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三鞍座容器计算

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计算依据: HG/T20582-1998,JB/T4731-2005。 说明:
   This calculation sheet is prepared in accordance with HG/T20582-1998 and JB/T4731-2005. (1) 本计算程序适用于支承在三个均匀且对称布置鞍座上的卧式容器。本计算程序未包
括风载荷和地震载荷作用下鞍座的强度校核。
(2) 浅蓝色单元格内的内容是需要输入的,并应确保输入数据的正确性。 
1 (3) 只有当容器在鞍座平面或靠近鞍座处设置加强圈时,才需要对J58至J68的单元格的
数据进行输入,不设加强圈时,这些单元格应为空白。
计算压力 Calculation pressure P= 0.2 Mpa
设计温度Design temperature 200 ℃
液压试验压力 Hydrostatic test pressure Pt= 0.27 Mpa
容器内径 Inside diameter of vessel
Di=
3800 mm
筒体名义厚度 Nominal wall thickness of shell δn= 20 mm
封头名义厚度 Nominal wall thickness of head
δH=
22 mm
筒体的有效厚度 Effective thickness of shell
δe=
19.7 mm
封头的有效厚度 Effective thickness of head
δhe=
19.1 mm
筒体内半径 Inside diameter of shell
Ri=
1900 mm
筒体平均半径 Mean diameter of shell Rm=Ri+0.5δn= 1910 mm
筒体长度(切线至切线) Length of shell (T.L to T.L) L= 9550 mm
封头内壁曲面深度 Depth of curved surface of head H= 950 mm
边支座中心线到近端部封头切线的距离 Diatance of side support's center line to nearest head's tangent line A= 950 mm
容器操作时的总重量 Total weight of vessel at operating condition W= 2000000 N
容器液压试验时的总重量                                                                  Total weight of vessel at hydrostatic test condition
Wt=
3000000 N
鞍座垫板底面至底板底面之间的距离                                            Distance from bottom of support pad to bottom of base plate Ls= 250 mm
鞍座包角 Saddle included angle θ= 150 °
鞍座垫板的包角 Included angle of saddle pad θ'= 162 °
鞍座垫板有效厚度 Effictive thickness of saddle pad
δPe=
15.7 mm
鞍座垫板的宽度 Width of saddle pad  Bp= 750 mm
鞍座腹板的有效厚度 Effective thickness of web bo= 11.2 mm
支座的轴向宽度 Axial width of supports b= 430 mm
圆筒有效宽度 Effective width of shell  b2=b+1.56×(Rmδn)0.5= 734.90  mm
设计温度下筒体材料的许用应力                                                                Allowable stress of shell material at design temperature
[σ]t=
183 Mpa
设计温度下封头材料的许用应力                                                                Allowable stress of head material at design temperature
[σ]ht=
183 Mpa
容器材料在设计温度的轴向许用压缩应力 Allowable axial compressive stress of vessel material at design temperature
[σ]crt=
96 Mpa
容器材料在常温的轴向许用压缩应力 Allowable axial compressive stress of vessel material at ambient temperature
[σ]cr=
104 Mpa
筒体材料常温屈服强度                                                              Yield strength of shell material at ambient temperature.
ReL=
345 Mpa
鞍座腹板的材料 Material of web Q235-B
鞍座腹板的许用应力 Allowable stress of web material
[σ]sa=
147 Mpa
容器的焊接接头系数 Joint efficiency of vessel Φ= 1
系数 Coefficient k= 0.1
注: 
容器不焊在鞍座上时取k=1,容器焊在鞍座上时取k=0.1
Note:  If the vessel isn't welded on the saddle support,then k=1;if not,k=0.1
鞍座是否设置加强圈?请输入“YES”或“NO”。                                     Are stiffening rings used? Input "YES" or "NO". NO
如果鞍座设置加强圈,请输入以下数据。                                                                                 Input the following data if the saddle has stiffening ring(s).
