API 579 Fitness for Service for salvage of heat exchanger

Failure in pipe as per API 579 Fitness for Service
Plate Lamination – Failure in Pipe as per API 579 FFS

Introduction

Laminations, air bubbles, cavities are one of the common defects in the pipes or shell which may occur during the rolling process of sheets or any other discontinuity in the metals. These laminations increase the chances of stress concentrations at such locations which may lead to cause of failure in the form of bursts or leakage. Such defects in process industries are hazardous hence validations of these defects for their fitness for service is very important. Below figure 1 and figure 2 shows kind of laminations in the process pipes or shells.

There are different Non Destructive tests can be used to find out region of such defects or cavities; Fitness of Service (FFS) Level 3 suggests validations of such laminations can be done using Finite Element Analysis approach to check whether such defects are fit for service under the current operating conditions

Problem Definition:

A prestigious client of ours had several laminations in the heat exchanger pipe which is why the operation of heat exchanger was stopped for the cause of safety. The client approached us to resolve the issue with utmost urgency and we suggested the use of API 579 Fitness for Service (FFS) Level 3 analysis for reviewing the laminations. API 579 FFS Level 3 suggests checking fitness of dents or laminations by Finite Element Analysis approach to calculate stresses at these locations and to check whether they are fit for service. We have performed FEA Analysis of 5 number of different laminations on heat exchanger pipe operating at 95 Kg/cm2 pressure to conclude whether they need to be replaced as un-fit for service or can be used by lowering the operating parameters.

Methodology for fitness for service analysis: 

Geometric Modeling: 

3D CAD Model of pipe with laminations in the thickness of pipe is generated, open cavities are created across the thickness. Dimensions of the flaws or cavities are provided by the client, below fig. 3 shows the pipe with laminations and figure 4 shows the close view of outline of the lamination into the thickness of pipe.

3D CAD model of pipe
3D CAD Model of Pipe with Lamination       
3D model of lamination in the pipe
 Laminations in the pipe – close-up view

Results & Findings:

Finite Element Analysis of Pipe with Lamination was carried out as per the guidelines of ASME Section VIII, division 2, Part 5. FEA Analysis was carried out for operating loading condition of Pipe, to check the distribution of stress at lamination region stress categorization was carried out and stresses are checked for the allowable limits of the material, below figures shows the Categorized stress lines near Laminations. 

stress categorization
Stress categorization line at lamination 1
Stress categorization line at lamination 2

Results Summary:

From Finite Element Analysis stress intensities at the laminations are found out, these stresses are further categorized into the primary membrane, membrane + bending and secondary stresses, which are further compared with the allowable limits as per ASME Section VIII, Division2, Part 5, figure 5.1, Summary of stresses induced at laminations of pipe are listed below in table.

Stresses at Laminations

Challenges & Achievements:

  1. The major challenge of lamination was to create 3D model from the data received by NDT test as the profile of defect was irregular shaped.
  2. Finite Element Model discretisation and refinement at the laminated region is required so as to maintain minimum more than two elements across the thickness for both side of lamination defect in order to calculate exact stress by stress categorization.
  3. FEA Analysis of Heat exchanger pipe with lamination was very time consuming task due to its heavy Finite Element Model size.
  4. FEA results post processing and validations of FEA Results with analytical approach.
  5. Following the procedure as per as per API 579 – Fitness for service is one of the very challenging task in this job.
  6. We have successfully saved client/OEM heat exchanger by implementing API 579 fitness for service methodology to save the heat exchanger and enhance the remaining life of the equipment.

Conclusion:

From the FEA Analysis of Heat Exchanger pipe with laminations, it is concluded that all the stresses induced as lamination region are within allowable limits of material as per API 579 FFS Part 13, hence heat exchanger pipe with laminations is safe for current operating condition.

