积冰对飞机纵向操稳特性的量化影响

提出了一种根据气象条件、飞机特征、飞行条件预测积冰对飞机飞行动力学特性影响的估算方法.采用热力学平衡分析方法完成了积冰增长过程的数学描述,利用逐步线性回归方法建立了结冰飞机的气动模型,计算得到了结冰飞机的气动参数,计算结果与试验结果吻合较好,表明这种方法具有一定的工程实用性.并在此基础上研究了不同部位积冰对飞机纵向操稳特性的影响,通过数值仿真计算得出,结冰飞机气动特性的急剧恶化会导致其纵向操稳特性显著降低,严重时会危及其飞行安全.      

提高金工实习教学质量之我见

结合多年实习教学经验,从调动学生学习积极性、采用创新教学模式、改进教学手段和方法以及加强实习管理与严格执行考核标准四个方面就如何提高金工实习教学质量进行探讨。     

概要工艺设计中的综合工艺能力估算方法

从估算工艺系统的输入性能即工艺要素能力出发,构造了一种具有工艺能力一般性质的工艺要素能力的通用量化函数,提出了一种度量整体工艺质量的指标——综合工艺能力指数及其估算函数,为在概要工艺设计阶段评估和优选工艺方案提供了有效手段.      

置信检验理论

本文提出了母体特征值置信分布的概念,建立了置信检验理论,该理论包括强检验、弱检验和弱强检验三种检验方法,分别满足了不同工程检验的需求。与假设检验相比,置信检验依据的是"大概率原则",而显著性假设检验依据的是"小概率原则",因此,置信检验能够以高概率确认工程中所关心的"条件"是否成立(如产品合格与否),能够对产品质量进行高精度的检验和控制,克服了显著性假设检验仅仅是一种拒绝检验,当接受一个假设时也只是意味着不拒绝该假设的缺点。置信检验不但能够大大提高工程检验精度,而且更加便于工程应用。      

微粒子喷丸技术研究进展

微粒子喷丸因其采用的弹丸介质尺寸小,具有强化基体表面并降低表面粗糙度的优点,已成为航空、能源动力等领域中一项重要的表面强化技术.目前对于该技术的研究仍处于对其强化机理的试验论证阶段,还未有完整的理论体系.对微粒子喷丸技术的原理和特点进行了综述,讨论了微粒子喷丸的强化机制,阐述了目前微粒子喷丸技术的研究现状及在各类材料中...     

Time delay compensation in lateral-directional flight control systems at high angles of attack

The previous studies of time delay compensation in flight control systems are all based on the conventional aerodynamic derivative model and conducted in longitudinal motions at low angles of attack. In this investigation, the effects of time delay on the lateral-directional stability augmentation system in high-α regime are discussed based on the $\dot{\beta }$ model, which is proposed in our previous work and proved as a more accurate aerodynamic model to reveal the lateral-directional unsteady aerodynamic characteristics at high angles of attack. Both the $\dot{\beta }$ model and the quasi-steady model are used for simulating the effects of time delay on the flying qualities in high-α maneuvers. The comparison between the simulation results shows that the flying qualities are much more sensitive to the mismatch of feedback gains than the state errors caused by time delay. Then a typical adaptive controller based on the conventional dynamic derivative model and a gain-prediction compensator based on $\dot{\beta }$ model are designed to address the time delay in different maneuvers. The simulation results show that the gain-prediction compensator is much simpler and more efficient at high angles of attack. Finally, the gain-prediction compensator is combined with a linearized $\dot{\beta }$ model reference adaptive controller to compensate the adverse effects of very large time delay, which exhibits excellent performance when addressing the extreme conditions at high angles of attack.     

Investigation on surface roughness,residual stress and fatigue property of milling in-situ TiB2/7050Al metal matrix composites

For higher efficiency and precision manufacturing, more and more attentions are focused on the surface roughness and residual stress of machined parts to obtain a good fatigue life. At present, the in-situ TiB₂/7050Al metal matrix composites are widely researched due to its attractive properties such as low density, good wear resistance and improved strength. It is of great significance to investigate the machined surface roughness, residual stress and fatigue life for higher efficiency and precision manufacturing of this new kind material. In this study, the surface roughness including two-dimensional and three-dimensional roughness, residual stress and fatigue life of milling in-situ TiB₂/7050Al metal matrix composites were analyzed. It was found from comparative investigation that the three-dimensional surface roughness would be more appropriate to represent the machined surface profile of milling particle reinforced metal matrix composites. The cutting temperature played a great role on the residual stress. However, the effect of increasing cutting force could slow down the transformation from compressive stress to tensile stress under 270 °C. An exponential relationship between three-dimensional roughness and fatigue life was established and the main fracture mechanism was brittle fracture with observation of obvious shellfish veins, river pattern veins and wave shaped veins in fracture surface.     

基于枝切截断的高质量相位解缠算法

针对传统枝切截断相位解缠算法受残差检测理论缺陷的影响,不能实现对相位完全正确解缠,在总结枝切截断法和质量图导向法的基础上,提出一种新的相位解缠算法。在残差检测理论的基础上,使用一种新的表征相位质量的可靠性导向图指导放置枝切阻断线,对低质量相位的界定使用一种自适应阈值的方法使残差检测达到最优,提高了相位解缠的质量。对于一些背景噪声严重的情况,调制度预处理的方法提高了相位解缠的鲁棒性。实验结果表明,该算法能自动避开相位不连续区域,得到较高质量的相位解缠结果。     

基于PDCA的EWIS设计质量提升研究与应用

为了全面提升军用飞机线束及线束敷设设计质量,从设计源头根本性改善外场线路问题,从系统设计的角度出发,开展了EWIS (电气线路互联系统)设计质量控制的新流程、新方法和新技术的研究和应用。根据设计质量问题和改进需求分析结果,提出了基于PDCA (质量环)的质量控制方法,并将其应用到实践中,完善了EWIS技术文件体系,形成了EWIS精细化设计及检查验证流程,提高了设计要求的提出、实现、验证和持续完善能力,在此基础上优化了对重量特性的控制过程,极大提高了设计质量和效率,对提升飞机EWIS设计质量具有参考意义。     

Effect of curing condition on bonding quality of scarf-repaired composite laminates

Both single-face vacuum bag curing(SVC) and double-face vacuum bag curing(DVC)can be used in scarf repair of composite structures. But different curing conditions caused by the sealing state may affect the bonding quality of scarf-repaired structures. In this paper, the effect of curing condition on bonding quality of scarf-repaired laminates was experimentally investigated in terms of surface profiles, moisture absorption curves and section profiles. In order to further explore the moisture abs...