加强圈的位置:在鞍座平面上时输入“1”,靠近鞍座时输入“2”。                     Location of stiffening ging(s): input "1" if the ring is in the plane of saddle, and "2" if it is adjacent to the saddle. 1
加强圈的材料 Material of stiffening ring
加强圈材料的许用应力 Allowable stress of stiffening ring material [σ]rt= Mpa
加强圈与圆筒有效段的组合截面积 Area of composite section
Ao=
mm2
组合截面对X-X轴的惯性矩 Moment of inertia of composite section
Io=
mm4
尺寸d (见下图) Dimension d (see sketch below)
d=
mm
尺寸e (见下图) Dimension e (see sketch below)
e=
mm
由JB/T4731查得系数C4 Coefficient C4 from JB/T4731
C4=
由JB/T4731查得系数C5 Coefficient C5 from JB/T4731
C5=
由JB/T4731查得系数K7 Coefficient K7 from JB/T4731
K7=
由JB/T4731查得系数K8 Coefficient K8 from JB/T4731
K8=
1
1.筒体轴向弯矩计算 calculation of shell longitudinal moment
(1) 操作工况 Operating condition
单位长度重量均布载荷 Uniform load per unit length due to the total weight of equipment q=W/(L+4H/3) 184.90  N/mm
边支座处弯矩                                 Moment at the side supports 1 -67768875 N.mm
中间支座处弯矩 Moment at the center support 1 -3.04E+08 N.mm
跨距中点弯矩                            Moment at Mid-span 1 162470427 N.mm
(2) 液压试验工况 Hydrostatic test condition
单位长度重量均布载荷 Uniform load per unit length due to the total weight of equipment qT=Wt/(L+4H/3) 277.35  N.mm
边支座处弯矩                                 Moment at the side supports 1 -1.02E+08 N.mm
中间支座处弯矩 Moment at the center support 1 -4.56E+08 N.mm
跨距中点弯矩                            Moment at Mid-span 1 243705641 N.mm
2.支座反力计算 calculation of reactor force on the support
(1) 操作工况 Operating condition
边支座反力                                    Reaction of side supports  1 701459.8 N
中间支座反力                                   Reaction of center support 1 997080.4 N
(2) 液压试验工况 Hydrostatic test condition
边支座反力                                    Reaction of side supports  1 1052189.7 N
中间支座反力                                   Reaction of center support 1 1495620.6 N
3.筒体轴向应力计算 calculation of longitudinal stress in the shell
(1) 操作工况 Operating condition
1)两支座中间处的横截面上 Cross-section in the middle of two supports
最高点 The highest point 1 8.98  Mpa
最低点 the lowest point 1 10.42  Mpa
2)边支座处横截面上 Cross-section at side supports
A/Rm= 0.497 
筒体被加强的最高点或筒体不被加强的靠近中间水平平面处 the toppest point on the shell when reinforced  or the point close to the middle hotizontal plane when not reinforced
查JB/T4731,得系数K1=    Refer to JB/T4731, coefficient K1= 1 1
1 10.00  Mpa
查JB/T4731,得系数K2=      Refer to JB/T4731 , coefficient K2=  1
最低点 The lowest point 1 9.40  Mpa
3)中间支座处横截面上 Cross-section at center support
0.5L/Rm= 2.500 
筒体被加强的最高点或筒体不被加强的靠近中间水平平面处 The toppest point on the shell when reinforced  or the point close to the middle hotizontal plane when not reinforced
查JB/T4731,得系数K1=    Refer to JB/T4731, coefficient K1= 0.161 注1:
1 18.07  Mpa 鞍座平面上没有加强圈时,对于中间鞍座应根据0.5L≤Rm/2或0.5L>Rm/2,由JB/T4731的表7-3查得K1和K2的数值。
查JB/T4731,得系数K2=      Refer to JB/T4731 , coefficient K2=  0.279 A/Rm= 0.497  0.5L/Rm= 2.500 
最低点 The lowest point 1 4.87  Mpa
4)筒体轴向应力验算 Ceck of shell longitudinal stress
取出上述轴向应力中的最大拉应力(最大正值) Take out the maximum tensile stress (the maximum positive) from the above calculated longitudinal stresses                                                                       
σmt=max{σ1,σ2,σ3A,σ3B,σ4A,σ4B}= 18.07  Mpa
Φ*[σ]t= 183.00  Mpa
 σmt<Φ[σ]t ,  合格,  Acceptable. 
