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叶型中弧线的最大弯度位置对跨音速压气机叶片性能影响的研究 被引量:4
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作者 陈乃兴 张宏武 +1 位作者 徐燕骥 黄伟光 《工程热物理学报》 EI CAS CSCD 北大核心 2005年第3期409-412,共4页
本文研究与分析了叶型中弧线的最大弯度位置对跨音速压气机叶片气动性能的影响。采取了注重流动机理的优化方法,对本文算例的风扇叶片进行了优化,改进后所得的叶片的效率比原设计有了较大的提高。
关键词 跨音速压气机气动设计 叶型中弧线最大弯度位置 叶片优化设计
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一种“大弯度”横梁冲压工艺及模具结构
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作者 唐海琪 袁明宇 +1 位作者 蔡锡斌 闫玉琴 《模具制造》 2022年第2期18-20,共3页
采用浅拉伸成形制件整体弯度形状,便于后工序型面定位可靠,切边-翻边整形-侧整形工艺保证了制件轮廓边线及间隙尺寸精度要求。内藏式斜楔结构与压料芯装配,设计紧凑、强度好、运动可靠。局部切舌结构合理,调试维修方便,效果良好。
关键词 大弯度”横梁 冲压工艺 模具结构
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跨音速单转子压气机气动设计的优化 被引量:2
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作者 张宏武 陈乃兴 +1 位作者 徐燕骥 黄伟光 《工程热物理学报》 EI CAS CSCD 北大核心 2005年第4期581-583,共3页
本文发展了一种提高跨音压气机效率的优化设计方法。该方法由快速叶片造型和网格生成、三维NS方程求解器和优化方法三部分组成。以绝热效率为设计目标,只选择两个参数-最大弯度和最大厚度相对位置沿叶高的分布为优化参数,成功设计了一... 本文发展了一种提高跨音压气机效率的优化设计方法。该方法由快速叶片造型和网格生成、三维NS方程求解器和优化方法三部分组成。以绝热效率为设计目标,只选择两个参数-最大弯度和最大厚度相对位置沿叶高的分布为优化参数,成功设计了一个跨音单转子压气机。在此基础上,进一步考察了叶片端布周向弯曲对跨音单转子压气机性能的影响。 展开更多
关键词 大弯度 最大厚度 优化设计
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静叶吸气对某轴流压气机裕度影响的研究 被引量:4
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作者 陈迪 桂幸民 《航空动力学报》 EI CAS CSCD 北大核心 2008年第3期527-533,共7页
运用Numeca CFD对某大弯度叶栅和某轴流压气机流动进行数值模拟,为减小由于边界层分离而带来的损失,拓宽稳定工作范围,提出叶片吸力面表面开缝抽气方案.综合研究开缝位置、开缝长度、及吸气量大小对流动分离结构和裕度的影响.结果表明... 运用Numeca CFD对某大弯度叶栅和某轴流压气机流动进行数值模拟,为减小由于边界层分离而带来的损失,拓宽稳定工作范围,提出叶片吸力面表面开缝抽气方案.综合研究开缝位置、开缝长度、及吸气量大小对流动分离结构和裕度的影响.结果表明通过静子叶片上边界层抽气引出分离区域的低能量气流,可以明显的改善气动性能,分离得到很好的抑制,稳定工作裕度得到了提高. 展开更多
关键词 航空 航天推进系统 大弯度叶型 抽吸气 轴流压气机 数值模拟
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永蓝东路高架桥挂篮技术研究
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作者 陈海林 《企业技术开发(下半月)》 2011年第10期141-142,共2页
文章介绍的挂篮设计是针对大弧度、大纵坡、高墩柱的高架桥施工。提出了挂篮的系统化、模块螺栓连接的设计思想,以加工厂制作、现场组装拼接的方法而完成。并且采取的一系列调整坡度弧度的措施,很好的解决了挂篮施工中调整困难的工程问... 文章介绍的挂篮设计是针对大弧度、大纵坡、高墩柱的高架桥施工。提出了挂篮的系统化、模块螺栓连接的设计思想,以加工厂制作、现场组装拼接的方法而完成。并且采取的一系列调整坡度弧度的措施,很好的解决了挂篮施工中调整困难的工程问题。简要的陈述在工程施工的实践与应用。 展开更多
关键词 大弯度 大坡度 模块化 螺栓联接 系统化 调平系统
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曲木家具生产设备
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《技术与市场》 1997年第1期30-30,共1页
曲木家具生产设备用单板式薄木片生产曲木家具的关键设备一QSY-150型三向高频液压机由重庆科力森电子木工机械联合厂研制成功,现已通过新产品鉴定。该机的特点是压力大,总吨位为150t,其垂直压头行程最大为800mm,水... 曲木家具生产设备用单板式薄木片生产曲木家具的关键设备一QSY-150型三向高频液压机由重庆科力森电子木工机械联合厂研制成功,现已通过新产品鉴定。该机的特点是压力大,总吨位为150t,其垂直压头行程最大为800mm,水平压头单向行程最大为600mm,有... 展开更多
关键词 曲木家具 木工机械 双向弯曲 液压机 新产品鉴定 生产设备 大弯度 弯曲木 薄木片 关键设备
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Calculation method of first collapse span with superhigh water material backfill mining 被引量:3
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作者 ZHANG Li-ya DENG Ka-zhong 《Journal of Coal Science & Engineering(China)》 2012年第4期374-378,共5页
It is critical for the material to be of active supporting capacity before initial collapse ot mare root wltn supermgn water material backfill mining, and the maximum bending moment should be first calculated in order... It is critical for the material to be of active supporting capacity before initial collapse ot mare root wltn supermgn water material backfill mining, and the maximum bending moment should be first calculated in order to determine the initial collapse span. In the light of principal of virtual work, the simple expression of deflection, bending moment of elastic clamped plate were deduced under the condition of vertical uniform distributed load, horizontal pressure and supporting by elastic foundation, and then, the maximal bending moment expression was derived too. At the same time, the influence degree on square clamped plate by adding horizontal pressure and elastic foundation were analyzed. The results show that the effect of horizontal pressure on maximal bending moment can be ignored when the value of horizontal pressure is two orders of magni- tude less than that of coeificient of elastic stiffness existing elastic foundation. 展开更多
关键词 first collapse span superhigh water material backfill mining elastic clamped plate principal of virtual work
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Axisymmetrical Nonlinear Bending and Buckling of a Circular Plate Under Large Load 被引量:2
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作者 侯朝胜 岳燕玲 《Transactions of Tianjin University》 EI CAS 2005年第3期216-222,共7页