Flange Evaluation as per ASME B16.5 Pressure-Temperature Rating

Standard flange for nozzle is having strength identification by dimensionless number which is called as a class. Class, followed by a dimensionless number, is the designate ion for pressure–temperature ratings as follows:

For Example:  Class   150   300   400   600   900   1500   2500

Pressure–temperature ratings are maximum allowable working pressures in bar units at the temperatures in degrees Celsius shown in ASME B16.5 Tables 2-1.1 through 2-3.19 for the applicable material and class designation. In ASME B16.5 Tables II-2-1.1 through II-2-3.19 of Mandatory Appendix II list pressure–temperature ratings using psi units for pressure at the temperature in degrees Fahrenheit.       For intermediate temperatures, linear interpolation is permitted. Interpolation between class designations is not permitted.

For High temperature application:

In high temperature application the creep range will result in decreasing bolt loads as relaxation of flanges, bolts, and gaskets takes place. Flange joint might be leak due to reduce the loads sustain capacity of flange. This is happened due to decreased bolt loads.

For Low temperature application:

In low temperature application the carbon steel may undergo a decrease in ductility. It leads to be unable to safely resist shock loading, sudden changes of stress.

For Case Study Example:

WNRF standard nozzle flange: MOC – SA105

Type / Flange Size / Schedule / Design Temperature / Design Pressure.

WNRF / 150 NB / 40S / 250 Degree Celsius design temperature / 10 barg design pressure.



Table: 1 ASME B16.5 Table 1A: List of Material Specification.

NOTE: 1. ASME Boiler and Pressure Vessel Code, Section II materials may also be used, provided the requirements of the ASME specification are identical to or more stringent than the corresponding ASTM specification for the Grade, Class, or Type listed.

Material of construction A105/SA105 for flange is in under material group 1.1 thus, select pressure-temperature rating table 2-1.1.



Table: 2 ASME B16.5 Table 2-1.1 Pressure-Temperature Rating for Group 1.1 Material
  1. For 150 class WNRF A105 flange Allowable working pressure = 12.1 barg @ 250 Degree Celsius. As per Table: 2 (i.e.)  ASME B16.5 Table 2-1.1 Pressure-Temperature Rating for Group 1.1 Material.
  2. Design pressure for flange is 10 barg @ 250 Degree Celsius.

Conclusion:

Allowable working pressure is greater than Design pressure therefore, 150 class WNRF is pass as per pressure-temperate rating.

Lifting Lug – WRC Calculation

Introduction:

All directly welded parts to the pressure parts like lifting lugs, support lug, trunnion etc. are need to be checked for WRC 107/537. All related calculations are carried out in PV Elite once given proper inputs. In some cases, it is not possible to build such directly welded parts in PV Elite due to software constrain. For example, adding lifting lug on top dish end of vertical equipment is not possible in PV Elite. In those cases, it is mandatory to perform WRC calculations by any other means. This article will help to perform such calculations with analytical solutions followed by CodeCalc calculations.

Inputs:

Consider an equipment with top 2:1 ellipsoidal dish end with directly welded lifting lugs. All necessary input data is given below.

VESSEL ODDm219.1MM
VESSEL THICKNESSt6.16MM
VESSEL WEIGHTWL304.7KG
VESSEL CG HEIGHTL31190.515MM
DESIGN LENGTH T-TL12105.9MM
CG TO TOPL2915.385MM
TAILING LUG OFFSETL4109.55MM
Fig.1 Loads acting on equipment during erection.

Solution:

To consider the maximum force acting on equipment, vessel is considered to be lifted from horizontal position to vertical. At all lifting positions forces acting on lifting and tailing lugs are calculated as given below and maximum of acting force is taken for the analysis. 