取出上述轴向应力中的最大压应力(最小负值)Take out the maximum compressive stress (the maximum negative) from the above calculated longitudinal stresses
σmc=|min{σ1,σ2,σ3A,σ3B,σ4A,σ4B}|= 0 Mpa
 σmc<[σ]crt ,   合格,  Acceptable. 
(1) 液压试验工况 Hydrostatic test condition
分别以P=Pt和P=0代入上述σ1、σ2、σ3A、σ3B、σ4A和σ4B的计算式中并以MTA、MTB和MTP代替式中的MA、MB和MP,就可以求得液压试验工况以及容器充满水但未加压时的轴向应力σT1、σT2、σT3A、σT3B、σT4A、和σT4B,计算结果见下表。
Let P=Pt and P=0 respectively in the calculation formulas for σ1,σ2,σ3A,σ3B,σ4A, and σ4B, and use MTA, MTB, MTP instead of MA, MB and MP, the longitudinal stresses under hydrostatic test condition σT1,σT2,σT3A,σT3B,σT4A, and σT4B can be obtained as follows.  
筒体的轴向应力 Longitudinal stresses in shell, Mpa
液压试验工况                           Hydrotest condition 充满水但未加压 Full of water but no pressure
两支座中间处的横截面上 Cross-section in the middle of two supports σT1 12.01  -1.08 
σT2 14.17  1.08 
边支座处横截面上 Cross-section at side supports σT3A 13.54  0.45 
σT4A 12.64  -0.45 
中间支座处横截面上 Cross-section at center support σT3B 15.11  2.02 
σT4B 11.07  -2.02 
液压试验工况                           Hydrotest condition σMT=max(σT1,σT2,σT3A,σT3B,σT4A,σT4B)= 15.11  Mpa
0.9ΦReL= 310.5 Mpa
σMT<0.9ΦReL,   合格,  Acceptable.
充满水但未加压 Full of water but no pressure σMC=|min(σT1,σT2,σT3A,σT3B,σT4A,σT4B)|= 2.02  Mpa
σMC<[σ]cr,   合格,  Acceptable.
4.切向剪应力计算 calculation of tangential shearing stress
(1)边支座处横截面上 Ccross-section at side supports 1
筒体中:查JB/T4731,得系数K3=                                                            For shell, refer to JB/T4731, coefficient K3= 0.485
1 9.04  Mpa
封头中:查JB/T4731,得系数K4=                                                                For head, refer to JB/T4731, coefficient K4= 0.295
1 5.67  Mpa
(2)中间支座处横截面上 Cross-section at center support
查JB/T4731,得系数K3=  Refer to JB/T4731, coefficient K3= 0.799
Q=FB/2= 498540.20  N
1 10.59  Mpa
(3)切向剪应力验算 Check of tangential shearing stress 注2:
对椭圆封头 For ellipsoidal head 鞍座平面上没有加强圈时,对于中间鞍座应根据0.5L≤Rm/2或0.5L>Rm/2,由JB/T4731的表7-3查得K1和K2的数值。
封头形状系数 Shape factor of ellipsoidal head  K= 1
1 19.90  Mpa A/Rm= 0.497  0.5L/Rm= 2.500 
max{τA,τB}= 10.59  Mpa
0.8[σ]t= 146.4 Mpa
 max{τA,τB}<0.8[σ]t ,   合格,   Acceptable. 
1.25[σ]ht= 228.75 Mpa
τH+σH=
25.57  Mpa
τH+σH<1.25[σ]t ,   合格,  Acceptable. 
5.筒体周向应力计算 calculation of shell circumference stress
(1) 无加强圈的圆筒或加强圈位于靠近鞍座处                                                                            For shells without stiffening rings or with stiffening rings adjacent to the saddles 
垫板是否起加强作用? Does the pad play a part in stiffening? YES
1) 支座处横截面最低点周向应力
   Circumference stress at the lowest point of the support's cross-section  1
查JB/T4731,得系数 K5=     Refer to JB/T4731, coefficient K5= 0.673
σ5A=σ5C=-k*K5*FA/(δe+δpe)*b2) -1.81  Mpa
 |σ5A|=|σ5C|<[σ]t ,   合格,  Acceptable. 
