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基于几何法的三峡升船机卷筒强度的可靠性分析 被引量:2
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作者 崔海涛 彭兆行 《计算力学学报》 CAS CSCD 1998年第3期353-355,共3页
用几何法分析了三峡升船机卷筒强度的可靠性,克服了传统随机有限元法分析的不足,计算中采用自编部分程序与有限元的通用程序SAP5相结合的方法,减小了自编程序的工作量。
关键词 几何法 卷筒强度 随机有限元 可靠性 升航机
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升船机承船厢有效尺度的分析 被引量:4
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作者 周华兴 《水道港口》 2000年第4期42-45,共4页
根据国内外升船机工程实践和模型试验成果 ,分析了承船厢有效尺度确定的影响因素 ,经统计提出了 L/l、B/b、h/T、n的变化范围以及断面设计。
关键词 升航机 承船厢 有效尺度 断面设计
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三峡水利枢纽航道冲沙建筑物模型试验研究 被引量:1
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作者 陈忠儒 《水电与新能源》 1993年第2期39-44,共6页
本文叙述了三峡枢纽冲沙隧洞和冲沙闸下泄水流为底流水跃多级消能情况时,隧洞洞身水面线和消力池导墙水面线、升船机和船闸航道及下游总航道的流速分布及水流形态。提出了消力池的合适高度,以及隧洞加高、陡坡曲面加肥等建议。并通过工... 本文叙述了三峡枢纽冲沙隧洞和冲沙闸下泄水流为底流水跃多级消能情况时,隧洞洞身水面线和消力池导墙水面线、升船机和船闸航道及下游总航道的流速分布及水流形态。提出了消力池的合适高度,以及隧洞加高、陡坡曲面加肥等建议。并通过工程类比评述了航道冲沙效果。 展开更多
关键词 冲沙建筑物 升航机航道 多级消力池 冲沙效果 工程类比
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Effects of Rising Angle on Upstream Blades and Intermediate Turbine Duct
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作者 LIU Jun WANG Pei +2 位作者 DU Qiang LIU Guang ZHU Junqiang 《Journal of Thermal Science》 SCIE EI CAS CSCD 2016年第4期293-301,共9页
With the improvement of requirement,design and manufacture technology,aero-engines for the future are characterized by further reduction in fuel consumption,cost,but increment in propulsion efficiency,which leads to u... With the improvement of requirement,design and manufacture technology,aero-engines for the future are characterized by further reduction in fuel consumption,cost,but increment in propulsion efficiency,which leads to ultra-high bypass ratio.The intermediate turbine duct(ITD),which connects the high pressure turbine(HPT) with the low pressure turbine(LPT),has a critical impact on the overall performances of such future engines.Therefore,it becomes more and more urgent to master the design technique of aggressive,even super-aggressive ITDs.Over the last years,a lot of research works about the flow mechanism in the diffuser ducts were carried out.Many achievements were reported,but further investigation should be performed.With the aid of numerical method,this paper focuses on the change of performance and flow field of ITD,as well as nearby turbines,brought by rising angle(RA).Eight ITDs with the same area ratio and length,but different RAs ranges from 8 degrees to 45 degrees,are compared.According to the investigation,flow field,especially outlet Ma of swirl blade is influenced by RA under potential effect,which is advisable for designers to modify HPT rotor blades after changing ITD.In addition to that,low velocity area moves towards upstream until the first bend as RA increases,while pressure loss distribution at S2 stream surface shows that hub boundary layer is more sensitive to RA,and casing layer keeps almost constant.On the other hand,the overall total pressure loss could keep nearly equivalent among different RA cases,which implies the importance of optimization. 展开更多
关键词 Intermediate Turbine Duct Swirl Blades Rising Angle Pressure Loss
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ECONOMY
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《Beijing Review》 2016年第25期6-7,共2页
Helicopter Purchase A Chinese consortium has ordered100 H135 twin-engine helicopters from Airbus Helicopters and will build a fnal assembly line in Qingdao,east China’s Shandong Province,Airbus said on June 13.In a p... Helicopter Purchase A Chinese consortium has ordered100 H135 twin-engine helicopters from Airbus Helicopters and will build a fnal assembly line in Qingdao,east China’s Shandong Province,Airbus said on June 13.In a press release,Airbus said that the consortium is made up of China Aviation Supplies Holding Co.,Qingdao United General Aviation Industrial Development Co.and CITIC Offshore Helicopter Co.Ltd. 展开更多
关键词 Aviation Qingdao consortium Shandong assembly ordered sector ECONOMY listed producer
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