Lifting lug forces:

Maximum transverse load per lug     P= P cosθ / N

Maximum longitudinal load per lug   PL= P sinθ / N

Where, N = number of lugs

Tailing lug forces:

Maximum radial load on a lug            P= T sinθ

Maximum longitudinal load on a lug  fL= T cosθ

LIFTING ANGLE θTAILING LOAD T (KG)LIFTING LOAD P (KG)
   
5131.8458372172.8541628
10131.2420611173.4579389
20129.9847735174.7152265
30128.5839955176.1160045
40126.9063811177.7936189
50124.7141611179.9858389
60121.4986062183.2013938
70115.8832583188.8167417
80102.2730061202.4269939
901.55963E-13304.7
   
MAX131.8458372304.7
LIFTING LOAD COMPONENT
MAX TRANSVERSE LOAD PER LUGPTmax1.86651E-14KG
MAX LONGITUDINAL LOAD PER LUGPLmax304.7KG
TAILING LOAD COMPONENT
MAX TRANSVERSE TAILING LOADfLmax131.344124KG
MAX LONGITUDINAL TAILING LOADfrmax11.49112187KG

Therefore, 304.7kg force is taken for WRC analysis and its components acting on lug are calculated as given

h125mm
wl37mm
wb82mm
   
C5.752101mm
Fig.2 Lifting lug geometry and its fillet weld dimensions
Radial load acting on lugPrad0kgf
Longitudinal shear force acting on lugVC304.7kgf
Circumferential shear force acting on lugVL304.7kgf
Circumferential momentMC0kg-m
Longitudinal momentML0kg-m
Torsional momentMT36.33483487kg-m

Thus after calculation of forces and moments acting on lifting lug, WRC 107/537 analysis is carried out in CodeCalc in following steps

Step-1: Input lifting lug data in CodeCalc

Lifting lug data
Fig. 3(a) Lifting lug input data in CodeCalc
Fig.3(b) Lifting lug input data in CodeCalc

Step-2: Input WRC 107/537 data in CodeCalc

lifting lug data
Fig. 4(a): WRC 107/537 inputs in CodeCalc
Fig. 4(b): WRC 107/537 inputs in CodeCalc
Computational fluid dynamics analysis

Computational fluid dynamics Analysis of Jet Mixing using Eductor-Pump in a Large Wastewater Tank

Theoretical Background:

Mixing is one of the common unit operations in chemical industries. The essential task of mixing equipment is to bring together two or more fluids/solids which are initially separated. McCabe rightly quoted “Many processing operations depend for their success on the effective agitation & mixing of fluids”. Desired mixing process could be Multiphase or Single phase, reacting or non-reacting, laminar or turbulent, isothermal or non-isothermal depending upon materials. Mixing could be accomplished either by rotating impellers or by liquid Jet.  Mixing by Impellers explained hereThe purpose of this blog is to give an overview on topic “Theoretical & Computational Fluid Mixing using Jet”.

In jet mixing, part of the liquid from the tank circulated into the tank at high velocities with the help of pumps through nozzles. Due to the nozzle, surrounding fluid entrains and creates a circulatory pattern, which leads to mixing in the tank as shown in Figure. 1.

Figure 1. Working of an Eductor

Comparing to conventional impellers, jet mixers have several advantages such as no moving parts as in conventional agitators, reducing maintenance costs, and it is easy to install when compared with impellers. Eductor consist of a nozzle followed by diffuser, as shown in Figure. 2. The fluid passing which pass through the nozzle section is called as motive fluid and fluid which is being entrained due to high motive velocity is called as entrain fluid. Here the ratio of motive to entrain fluid is 1:4.

Figure 2. Eductor consisting two sections Nozzle followed by Diffuser

Problem Definition:

The selected problem consists of a large rectangular waste water tank with three eductors submerged in the wastewater as shown in Figure. 3 below. The tank is 15-meter-long and 2.8-meter height. The mixing characteristics in the tank is strongly coupled with the kinetic energy transformation by eductors. Therefore, it is desirable to know the accurate flow rate from eductor. The total flowrate from the diffuser section of eductor is calculated from energy balance.

Figure 3. Geometry of Large Rectangular Tank with Three Eductors

Numerical Model, Meshing and Initial & Boundary Conditions:

Computational Fluid Dynamics is very useful to assist in the design, optimization and scale-up of mixing tanks. Still, there are some difficulties which have been countered by some approximation of the physical phenomena, such as turbulence model, rheological models, ideal boundary conditions etc. The generalize equations solved in a mixing calculation i.e. conservation of mass, momentum and energy can be found in a standard chemical engineering books. Fundamental CFD approach can be found in fundamental CFD books.

