sw6强度校核设计源文件-反应器

立式搅拌容器校中—航空动力控制系内筒夹22222校核合校核合校核合校核合校核合 量备注夹套压力试验时，内筒至少需保0.0914991MPa的内压，否则将导致内筒内筒体中航一航空动力控制系GB150.3- 板材 =2[]t =e=n-C1-C2=n=试pT=1.25p[]= [T0.90s=T=pT.(Die)=T合2e[]t[pw]=(Die)=pc(Diet =et合内筒体中航一航空动力控制系GB150.3-- (板材试pT=1.25p=T0.90s=T=pT.(Die)=T合=e=n-C1-C2=n=L=Do=Di+2n=AA=BB=D20时，[pB Do/Doe20时[p]min{(2.251Do/Do/Do/内筒上封头内压计中航一航空动力控制系GB150.3- (板材试pT1.25p[0.5500T0.90s=T=pT.(KDi0.5eh)=T合1 D2K 2i=6 2h i h=2[]t0.5 =eh=nh-C1-C2=min=nh=满足最小厚度要压力计 =KDi合内筒下封头内压计中航一航空动力控制系GB150.3- (板材试pT1.25p[0.5500T0.90s=T=pT.(KDi0.5eh)=T合1 D2K 2i=6 2h i h=2[]t0.5 =eh=nh-C1-C2=min=nh=满足最小厚度要压力计 =KDi合内筒下封头外压计中航一航空动力控制系GB150.3-- (板材试pT=1.25p=T0.90s=T=pT.(KDi0.5e)=T合厚度计h=eh=nh-C1-C2=nh=Do=Di+2nh=K1=A A=K1Do/e =BB=压力计 [p]=(K1Do/e)=夹套圆中航一航空动力控制系GB150.3- 板材 =2[]t =e=n-C1-C2=n=试pT=1.25p[]= [T0.90s=T=pT.(Die)=T合2e[]t[pw]=(Die)=pc(Diet =et合夹套封头计中航一航空动力控制系GB150.3- 试pT1.25p[0.5500T0.90s=T=pT.(KDi0.5eh)=T合1 D2K 2i=6 2h i h=2[]t0.5 =eh=nh-C1-C2=min=nh=满足最小厚度要压力计 =KDi合窄面整体(或带颈松式)法兰计中航一航空动力控制系 N壳体法兰f螺栓bdd个垫片DD-h软垫Nmb b=b0> b=2.53 DGD外+Db0 DGD螺栓受力计Wa=πbDGy=NWp=Fp+F=NAm=max(Ap,Aa)=Ab=nd2=4力矩计FD=0.785D2i=NLD=LA+=MD=FD=FG==NLG=0.5(Db-DG=MG=FG=FT=F-=-NLT=0.5(LA+1+LG=MT=FT=-外压:Mp=FD(LD-LG)+FT(LT-LG);内压:Mp= Mp=W=NLG=Ma=WLG=计算力矩Mo=Mp与Ma[]f/[]中大 M=t 螺栓间距校 Lmin Lmax形状常数确h0Di0h/ho=K=Do/DI=10K7-9ZYeFIh0eFLh01/of=d1Uho =d1Uho =f ψ=δf==4fe13=计算许用结论W DiWp Di 输入法兰厚度δf100.0mm计算许用结论HfMo 1.5[]t=188.2fn n校核合(1.33fe1)