欢迎来到天天文库
浏览记录
ID:55158200
大小:126.50 KB
页数:5页
时间:2020-04-29
《预应力钢筋张拉计算.doc》由会员上传分享,免费在线阅读,更多相关内容在工程资料-天天文库。
1、预应力钢绞线张拉计算预应力钢绞线共4束,采用Φj15.24预应力钢绞线,张拉控制应力σcon=0.75Ry=1395Mpa,单根张拉控制力F=1395×140=195.3KN。一、100%σcon理论伸长量计算伸长量计算公式如下:⊿L=;Pp=其中:Pp—预应力筋平均张拉力(N);P—预应力筋张拉端张拉力(N);L—从张拉端至计算截面的孔道长度(m);Ep—预应力筋弹性模量(MPa),取1.95×10;Ap—预应力筋的截面面积(mm)θ—从张拉端到计算截面曲线孔道部分切线的夹角之和(rad);k—孔道每米局部偏差对
2、摩擦的影响系数,取0.0015μ—预应力筋与孔道的摩擦系数,取0.2~0.25;半跨预应力钢绞线参数表钢束线段长度L(m)夹角θ(rad)KL+μθe-(KL+μθ)P(KN)Pp(KN)N1O1A10.7001195.3195.3A1B19.815001195.3195.3B1C18.378(弧长)0.0.0.195.3182.1C1D11.373001182.1182.1N2O2A20.7001195.3195.3A2B27.3001195.3195.3B2C28.378(弧长)0.0.0.195.3182.1
3、C2D23.927001182.1182.1N3O3A30.7001195.3195.3A3B31.037001195.3195.3B3C32.234(弧长)0.0.0.195.3191.7C3D316.378001191.7191.7N4O4A40.7001195.3195.3A4B41.037001195.3195.3B4C42.234(弧长)0.0.0.195.3191.7C4D416.378001191.7191.7注:OA段为千斤顶、工具锚、限位板等占用长度,OA段系数k、μ取值为零伸长量计算如下:N1钢
4、束O1A1段△L1A1B1段△L2B1C1段△L3C1D1段△L4N2钢束O2A2段△L1A2B2段△L2B2C2段△L3C2D2段△L4N3钢束O3A3段△L1A3B3段△L2B3C3段△L3C3D3段△L4N4钢束的伸长量同N3钢束;钢束线段(半跨)总伸长量(mm)OA(mm)AB(mm)BC(mm)CD(mm)N15.0170.2255.889.16280.54N25.0152.2255.8826.19278.6N35.017.4215.69115.01286.26N45.017.4215.69115.012
5、86.26二、张拉力计算张拉采用两端对称张拉,张拉过程中设定大里程端为张拉甲,小里程端为张拉乙,张拉所使用的千斤顶及配套压力表如下:张拉端千斤顶规格、型号配套压力表回归方程张拉甲1#9211.69#Y=34.9915X+19.1429张拉乙2#7016.66#Y=34.3997X+12.7857各行程甲、乙端张拉力、压力表、伸长量如下:钢束第一行程10%σcon第二行程20%σcon第三行程10%σcon张拉力(KN)压力表读数伸长量(mm)张拉力(KN)压力表读数伸长量(mm)张拉力(KN)压力表读数伸长量(mm
6、)张拉甲(MPa)张拉乙(MPa)张拉甲(MPa)张拉乙(MPa)张拉甲(MPa)张拉乙(MPa)N1136.713.363.628.05273.427.277.5856.111367.138.5239.37280.54N2156.243.924.1727.86312.488.388.7155.721562.444.145.05278.6N3175.774.484.7428.63351.549.509.8557.251757.749.6950.72286.26N4175.774.484.7428.63351.549
7、.509.8557.251757.749.6950.72286.26钢束第一行程10%σcon第二行程20%σcon第三行程10%σcon张拉力(KN)压力表读数伸长量(mm)张拉力(KN)压力表读数伸长量(mm)张拉力(KN)压力表读数伸长量(mm)张拉甲(MPa)张拉乙(MPa)张拉甲(MPa)张拉乙(MPa)张拉甲(MPa)张拉乙(MPa)N1136.7133.0921.71273.426.856.943.421367.137.6537.39217.08N2156.243.553.6321.52312.487
8、.957.9943.041562.443.1542.83215.24N3175.774.14.1821.2351.549.059.0842.41757.748.6548.28211.98计算:复核:
此文档下载收益归作者所有