Figure. 4 depicts the generated mesh for the numerical analysis. Mesh is finer near  eductors outlet due  to large gradients and coarser in elsewhere. Most of industrial mixing tank problems involves turbulent flow, vortices and circulation therefore, resolving of such flow phenomena should be utmost priority while model selection. The standard k-epsilon & k-omega model has been criticized for poor performance with swirling or recirculating flow occurs in mixing tank. The Curvature Correction (CC) modification to k-omega model accounts re-circulation and vortices and hence same has been utilized in this study. Multiphase model selected for the analysis with two fluids having same properties; one fluid is already inside the tank and other is pumped using eductor. Interaction of two fluids provides mixing characteristics. The boundary conditions selected are shown in Table. 1.

Figure. 4 Generated Mesh for Rectangular Tank with Three Eductors

Table 1. Initial & Boundary Conditions

Results & Discussion:

The study has been carried out to find mixing characteristics using eductor pump in large rectangular tank. The analysis has been carried out to optimize the mixing in the tank with respect to number of eductors, position and angle of eductors. Here, the eductors positioned at a position from the bottom of the tank has been discussed only.

Volume fraction of fluid from the eductors noted at different locations in the tank provides the mixing characteristics and interaction two fluids very well. Figure 5 provides wastewater volume fraction (from eductor) over the line passing from the center of one of the eductor respectively at time 1200 secs. From Figure 5. it can be concluded that the three eductors have provided the enough kinetic energy for mixing in a given time of 1200 secs. Each eductor has shown the capacity to drive the fluid for 10 to 11 meter in the compartment. The pumped fluid fraction in middle of the tank is found to be in the range of 0.45 to 0.5, which conforms the strong momentum force acting in this section. With current eductor position it can be concluded that the linear momentum energy transfer is dominant and therefore strong linear mixing has occurred only in the tank. At corners and at the back of all three eductors, negligible momentum transfer has been observed (i.e. zero fraction). Figure. 6. depicts the wastewater fraction over the horizontal section at the definite height interval from bottom to top. Figure 6. also, supports the statements concluded from Figure. 5 in border way.

Figure. 5 Volume fraction over the length of the tank length

Also, check the video below for more information about jet fluid interaction in the tank.

