sw6強(qiáng)度校核設(shè)計(jì)源文件-反應(yīng)器

立式攪拌容器校中—航空動(dòng)力控制系內(nèi)筒夾22222校核合校核合校核合校核合校核合 量備注夾套壓力試驗(yàn)時(shí)，內(nèi)筒至少需保0.0914991MPa的內(nèi)壓，否則將導(dǎo)致內(nèi)筒內(nèi)筒體中航一航空動(dòng)力控制系GB150.3- 板材 =2[]t =e=n-C1-C2=n=試pT=1.25p[]= [T0.90s=T=pT.(Die)=T合2e[]t[pw]=(Die)=pc(Diet =et合內(nèi)筒體中航一航空動(dòng)力控制系GB150.3-- (板材試pT=1.25p=T0.90s=T=pT.(Die)=T合=e=n-C1-C2=n=L=Do=Di+2n=AA=BB=D20時(shí)，[pB Do/Doe20時(shí)[p]min{(2.251Do/Do/Do/內(nèi)筒上封頭內(nèi)壓計(jì)中航一航空動(dòng)力控制系GB150.3- (板材試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=滿足最小厚度要壓力計(jì) =KDi合內(nèi)筒下封頭內(nèi)壓計(jì)中航一航空動(dòng)力控制系GB150.3- (板材試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=滿足最小厚度要壓力計(jì) =KDi合內(nèi)筒下封頭外壓計(jì)中航一航空動(dòng)力控制系GB150.3-- (板材試pT=1.25p=T0.90s=T=pT.(KDi0.5e)=T合厚度計(jì)h=eh=nh-C1-C2=nh=Do=Di+2nh=K1=A A=K1Do/e =BB=壓力計(jì) [p]=(K1Do/e)=夾套圓中航一航空動(dòng)力控制系GB150.3- 板材 =2[]t =e=n-C1-C2=n=試pT=1.25p[]= [T0.90s=T=pT.(Die)=T合2e[]t[pw]=(Die)=pc(Diet =et合夾套封頭計(jì)中航一航空動(dòng)力控制系GB150.3- 試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=滿足最小厚度要壓力計(jì) =KDi合窄面整體(或帶頸松式)法蘭計(jì)中航一航空動(dòng)力控制系 N殼體法蘭f螺栓bdd個(gè)墊片DD-h軟墊Nmb b=b0> b=2.53 DGD外+Db0 DGD螺栓受力計(jì)Wa=πbDGy=NWp=Fp+F=NAm=max(Ap,Aa)=Ab=nd2=4力矩計(jì)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=-外壓:Mp=FD(LD-LG)+FT(LT-LG);內(nèi)壓:Mp= Mp=W=NLG=Ma=WLG=計(jì)算力矩Mo=Mp與Ma[]f/[]中大 M=t 螺栓間距校 Lmin Lmax形狀常數(shù)確h0Di0h/ho=K=Do/DI=10K7-9ZYeFIh0eFLh01/of=d1Uho =d1Uho =f ψ=δf==4fe13=計(jì)算許用結(jié)論W DiWp Di 輸入法蘭厚度δf100.0mm計(jì)算許用結(jié)論HfMo 1.5[]t=188.2fn n校核合(1.33fe1)