With the terms of the exact series solution taken as trial functions, the method of point collocation was used to calculate the large deflection of a circular plate. The axisymmetrical bending formulae were developed ... With the terms of the exact series solution taken as trial functions, the method of point collocation was used to calculate the large deflection of a circular plate. The axisymmetrical bending formulae were developed for the calculation of a circular plate subjected to polynomial distributed loads, a concentrated load at the center, uniform radial forces and moments along the edge or their combinations. The support may be elastic. The buckling load was calculated. Under action of uniformly distributed load, central load or their compound load, solutions were compared with those obtained by other methods. Buckling beyond critical thrust was compared with that calculated by the power series method. The method presented in this paper has advantages of wide convergent range, high precision and short computing time. Moreover, the computing time is nearly independent of the complexity of the loads. 展开更多
关键词 circular plate large deflection BUCKLING compound load method of point collocation
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The influence of Fe extracting as a filler of fiber concrete performance
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作者 Nawir Rasidi 《Journal of Civil Engineering and Architecture》 2009年第5期46-52,共7页
This research is showing the effect of increasing an Fe extracting from the compression strength, tension and bending moment. The variations in this experiment are the increasing of Fe extracting 0.5%, 1% and 1.5% of ... This research is showing the effect of increasing an Fe extracting from the compression strength, tension and bending moment. The variations in this experiment are the increasing of Fe extracting 0.5%, 1% and 1.5% of concrete volume. Water Cement Ratio (WCR) variation of 0.48, 0.56 and 0.60. The result of increasing 1.5% Fe extracting causes the increasing of tension strength 44.028 kN/cm2, the increasing of slit tension strength 2.226 kN/cm2, the increasing of bending moment 14.81 kN/cm2 from normal concrete. 0.48 WCR produces tension strength, slit tension strength and bending moment more than 0.56 and 0.60 WCR. The increasing of Fe extracting with the distribution variation area and the spread concrete in the tension concrete area produce 3.705 kN/cm2 bending moment higher than the spread fiber in all of concrete area. The 4 cm fiber length produces the higher bending moment than the 2 cm fiber length. The difference is equally 5.185 kN/cm2. The combination result of the examined acting varieties by continuation statistic test gives the result to get the maximum tension and split tensile. It is a concrete combination of increasing 1.5% fiber percentage, 0.48 WCR, full spreading area and the 4 cm fiber length. The maximum bending moment is the increasing of 0.5% fiber percentage, 0.48 WCR, full spreading area and the 4 cm fiber length. 展开更多
关键词 Fe extracting fiber concrete performance acting combination
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Analysis and Improvement of Standing-Up Action for Elderly People from a Chair Using a Cushion-Type Support Tool
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作者 Masakazu Takahashi Reiji Nanba 《Computer Technology and Application》 2012年第11期713-722,共10页
This paper reports the problems that elderly people have when they stand up from a chair, and proposes an adequate standing-up procedure that solves these problems. The important points for an adequate standing-up pro... This paper reports the problems that elderly people have when they stand up from a chair, and proposes an adequate standing-up procedure that solves these problems. The important points for an adequate standing-up procedure are "leaning the upper body forward" and "pulling the legs to the side". Furthermore, this paper proposes a standing-up support tool. The characteristics of the support tool are a cushion-type shape with an adjustable flange and an air-pressure-driven mechanism. When the proposed standing-up procedure and support tool are applied to elderly people, the measured values related to standing-up, such as maximum acceleration, arm force, standing-up time, heel position and forward-bending angle, are improved. Furthermore, elderly people felt that it made the standing-up action easy. We could confirm the effectiveness of the proposed standing-up procedure and support tool. 展开更多
关键词 Elderly people standing-up procedure standing-up support tool cushion-type shape air-pressure-driven mechanism.
