ASME Code Section VIII Pressure vessel design Leonard

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ASME Code Section VIII Pressure vessel design Leonard D. Tijing Ph. D Candidate

ASME Code Section VIII Pressure vessel design Leonard D. Tijing Ph. D Candidate

Factor A

Factor A

Factor A

Factor A

Factor B : Fig. CS-2 For most common materials

Factor B : Fig. CS-2 For most common materials

Fig. NFA-1 Aluminum alloy 3003

Fig. NFA-1 Aluminum alloy 3003

Internal pressure formulas

Internal pressure formulas

Heads

Heads

Allowable stress for carbon and low alloy steel (S)

Allowable stress for carbon and low alloy steel (S)

External pressure: Sphere and hemispherical head n Procedure: – 1) Assume t. – 2)

External pressure: Sphere and hemispherical head n Procedure: – 1) Assume t. – 2) Calculate A, A=0. 125/(Ro/t) – 3) Get value of B. § If A falls to the left, use Pa=0. 0625 E/(Ro/t)2 – 4) Calculate Pa=B/(Ro/t)

External pressure: Ellipsoidal head n Procedure: – Same with sphere procedure. – Use Ro=0.

External pressure: Ellipsoidal head n Procedure: – Same with sphere procedure. – Use Ro=0. 9 Do

External pressure: Torispherical head n Procedure: – Same procedure. – Use Ro(maximum)=Do

External pressure: Torispherical head n Procedure: – Same procedure. – Use Ro(maximum)=Do

Example: Internal pressure n Design data: – P = 100 psi – S =

Example: Internal pressure n Design data: – P = 100 psi – S = SA 515 -70 plate at 650 o. F – E = 0. 85 (spot-examined for shell and semispherical head) – E = 1. 0 (seamless head) – R = 48 in – D = 96 in – t = required wall thickness – CA = 0. 125

Internal pressure: Cylindrical shell 1) Determine the required thickness of a shell. n 2)

Internal pressure: Cylindrical shell 1) Determine the required thickness of a shell. n 2) Determine the MAWP, P for the design thickness used when the vessel is in new condition. n

Internal pressure: Sphere and hemispherical head 1) Determine the required thickness of a hemispherical

Internal pressure: Sphere and hemispherical head 1) Determine the required thickness of a hemispherical head. n 2) Determine the MAWP, P for the head design thickness used when it is in new condition. n

Internal pressure: Ellipsoidal head 1) Determine the required thickness of a seamless ellipsoidal head.

Internal pressure: Ellipsoidal head 1) Determine the required thickness of a seamless ellipsoidal head. n 2) Determine the MAWP, P for the seamless head design thickness used when it is in corroded condition. n

Example 1: External pressure n Design information: – P = full vacuum – T

Example 1: External pressure n Design information: – P = full vacuum – T = 500 o. F – Shell and head material = SA-285 Gr. B, S=27 ksi – CA = 0. 0625 in. n Question: Is 7/16 in thickness acceptable?

External pressure: Solution procedure n n 1)Calculate unstiffened design length, L and Do of

External pressure: Solution procedure n n 1)Calculate unstiffened design length, L and Do of the shell 2) Determine ratios L/Do and Do/t 3) Determine value of A using figure 4) Get value of B from graph. – If A is to the left of the graph, calculate Pa=2 AE/[3(Do/t)] 5) If there is B, use Pa=4 B/[3(Do/t)] n 6) Compare Pa with design external pressure. If Pa is greater, thickness is acceptable n

Example 2: External pressure with stiffeners n n n n P = 15 psig

Example 2: External pressure with stiffeners n n n n P = 15 psig Do = 96 in L = 48 ft Heads 2: 1 ellipsoidal Material of shell SA 285 C plate T = 500 o. F E = see chart t=?

Example: External pressure Vessel with stiffeners n n 1)Calculate unstiffened design length, L and

Example: External pressure Vessel with stiffeners n n 1)Calculate unstiffened design length, L and Do of the shell 2) Determine ratios L/Do and Do/t 3) Determine value of A using figure 4) Get value of B from graph. – If A is to the left of the graph, calculate Pa=2 AE/[3(Do/t)] 5) If there is B, use Pa=4 B/[3(Do/t)] n 6) Compare Pa with design external pressure. If Pa is greater, thickness is acceptable n

Thickness range (inches) (1/16 inches step) n n n n 0. 1875 0. 25

Thickness range (inches) (1/16 inches step) n n n n 0. 1875 0. 25 0. 3125 0. 375 0. 4375 0. 5625 0. 6875 n 0. 8125 n 0. 875 n 0. 9375 n 1. 0 … 6. 0 n