电联储方案与传统方案相比,能达到减少航天员出舱活动携带物品种类和提高能源利用率的目的。并重点对冷电联储系统储氢冷却器相关参数的选取对系统一次能源利用率及系统整体质量的影响进行分析,结果表明LaNi5和LmNi4.9Sn0.1较适合用于本文提出的舱外航天服生命保障冷电联储系统。  相似文献   
987.
《中国航空学报》2023,36(3):357-367
Flight delay prediction has attracted great interest in civil aviation community due to its significant role in airline planning, flight scheduling, airport operation, and passenger service. Flight delay is affected by numerous factors and irregularly propagates in air transportation networks owing to flight connectivity, which brings critical challenges to accurate flight delay prediction. In recent years, Graph Convolutional Networks (GCNs) have become popular in flight delay prediction due to the advantage in extracting complicated relationships. However, most of the existing GCN-based methods have failed to effectively capture the spatial–temporal information in flight delay prediction. In this paper, a Geographical and Operational Graph Convolutional Network (GOGCN) is proposed for multi-airport flight delay prediction. The GOGCN is a GCN-based spatial–temporal model that improves node feature representation ability with geographical and operational spatial–temporal interactions in a graph. Specifically, an operational aggregator is designed to extract global operational information based on the graph structure, while a geographical aggregator is developed to capture the similar nature among spatially close airports. Extensive experiments on a real-world dataset demonstrate that the proposed approach outperforms the state-of-the-art methods with a satisfying accuracy improvement.  相似文献   
988.
王华  王曦 《航空发动机》2007,33(2):38-43
基于符号微分运算对偏微分的解析解方法,提出了1种双转子涡喷发动机动态数学模型建立的方法.在给定双转子涡喷发动机稳态点数据和高、低压压气机特性线的条件下,通过符号微分运算,可获得关于该线性微分代数方程组系数的解析解,简化了发动机的建模过程.  相似文献   
989.
王华  王曦 《航空发动机》2007,33(4):43-45,35
利用符号运算,针对代数方程组求解的解析解功能和数值解功能,提出了1种对1阶被控对象和2阶被控对象模型进行PI控制器和PID控制器极点配置的设计方法,给出了相应控制器结构参数的解析解,并在算例中进行了数值仿真验证。  相似文献   
990.
Rosetta Ground Segment and Mission Operations   总被引:1,自引:0,他引:1  
At the European Space Operations Centre in Darmstadt (Germany) the activities for ground segment development and mission operations preparation for Rosetta started in 1997. Many of the characteristics of this mission were new to ESOC and have therefore required an early effort in identifying all the necessary facilities and functions. The ground segment required entirely new elements to be developed, such as the large deep-space antenna built in New Norcia (Western Australia). The long duration of the journey to the comet, of about 10 years, required an effort in the operations concept definition to reduce the cost of routine monitoring and control. The new approaches adopted for the Rosetta mission include full transfer of on-board software maintenance responsibility to the operations team, and the installation of a fully functioning spacecraft engineering model at ESOC, in support of testing and troubleshooting activities in flight, but also for training of the operations staff. Special measures have also been taken to minimise the ground contact with the spacecraft during cruise, to reduce cost, down to a typical frequency of one contact per week. The problem of maintaining knowledge and expertise in the long flight to comet Churyumov–Gerasimenko is also a major challenge for the Rosetta operations team, which has been tackled early in the mission preparation phase and evolved with the first years of flight experience.  相似文献   
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