外圆无心磨削工艺对轴承套圈成型质量的影响

为了得到取消外圆修磨的外圆无心磨削工艺对轴承套圈外圈的影响规律，本文以6202深沟球轴承套圈外圈为研究对象，通过外圆无心磨削试验，分析了取消外圆修磨后新无心外圆磨削工艺对套圈圆度、直径的影响，并利用谐波控制原理分析磨削加工中谐波对轴承套圈外圈圆度的控制。研究结果表明：新工艺可以满足6062轴承套圈的尺寸精度要求，外圆无心磨削时采用加工余量先大后小的方法，有助于改善轴承套圈的外圆圆度，缩短工艺流程，减少生产时间，提高生产效率；无心磨削可以降低轴承套圈表面低次谐波的幅值，外圆超精加工可以有效降低套圈表面高次谐波，从而达到控制圆度的目的。取消外圆修磨的新磨削工艺不但能提高产品质量，还能提升生产效率。     

On a plastic instability criterion for ultra-large radial-axial ring rolling process with four guide rolls

A dynamic mechanical model is proposed to describe the complexing actions of all the rolls on the ring during the ultra-large radial-axial ring rolling(RARR) process with four guide rolls. Based on the model, the calculation models for bending moment and normal stress at any section of the ring are deduced by force method. If the maximum section bending normal stress exceeds the yield stress of the ring materials, the ring will be distorted thus leading to the instability of the RARR process. Ac...     

Lift enhancement based on virtual aerodynamic shape using a dual synthetic jet actuator

The Dual Synthetic Jet Actuator (DSJA) is used to develop a new type of lift enhancement device based on circulation control, and to control the flow over the two-dimensional (2D) NACA0015 airfoil. The lift enhancement device is composed of a DSJA and a rounded trailing edge (Coanda surface). The two outlets of the DSJA eject two jets (Jet 1 and Jet 2). Jet 1 ejects from the upper trailing edge, which increases the circulation of airfoil with the help of the Coanda surface. Jet 2 ejects from the lower trailing edge, which acts as a virtual flap. The Reynolds number based on the airfoil chord length and free flow velocity is 250000. The results indicate that the circulation control method based on Dual Synthetic Jet (DSJ) has good performance in lift enhancement, whose control effect is closely related to momentum coefficient and reduced frequency. With the increase of the reduced frequency, the control effect of the lift enhancement is slightly reduced. As the momentum coefficient increases, the control effect becomes better. When the angle of attack is greater than 4°, the increments of lift coefficients under the control of DSJ are larger than those under the control of the steady blowing at a same momentum coefficient. The maximum lift augmentation efficiency can reach 47 when the momentum coefficient is 0.02, which is higher than the value in the case with steady blowing jet circulation control.     

基于电加热膜防冰设计方案的分流环表面换热特性试验研究

分流环表面换热特性对提升防冰设计效能至关重要。针对传统热气防冰方案中试验件与试验方案系统复杂、成本高昂等问题，本文提出了一种新型电加热膜防冰设计方案的分流环表面换热系数的试验方法。根据能量守恒定律，推导出分流环表面换热系数理论公式。试验研究了不同俯仰角、速度、液态水含量（Liqid water content,LWC）以及水滴中位体积直径（Median volumetric diameter, MVD）等对分流环表面换热特性的影响。试验结果表明：前缘区域换热系数随俯仰角先增大后降低，25°俯仰角是明显的转折点；相同喷雾条件下的前缘区域、下表面区域的平均换热系数约是干空气条件下的3倍；分流环前缘的换热系数明显大于上、下表面的换热系数。     

Pressure performance for a thin-walled ring and turbulent-jet orifice modeled elastic squeeze film damper

This paper explores an analytical model for Elastic Ring Squeeze Film Damper (ERSFD) with thin-walled ring and turbulent-jet orifices, and uncovers its Oil Film Pressure Performance (OFPP). Firstly, the ring deformation is addressed by using the Fourier series expansion approach and the orifice outflow rate is characterized with the Prandtl boundary layer theory. Secondly, applying finite difference scheme, the influence of elastic ring flexibility, orifice diameter, and attitude angle on the OFPP is analyzed. Finally, Outer chamber pressure was measured experimentally at different rotor speeds. The results indicate that the outer chamber pressure coats an individual load-carrying region and spreads symmetrically pertaining to the attitude angle. Its amplitude drops as the elastic ring flexibility decreases but boosts with the reduction of the orifice diameter. For inner chamber pressure, the orifice diameter effects a similar trend to the outer cavity, but exhibits more stable distribution regarding the attitude angle. Minimizing the elastic ring flexibility causes an increase in amplitude. The model is validated by the test results giving that the outer chamber pressure shifts synchronously and periodically with the variation of the attitude angle, while the pressure amplitude increases slightly at higher rotor speeds.     

Modelling and analysis of metal flowing behaviors in constraining ring rolling of tapered ring with thin wall and three high ribs

Tapered ring with thin wall and three high ribs(TRTWTHR), showing complicated geometry(wall thickness is less than 4 mm and rib height exceeds 20 mm), is extensively utilized to fabricate the critical structural parts of aerospace equipment such as spacecraft cabin, rocket body and fuel tank because of light weight and high carrying capacity. How to fabricate TRTWTHR with high performance is a critical problem that aerospace area needs to solve. In this work, constraining ring rolling(CRR) techn...