Theoretical & Computational Material Mixing using Rotating Impeller

Introduction: The purpose of this blog is to give an overview of “Theoretical & Computational Fluid Mixing using Rotating Impeller”. Current Chemical & Bio-technical Process Industry widely used different types of Impellers according to their requirements which demands adequate & uniform concentration and temperature. The essential task of the mixers is to bring together two or more fluids and/or solids which are initially separated. Mixing could be accomplished either by rotating impellers or by jets of liquid. Mixing by rotating impellers is the point of interest for as of now for this blog. Liquid Jet Mixing explained here. Also, check agitator design aspects here. McCabe rightly quoted “Many processing operations depend for their success on the effective agitation & mixing of fluids”. Desired mixing process could be Multiphase or Single phase, reacting or non-reacting, laminar or turbulent, Isothermal or Non-isothermal depending upon materials to be mixed and requirement. In most of processes mixing equipment is a simple batch reactor tank with an impeller mounted on a shaft and optionally can contain baffles, and other internals (spargers, coils and draft tubes). The optimum design of a such mixing equipment depends on the desired production rate, properties of the fluids/solids to be mixed, choice of tank and impeller geometry, rotational speed and location of fluid addition and removal. The typical configuration of a stirred tank is shown below in Figure. 1. Figure. 1 Typical Configuration of a  Stirred Tank PART [I]        Theoretical Background: Introduction: In general, mixing refers to any physical operation used to change a non-uniform system into a uniform one. It involves processes such as blending, dissolving, dispersion, suspension, emulsification, heat transfer and chemical reaction. The electric motor is used to rotate the shaft and impeller which transfers the momentum to the fluids by means of blades. The momentum transfer from blades to fluid is basically due to shearing and normal stresses.  In earlier transfer mechanism, the momentum transfer is perpendicular to the flow direction. Whereas in later transfer mechanism the momentum transfer is parallel to the flow direction. Based on these two-momentum transfer mechanism, agitator classification can be made. The shearing stresses momentum transfer includes the rotating disc and cone type agitators and the normal stresses momentum transfer includes the paddle, propeller, and turbo mixer agitators. The momentum of the fluid gain from the impeller blades must be enough to carry material into the most parts of the tank. Therefore, with little understanding of flow types one can conclude that mixing is more effective in turbulent regime compare to laminar. This also can be understood by knowing phenomena’s which contributes mixing. The mixing in the tank is contributed mainly by two phenomena’s, Distribution; in which materials are transported to all regions by advection i.e. bulk circulation currents and Dispersion; in which the eddies (possessing kinetic energy) formed by continuous stirring breakup into smaller eddies. Some characteristics of distribution and dispersion are given below in Table. 1. Other than these two parameters, the third important parameter which plays a vital role is momentum transfer by molecular Diffusion; here, mixing take place on a scale smaller than komogorov scale . Table. 1 Characteristics of different Mixing Phenomena’s Impeller Types, Selection & Flow Field: Impellers are classified conveniently according to the dominance of flow direction. However, due to baffles and other internals, flow patterns in most cases are mixed. Fig. 2 provides some different types of impellers used in industries. While selecting impellers some agitating fluid characteristics is essential to study, which are given below: Characteristics for agitating fluids:
  • Blending of two miscible or immiscible liquids.
  • Dissolving solids in liquids.
  • Dispersing a gas in a liquid as fine bubbles (e.g., oxygen from air in a suspension of microorganism for fermentation or for activated sludge treatment).
  • Agitation of the fluid to increase heat transfer between the fluid and a coil or jacket.
  • Suspension of fine solid particles in a liquid, such as in the catalytic hydrogenation of a liquid where solid catalyst and hydrogen bubbles are dispersed in the liquid.
  • Dispersion of droplets of one im-miscible liquid in another (e.g., in some heterogeneous reaction process or liquid-liquid extraction).
Figure. 2 Impeller Types Table. 2 Provides in brief classification of agitator types with their application, advantages & disadvantages. Also, Fig. 4 provides selection of an impeller based on viscosity of agitating fluid. However, the performance of a shape, size and no of blades of impeller usually difficult to predict which requires experimental or computational resources. Here comes the role of Computational Fluid Dynamics (CFD) to judge the performance of a given design. With robust CFD methodology it is easier to have a judgment on mixing characteristics. Figure 3 Impeller Type Selection based on Fluid Viscosity Table. 2 Classification of Agitator Types with their Application, Advantages & Disadvantages Assessing & Optimizing Mixing: According to industry requirement and with natural limitations by mixing fluid and agitator design, assessment and optimization is vital. In most of times mixing time and power required for mixing considered for the assessment & optimization by varying angle of shaft insertion in tank, angle of tip to end of a blade, no. of blades size of the blade etc.
  • Mixing Time:
As name suggest, it is time required to achieve desired homogenized/uniform solution. Experimentally, it can be measured by injecting tracer into the vessel and following concentration at a fixed point in the tank. Using CFD will be discussed in PART [III]
  • Power Requirement for Mixing:
Electric powered motor is usually used to drive the impeller in the tank. Power requirement for mixing is essentially depending on resistance offered by the fluid to rotation of the impeller. However, fluid properties, required level of mixing, tank size, impeller type & size are also important. The power requirement per unit fluid volume ranges from 10 kW/m3 for small tanks to 1~2 kW/m3 for large tanks. For the power requirement calculation, it is always preferable to work with dimensionless numbers such as the impeller Reynolds number (Re), Flow Number (NQ) and the Power Number (Np). Essential Dimensionless Numbers in Mixing Tank Analysis: Dimensional numbers are very helpful when dealing with fluid flow operations. Some desired numbers useful for optimum design of mixing equipment are given below:
  • Impeller Reynolds Number (Re) : To characterize flow regime
  • Power Number (Np): To calculate power consumed by the turbine
 
