nozzle_flexibility

8/7/2019 NOZZLE_FLEXIBILITY

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M ODELING N OZZLE F LEXIBILITY

The addition of a nozzle flexibility element is meant to model the vessel shell flexibility. Assuming a rigid nozzlewould attract too large of reaction forces at the nozzle and would be too conservative for vessel design. AutoPIPEnozzle flexibility element makes it very easy to estimate shell flexibility using several methods. For cylindricalvessels, the WRC297 and Bijlaard are the preferred methods. For cylindrical tanks with large diameters (order of 100 feet), the API 650 method is the preferred method.

For reduced tee branches, the ASME class I piping formula is appropriate. For nozzles on spherical or tori-spherical heads, the Spherical method is the most appropriate and is based on Bijlaard and is also part of theBD5500 British piping code.

The nozzle element is a modified and simplified expansion joint element. While the expansion joint element has 6stiffnesses, the nozzle element will have only 3 stiffnesses. The three stiffness are, radial, circumferential bendingand longitudinal bending stiffnesses. Two shear and torsion stiffnesses are not applied to the nozzle element. Alsofor the nozzle element, the radial load due to pressure is not added as in the case of the flexible joint. The radialpressure thrust can be added automatically in WinNozl when calculating nozzle stresses.

When modeling the nozzle, the length between the nozzle flange and vessel wall should be modeled as a pipeelement. The nozzle element should always be short; and the shorter it is the more accurate the model. It shouldbe centered at the wall of the shell since it is meant to model the bending flexibility of the shell wall. The best

way to model the nozzle flexibility element is to start it at outer face of the vessel and end it the inner face. Thetotal length would then be the vessel thickness

AutoPIPE will not calculate stresses in the nozzle or the connected vessel. It is recommended that the anchorreaction forces calculated in AutoPIPE be used in WinNozl for evaluating nozzle as well as vessel or shellstresses per the applicable ASME Div I or II, BD5500, KHK and API 650 codes.

AutoPIPE can transmit these forces directly to WinNozl to minimize errors.


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Pressure Thrust on Vessel/Nozzle Junctions

Typical vessel/nozzle configuration showing the pressure thrust acting thenozzle and interconnecting pipework.

Anchor or AxialSupport

Pressure Thrust

AB

C

Figure 1

Where:

P = Internal design or operating pressure of the vessel and piping.A = Inside pipe area of the nozzle.

The pressure thrust of concern is P*A acting on the upstream elbow in aoutward radial direction from the vessel nozzle. The balancing force (P*A) actson the vessel wall opposite to the nozzle as shown in Figure 1. It is assumedthis P*A acting on the vessel is resisted by the vessel support and notconsidered in this load evaluation. The load on the vessel-nozzle junction will bea function of the stiffness between the vessel anchor and load (including any

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nozzle flexibilities) (i.e. K1(x) , Spring 1), and the stiffness of the system (actingin the X direction) upstream of the thrust load (i.e. K2(x), Spring 2) as shown infigure 2 below.

Pressure Thrust P*A

Figure 2

The force F is in equilibrium with the two spring forces F1 and F2:

F = F1 + F2 (1)

The spring stiffness K and the displacement can be related as:

K1 = F1 / 1K2 = F2 / 2

So:

F = 1 * K1 + 2 * K2

Since, 1 = 2, lets denote it by :

So:F = * ( K1 + K2 ) = F / ( K1 + K2 )

Pressure thrust load on the vessel-nozzle junction:F1 = F * K1 / ( K1 + K2 ) (2)

If the piping system on the other side of the applied load (Spring 2) is stiff, for example due to an anchor, then pressure thrust will be absorbed by the anchor.Thus, the nozzle will experience very little direct axial stress. This can be seenfrom equation 2. Note that a greater K2 results in a lower thrust force F1.

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Therefore, in this case including all of the pressure thrust into analysis will beconservative. However if the pipe shown by spring 2 is flexible (maybe anexpansion loop or small diameter pipe with bends) then the nozzle will see moreof the force due to the pressure thrust. Therefore it is appropriate to analyze thelocal vessel/nozzle stresses due to most of the pressure thrust load.

Pressure Thrust GuidelinesIf the combined (membrane + bending) stresses exceed the allowable stresswith the applied full (pressure thrust option under combinations Load TAB) or partial (applied load with correct sign under LOADS TAB) thrust load then it issuggested to check the membrane and combined (secondary ) stress levelswith WRC368 option enabled and thrust load (or option) removed.

WinNOZL WRC368 within its geometric limits provides a good design check of pressure stress levels which includes the full thrust load otherwise use FEAanalysis to obtain more accurate combined stresses.

If the full pressure thrust is acting on the vessel/nozzle junction e.g. nozzle witha blind flange then FEA would generally be the most accurate analysis tool toevaluate.

Note: FEA programs have limitations due to the accuracy of the type of elements used e.g. many programs use thin shell elements which do not

capture transverse shear effects of thick shell elements.

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