航天器横向振动试验的力限条件设计研究

航天器力限振动试验技术可以缓解振动过试验现象.在横向力限振动试验中,除了界面横向力以外,界面力矩同样是一个重要的监测和控制参量.文章介绍了力限振动试验的基本原理以及简单二自由度方法、复杂二自由度方法和半经验方法;然后基于模态有效质量概念提出了力矩限设计策略;最后,计算了某航天器有效载荷的力限条件和力矩限条件,结果显示力...     

便携式红外寻的防空导弹初制导探索

对便携式红外寻的防空导弹的初制导进行了定性研究。根据期望前置角,讨论了导弹发射出筒后的侧向力控制方案,给出了发射时下沉的补偿措施。分析了俄制针式便携式红外寻的防空导弹初制导系统的控制律并进行了讨论。     

某型机主桨助力器最大输出力的确定

本文从某型机先期方案四片桨叶旋翼风洞吹风得出的铰链力矩随方位角变化的关系曲线出发,求出铰链力矩表达式。然后利用所求出的铰链力矩表达式对某型机助力器120°布置方案进行计算,得出按此布置的主桨助力器的最大输出力,结果与先期方案给出的助力器最大输出力相符,从而验证了上述的计算分析是正确的。最后再运用上述相同的分析方法对某型机助力器90°布置方案进行计算,得出了某型机按此布置的主桨助力器的最大输出力。     

Orbital steady motions of a system of two bodies with an elastic connection

Steady motions of a pair of mass points connected by a rigid rod were studied by Abrarova and Karapetyan [1], the motions of a pair of mass points connected by an elastic spring were considered by Burov and Stepanov [2]. The present article is devoted to the existence, stability and bifurcation of the steady motions for a system composed of two bodies connected by an elastic torsional spring. Each of these bodies is a massless bar with mass points at the ends. One supposes that these bars are elastically connected and the system moves in the plane of the orbit of its mass centre. The trivial steady motions are studied (the principal axes of inertia of the system are directed as the radius-vector of the centre of inertia and as the tangent to the orbit). The non-trivial steady motions (the principal axes of inertia of the system are not directed as the radius vector or as the tangent to the orbit and the bars are not orthogonal each other) are also studied. We expose the complete study of the stability and of the bifurcation diagrams.     

二维燃油泵的设计与研究

提出一种新型的二维燃油泵，说明了其诸多优点。为研究其结构性流量脉动，利用仿真软件AMESIM建立了二维燃油泵的仿真模型进行理论研究，并进行了实验验证。通过齿轮泵与轴向柱塞泵的对比，说明了轴向柱塞泵在燃油系统应用中的优势。针对轴向柱塞泵中存在的一些不可避免的缺陷，提出了能避免这些缺陷的二维燃油泵。通过解释二维燃油泵的结构组成与工作原理，说明了二维燃油泵的优势，包括结构力平衡、工作效率高、无直接的滑动摩擦副和无结构性流量脉动等。为了解释无结构性流量脉动这一优点，进行了仿真分析与实验验证，验证了二维燃油泵具有无结构性流量脉动这一潜力。     

Hypersonic starting flow at high angle of attack

Compressible starting flow at small angle of attack(Ao A) involves small amplitude waves and time-dependent lift coefficient and has been extensively studied before. In this paper we consider hypersonic starting flow of a two-dimensional flat wing or airfoil at large angle of attack involving strong shock waves. The flow field in some typical regions near the wing is solved analytically. Simple expressions of time-dependent lift evolutions at the initial and final stages are given. Numerical simulations by compuational fluid dynamics are used to verify and complement the theoretical results. It is shown that below the wing there is a straight oblique shock(OSW) wave,a curved shock wave(CSW) and an unsteady horizontal shock wave(USW), and the latter moves perpendicularlly to the wing. The length of these three parts of waves changes with time. The pressure above OSW is larger than that above USW, while across CSW there is a significant drop of the pressure, making the force nearly constant during the initial period of time. When, however, the Mach number is very large, the force coefficient tends to a time-independent constant, proportional to the square of the sine of the angle of attack.     

滚转轴操纵灵敏度与动稳定性分析

在国军标的基础上,结合试飞实际和理论分析,深入研究了滚转模态时间常数过小的不利影响,提出了改进方法,并且结合试飞实际对该方法进行了验证。结果表明:适当调整滚转操纵灵敏度可以提高滚转模态时间常数,从而避免在横向小杆量操纵中飞机出现持续锯齿状滚转的现象,提高了飞行品质。该项研究为完善滚转轴飞行品质评价提供了有价值的参考。     

武警初级指挥院校学员人文素质的培养

武警初级指挥院校作为培养武警部队高素质人才的重要基地,由于主客观方面的原因,学员人文素质的培养一直相对较弱.要适应现代教学的发展,武警初级指挥院校必须在课程体系、课堂教学、教员职责、校园环境等多个方面采取有效措施,尽快提高学员的人文素质.     

不分离型超声椭圆振动切削力特性研究

分离型超声椭圆振动切削加工效率低的特点阻碍了超声椭圆振动切削技术的广泛应用和进一步发展.为拓展超声椭圆振动切削技术的应用领域,在分析了超声椭圆振动切削过程的基础上,深入研究了不分离型超声椭圆振动切削降低平均切深抗力的有效性机理,并在此基础上分析了速度系数和切深方向振幅对切深抗力的影响,揭示了不分离型超声椭圆振动切削逆变区及动态前角是降低平均切深抗力的主要原因,给出了速度系数对降低切削力失效的判断公式,并通过实验验证了不分离型超声椭圆振动切削具有降低切削力和提高加工过程稳定性的优势.这对于发挥超声椭圆振动切削技术优势,拓宽其应用领域具有重要的意义.     

一种机翼弯剪载荷包线近似计算方法

在机翼静强度初步设计中,为了快速准确地得到其载荷包线并用于确定翼盒结构基本参数,提出一种近似计算方法。通过比较多种重量估算方法,发现三角形分布能较好地拟合机翼重量。考虑到大型民用运输机飞行临界过载和集中载荷等特性,综合利用Schrenk升力分布和三角形重量分布,得到在飞行载荷下的一种近似计算机翼剪力和弯矩载荷包线方法。通过分析两机翼风洞试验数据得到的机翼剪力和弯矩包线,证明该近似方法是可行的。