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Flexural behavior of in-plane bending glass structures for design method
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作者 吴丽丽 王元清 +2 位作者 严茂超 石永久 张恒秋 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第8期3133-3140,共8页
Experimental study was carried out on the in-plane bending behavior of glass plates without lateral supports, and the effects of the factors, such as height-to-span ratio, on the stability of glass panels were studied... Experimental study was carried out on the in-plane bending behavior of glass plates without lateral supports, and the effects of the factors, such as height-to-span ratio, on the stability of glass panels were studied. Results show that the in-plane bending glass plates with both ends simply supported and their upper edge free lose overall stability under loads, which belongs to the limit-point type of instability. It is found that the buckling load increases linearly with the increase of height-to-span ratio of the glass plates. The lateral stress of in-plane bending glass plates without lateral supports increases linearly under loads; while the large-area stress increases nonlinearly and the lateral stress is not the controlling factor of instability. In finite element analysis, the first buckling mode is regarded as the initial imperfection and imposed on the model as 1/1000 of the span of the components. The numerical buckling load according to the theory of large deflection is less than the experiment result, which is more conservative and can provide some reference for design. For the design method, when the in-plane load is imposed on the glass plate, its lateral strength and the deflection should be verified. Considering the stability of the in-plane bending glass plate without reliable lateral support, buckling is another possible failure mode and calls for verification. 展开更多
关键词 load-bearing glass structure flexural performance in-plane bending BUCKLING
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桨叶翼型弯度对摆线桨悬停状态的气动性能影响
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作者 钱悦 黄典贵 《航空动力学报》 EI CAS CSCD 北大核心 2018年第6期1500-1509,共10页
以悬停状态下的摆线桨为研究对象,利用数值模拟方法,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。结果表明:与桨叶为对称翼型的摆线桨相比,当桨叶具有一定弯度且最大弯度位置适中时,摆线桨气动性能得到很大的提升... 以悬停状态下的摆线桨为研究对象,利用数值模拟方法,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。结果表明:与桨叶为对称翼型的摆线桨相比,当桨叶具有一定弯度且最大弯度位置适中时,摆线桨气动性能得到很大的提升。当桨叶相对弯度X为4%C(C为翼型弦长)、最大弯度位置Y距离前缘40%C^50%C时,摆线桨升力和气动功耗比较低,悬停效率最高,整体气动性能更好。 展开更多
关键词 摆线桨 悬停 相对弯度 大弯度位置 气动性能
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桨叶翼型弯度对摆线桨前飞状态气动性能的影响
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作者 钱悦 黄典贵 《热能动力工程》 CAS CSCD 北大核心 2018年第6期26-33,65,共9页
以前飞状态下的摆线桨为研究对象,使用CFD软件进行数值模拟,非定常时间推进采用双时间法,计算模型的刚体运动采用滑移网格技术处理,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。研究表明:与桨叶为对称翼型的摆线... 以前飞状态下的摆线桨为研究对象,使用CFD软件进行数值模拟,非定常时间推进采用双时间法,计算模型的刚体运动采用滑移网格技术处理,分别研究了桨叶相对弯度X和最大弯度位置Y对摆线桨气动性能的影响。研究表明:与桨叶为对称翼型的摆线桨相比,当桨叶具有一定的弯度且最大弯度位置适中时,推力和推进效率都有显著提高;随着相对弯度的增加,推进效率先增大后减小,存在一个最佳的相对弯度X使得推进效率最高;随着最大弯度位置向尾缘移动,相对弯度X=2%C时,推进效率缓慢上升,相对弯度X〉2%C时,推进效率先增大后减小,存在一个最佳的最大弯度位置Y使得推进效率最高,但升力和载重系数都有所下降。实际应用时,需综合考虑飞行器实际载重确定合适的桨叶弯度。 展开更多
关键词 摆线桨 前飞 相对弯度 大弯度位置 气动性能
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绕线轮的选购与使用
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作者 谭佛航 《中国钓鱼》 1999年第3期23-23,共1页
关键词 绕线轮 曳力 收放线 钓线 绕线轴 操作方法 开关 收线 旋压 大弯度
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A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and Maximum Camber 被引量:1
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作者 Naixing Chen Hongwu Zhang Yanji Xu Weiguang HuangInstitute of Engineering Thermophysics, Chinese Academy of Sciences, P.O. Box 2706, Beijing 100080, 《Journal of Thermal Science》 SCIE EI CAS CSCD 2003年第3期198-203,共6页
A design procedure for improving the efficiency of a transonic compressor blading was proposed based on a rapid generation method for three-dimensional blade configuration and computational meshes, a three-dimensional... A design procedure for improving the efficiency of a transonic compressor blading was proposed based on a rapid generation method for three-dimensional blade configuration and computational meshes, a three-dimensional Navier-Stokes solver and an optimization approach. The objective of the present paper is to design a transonic compressor blading optimized only by selection of the locations of maximum camber and maximum thickness for the airfoils at different span heights and to study how do these two design parameters affect the blade performance. The blading configuration and the computational meshes can be obtained very rapidly for any given combination of maximum camber and maximum thickness. The computational grid system generated is used for the Navier-Stokes solution to predict adiabatic efficiency, total pressure ratio and flow rate. As a main result of the optimization, adiabatic efficiency was successfully improved. 展开更多