σ5B=-k*K5*FB/((δe+δpe)*b2) -2.58  Mpa
 |σ5B|<[σ]t ,   合格,  Acceptable. 
2) 边鞍座边角处 At horn of side supports 
查JB/T4731,得系数K6=     Refer to JB/T4731, coefficient K6= 0.008
(0.5L+A)/Rm= 3.00 
(0.5L+A)/Rm≥8时:
σ6A=σ6C=-FA/(4(δe+δpe)b2)-3*K6*FA/(2(δe^2+δpe^2)) Mpa
(0.5L+A)/Rm<8时: 注3:
σ6A=σ6C=-FA/(4(δe+δpe)b2)-12K6*FA*Rm/((0.5L+A)*(δe^2+δpe^2)) -42.14  Mpa 鞍座平面上没有加强圈时,对于中间鞍座应以0.5L/Rm取代A/Rm,由JB/T4731的表7-3查得K6b的数值。
σ8A=σ8C= -42.14  Mpa
|σ6A|=|σ6C|<1.25[σ]t,    合格,   Acceptable. A/Rm= 0.497  0.5L/Rm= 2.500 
3) 中间鞍座边角处 At horn of central support 
查JB/T4731,得系数K6b=     Refer to JB/T4731, coefficient K6b= 0.032
(L-2A)/Rm= 4.01 
(L-2A)/Rm≥8时:
σ6B=-FB/(4(δe+δpe)*b2)-3*K6b*FB/(2(δe^2+δpe^2)) Mpa
(L-2A)/Rm<8时:
σ6B=-FB/(4(δe+δpe)*b2)-12*K6b*FB*Rm/((L-2A)(δe^2+δpe^2)) -160.22  Mpa
σ6B= -160.22  Mpa
|σ6B|<1.25[σ]t,    合格,   Acceptable.
4) 边鞍座垫板边角处 At horn of side support pad 
根据A/Rm和θ'=θ+12°的数值,由JB/T4731查得K6'  Based on the values of A/Rm and θ'=θ+12°, obtain K6' from JB/T4731 K6'= 0.006
σ6A'=σ6C'=-FA/(4*δe*b2)-12*K6'*FA*Rm/((0.5L+A)*δe^2) -55.53  Mpa
|σ6A'|=|σ6C'|<1.25[σ]t,    合格,   Acceptable.
5) 中间鞍座垫板边角处 At horn of central support pad 
根据0.5L/Rm和θ'=θ+12°的数值,由JB/T4731查得K6b' Based on the values of 0.5L/Rm and θ'=θ+12°, obtain K6b' from JB/T4731 K6b'= 0.025
σ6B'=-FB/(4*δe*b2)-12*K6b'*FB*Rm/((L-2A)*δe^2) -209.66  Mpa
|σ6B'|<1.25[σ]t,    合格,   Acceptable.
(2) 有加强圈的圆筒 For shells with stiffening rings
1) 边鞍座边角处圆筒的周向应力                                                                 Circumferential stress in the shell at corner of side support  
1 Mpa
2) 中间鞍座边角处圆筒的周向应力                                                                 Circumferential stress in the shell at corner of central support 
1 Mpa
3) 边鞍座边角处加强圈内缘或外缘表面的周向应力                                                                 Circumferential stress in the stiffening ring at corner of side support  
1 Mpa
4) 中间鞍座边角处加强圈内缘或外缘表面的周向应力                                                                 Circumferential stress in the stiffening ring at corner of central support  
1 Mpa
6.腹板拉伸应力计算 calculation of tensile stress in web
F=max(FA,FB) 997080.4 N
K9= 0.259
Fs=F9*F 258243.82 N
Hs=min(Ls,Rm/3) 250 mm
σ9=Fs/(Hs*bo+b2*δpe) 18.01  Mpa
σ9<[σ]sa,   合格,  Acceptable.
计算
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