波音777飞机高升力控制系统余度管理分析

飞行控制系统普遍采用余度技术来提高自身的任务可靠性。余度部件效能的发挥程度主要取决于余度管理策略和方法。根据波音777飞机高升力控制系统的基本构架,通过在线监控与信号表决相结合的方法对系统余度管理方法进行研究。在余度管理方法的设计过程中,充分考虑了布线技术、硬件设计技术及与软件相结合的方法,不但简化了襟缝翼控制器的硬件设计,同时也简化了控制器软件的设计难度,提高了系统可靠性,所用到的方法对同类系统设计有一定的参考价值。     

Energy dependence of the rigidity spectrum of Forbush decrease of galactic cosmic ray intensity

We show that rigidity spectrum of Forbush decrease (Fd) of galactic cosmic ray (GCR) intensity in September 9–23, 2005 clearly depends on energy. We calculated rigidity spectrum of the Fd based on the neutron monitors and Nagoya muon telescope channels’ data divided in three groups according to their cut off rigidities. We found that temporal changes of rigidity spectrum exponent γ are approximately similar for all cut off rigidity groups, but γ values are the larger the higher are cut off rigidities. We conclude that rigidity spectrum of Fd is hard for lower energy range and is soft for the higher energy range. We believe that an energy dependence of the power law rigidity spectrum of Fd is observed owing to the preferential convection–diffusion mechanism during Fd in September 9–23, 2005. It is a reflection of an influence of the temporal changes of the structure of the interplanetary magnetic field (IMF) turbulence in different range of frequency f during Fd. Particularly, a decisive role in formation of the character of the rigidity spectrum belongs to the changes of the exponent ν of the power spectral density (PSD) of the IMF turbulence (PSD ∝ f^−ν). The exponent ν is greater for high frequency region of the IMF turbulence (responsible for scattering of low rigidity particles of GCR), than for low frequency region of the IMF turbulence (being responsible for scattering of higher rigidity particles). Also, we challenge to estimate an existence of slab/2D structure of solar wind turbulence during the Fd in September 9–23, 2005 based on the distribution of average turbulence energy among the IMF’s components.     

用于导弹发射装置的平衡机

简述了导弹发射装置中弹簧式和扭杆式两种平衡机的特点及制造工艺。介绍了单发、多联装、箱式和舰用型等不同导弹发射装置中平衡机的结构布局,以及各自的特点,给出了平衡机设计的一般原则。     

碳/环氧网格面板-铝蜂窝夹层结构板弯曲刚度试验研究

根据任务需要 ,对碳 /环氧网格面板 -铝蜂窝夹层结构板进行弯曲刚度性能试验 ,因目前尚无该产品试验标准 ,文章通过对试验方法的研究后 ,参考相应试验标准 ,测试了有关性能数据 ,为材料研究及产品验收提供了可靠的依据     

微机化弹条测量仪的研制

该仪器综合运用机、光、电等技术 ,在微机系统控制下 ,可在弹条一次安装下自动测量弹条的 9项几何参数 ,测量不确定度远小于被测几何参数公差的 1/ 10 ,测量一件弹条只需 4 0余秒。文中简述了仪器的结构、工作原理及专门研制的机—光—电传感器和光—电传感器的原理     

民用飞机复合材料主结构适航符合性研究

介绍了民用飞机复合材料主结构适航取证方法。该取证方法是基于试样和组合件试验支持的分析方法,符合FAA和EASA发布的指导条例。根据FAA新近发布的资讯通报AC20—107B,给出了复合材料主结构静强度、疲劳和损伤容限符合性方法需遵循的原则。最后给出了全尺寸复合材料部件静强度、疲劳和损伤容限试验流程。研究的复合材料主结构取证方法符合适航当局颁布的适航规章和咨询通报要求。     

飞机结构中柔性件装配偏差分析与控制研究进展

飞机柔性结构的装配偏差分析与控制一直是飞机装配中的难点,随着复合材料在飞机结构中的广泛应用,这一问题越发明显.采用预浸料固化工艺的复合材料零件具有制造偏差大、非主应力方向在装配过程中容易损伤等特点,对柔性件装配中的偏差分析和控制提出了更高的要求.如何合理地进行容差分配、工艺补偿、过约束装配以满足装配后的性能要求,是目前...     

Effects of splined shaft bending rigidity on cylinder tilt behaviour for high-speed electro-hydrostatic actuator pumps

High-speed axial piston pumps are hydraulic power supplies for electro-hydrostatic actuators(EHAs). The efficiency of a pump directly affects the operating performance of an EHA, and an understanding of the physical phenomena occurring in the cylinder/valve plate interface is essential to investigate energy dissipation. The effects of the splined shaft bending rigidity on the cylinder tilt behaviour in an EHA pump need to be considered, because the deflection and radial expansion of a steel shaft rotating at a high speed cannot be ignored. This paper proposes a new mathematical model to predict the cylinder tilt behaviour by establishing a quantitative relationship between the splined shaft deflection, the cylinder tilt angle, and the tilt azimuth angle. The moments exerted by the splined shaft are included in the equilibrium equation of the cylinder. The effects of solid and hollow splined shafts equipped in an EHA pump prototype are compared at variable speeds of 5000–10,000 r/min. With a weight saving of 29.7%, the hollow shaft is experimentally found to have almost no influence on the volumetric efficiency, but to reduce the mechanical efficiency by 0.6–2.4%. The results agree with the trivial differences of the simulated central gap heights of the interface between the two shafts and the enlargement of the simulated tilt angles by the hollow shaft. The findings could guide designs of the cylinder/valve plate interface and the splined shaft to improve both the efficiency and power density of an EHA pump.     

复杂薄壁零件加工的辅助刚性增强方法

刚性差是薄壁零件加工领域的一个难题,采用包裹或填充辅料提高薄壁零件刚性的方法对解决薄壁零件加工变形问题、提高工艺性、控制尺寸变化有良好的效果,是提高薄壁件加工性能的有效途径,对提高加工质量和生产效率有着积极的意义。     

航天任务控制中心容灾模式研究

航天任务是一项高投入、高风险的活动,作为管理所有在轨飞行航天器及资源的航天任务控制中心,要求具备很高的可靠性与较强的容灾能力。国际航天大国对地面系统,特别是任务中心级的备份均非常重视,也开展了相关建设和系统运行。在对我国航天任务控制中心容灾模式进行探讨的基础上,提出容灾中心的技术要素、需求分析以及运行机制。