关键词 axial transonic compressor 3D aerodynamic design optimization N.S. solver rapid generation of computational meshes
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A sixth-order wavelet integral collocation method for solving nonlinear boundary value problems in three dimensions 被引量:1
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作者 Zhichun Hou Jiong Weng +2 位作者 Xiaojing Liu Youhe Zhou Jizeng Wang 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2022年第2期81-92,I0003,共13页
A sixth-order accurate wavelet integral collocation method is proposed for solving high-order nonlinear boundary value problems in three dimensions.In order to realize the establishment of this method,an approximate e... A sixth-order accurate wavelet integral collocation method is proposed for solving high-order nonlinear boundary value problems in three dimensions.In order to realize the establishment of this method,an approximate expression of multiple integrals of a continuous function defined in a three-dimensional bounded domain is proposed by combining wavelet expansion and Lagrange boundary extension.Through applying such an integral technique,during the solution of nonlinear partial differential equations,the unknown function and its lower-order partial derivatives can be approximately expressed by its highest-order partial derivative values at nodes.A set of nonlinear algebraic equations with respect to these nodal values of the highest-order partial derivative is obtained using a collocation method.The validation and convergence of the proposed method are examined through several benchmark problems,including the eighth-order two-dimensional and fourth-order three-dimensional boundary value problems and the large deflection bending of von Karman plates.Results demonstrate that the present method has higher accuracy and convergence rate than most existing numerical methods.Most importantly,the convergence rate of the proposed method seems to be independent of the order of the differential equations,because it is always sixth order for second-,fourth-,sixth-,and even eighth-order problems. 展开更多
关键词 Nonlinear boundary value problems Eighth-order derivative Coiflet wavelet Integral collocation method Von Karman plate
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Aerodynamic/mechanism optimization of a variable camber Fowler flap for general aviation aircraft 被引量:1
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作者 TIAN Yun WANG Tao +1 位作者 LIU PeiQing FENG PeiHua 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2017年第8期1144-1159,共16页
A conventional Fowler flap is designed to improve the take-off and landing performances of an aircraft. Because the flight states of general aviation aircraft vary significantly. A Fowler flap with a double-sliding tr... A conventional Fowler flap is designed to improve the take-off and landing performances of an aircraft. Because the flight states of general aviation aircraft vary significantly. A Fowler flap with a double-sliding track has been designed, which is ca- pable of changing airfoil camber while cruising and climbing as well as meeting low-speed performance requirements. The aerodynamic characteristics of the variable camber Fowler flap were studied by computational simulation, and cambering was found to be beneficial for improving the lift-to-drag ratio when the lift coefficient was larger than the critical value, below which decambering was more effective; this critical value differed somewhat under different conditions. Taking the mecha- nism into account, the take-off and landing configurations were optimized on the basis of the GA (W)-1 airfoil with a 30% chord Fowler flap. Compared with reference configuration, the maximum lift coefficient of optimized take-off configuration was increased by 6.6% as well as the stalling angle and the lift-to-drag ratio were increased by 1.3° and 7.58%, respectively. Moreover, the maximum lift coefficient of the optimized landing configuration was increased by 6.3%, and the stalling angle was increased by 1.1°; however, the nose-down pitching moment of both configurations increased. Similar results were at- rained on a general aviation aircraft wing/body combination nism was established in a computer-aided design system, achieved by the double-sliding track. A 3D model of the variable-camber Fowler flap driving mecha- and the results showed that all design configurations could be 展开更多
关键词 Fowler flap general aviation aircraft variable camber OPTIMIZATION
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