  • Flow Number(NQ): To express pumping capacity
Q is volumetric flow rate (m3/s), μ = fluid viscosity (Ns/m2), Ni = Rotational speed of the stirrer (revolution per minute), P = Power (Watt), ρ = density of the mixing fluid (Kg/m3), Di = impeller diameter (m) Also, there has been vast study carried out using these numbers to provide correlations to calculate mixing time and power requirement. PART [II]       CFD Aspects for Mixing Tank Analysis: Introduction: Computational Fluid Dynamics is very useful to assist in the design, optimisation and scale-up of mixing tanks. Still, there are some difficulties which have been countered by some approximation of the physical phenomena, such as turbulence model, rheological models for non-Newtonian fluids and impeller boundary conditions. The basic equations solved in a mixing calculation i.e. conservation of mass, momentum and energy can be found in a standard chemical engineering books. Fundamental CFD approach can be found in fundamental CFD books. Representation of the Rotating Impeller: Resolving rotating impeller-fluid is one of the complicated challenges faced by CFD developers. There are few strategies developed to counter the same, described in brief below: (a) Use of a Momentum Source Term:  The momentum exchange between the impeller blades and the bulk fluid is resolved by empirical co-relation extracted experimentally. However, it is not fully predictive, reliable and implicit. (b) Single & Multiple Frames of Reference (SRF & MRF):  SRF solves governing equations using single rotating frame only, whereas MRF solves rotating zone in rotating reference frame and stationary zone in stationary reference frame. Both approaches don’t count the impeller rotation, it is fixed in one position. Therefore, it can only predict the steady state flow field and does not account for transient impeller-baffle interactions. Using these two methods it is not possible to calculate the mixing time. (c) Sliding Mesh Approach: The Sliding Mesh Approach is the only method which can resolve transient impeller-baffle interaction and provides more accurate solution comparatively. However, the computational cost is more. The basic idea in Sliding Mesh Approach is to employ two grids one of which rotating in small angular steps with the impeller while the other is fixed to the tank. At each step the flow field is recalculated to take into account the new impeller position. Moving mesh is allowed to slide relative to stationary one and interpolation between two meshes is provided by the special cyclic boundary condition. This method allows us to calculate mixing time. Turbulence Model Selection: Most of industrial mixing tank problems involves turbulent flow. In turbulent flow regime, the dispersion plays an important role for mixing therefore it is preferable to utilized robust turbulence model. Large Eddy Simulation (LES) and Direct Numerical Methods (DNS) are not preferable to solve large industrial problems due to high computational cost, though they provide highly accurate solution. Therefore, approximated Reynolds Navier Stokes (RANS) two equation model such as k-epsilon & k-omega widely used to solve industrial problems involving turbulence. For mixing tank problems, vortices and circulation occurred near impeller blades are the source for eddy formation and are vital for momentum transfer and hence for mixing. Therefore, resolving of such flow phenomena should be utmost priority while model selection. The standard k-epsilon & k-omega model has been criticised for poor performance with swirling or recirculating flow which occurs in mixing tank. To account recirculation and vortices, Curvature Correction (CC) modification has been added to the standard RANS models. Furthermore, modifications have been done to predict the onset of separation using Shear Stress Transport (SST) Model and Reattachment Modification (RM) model to account large separation zones. Overall, modified blend of SST-RM-CC model can provide better solution to encounter turbulence occurred in mixing tank. However, with all these modifications to standard two equation model dissipation rate is still underpredicted and turbulence is assumed to be isotropic. To overcome these two problems Reynolds stress transport equations based “Explicit Algebraic Reynolds Stress Models” (EARSM) has been developed. More details about these models can be found in standard books such as Computational Methods for Fluid Dynamics by J. H. Ferziger or else ANSYS CFX theory manual. From literature, it has been found that while most of turbulence models provides good predictions of the mean flow field. However, the accuracy of predictions of turbulence kinetic energy and its dissipation rate has generally been quite poor. However, SST-CC, SST-RM-CC and EARSM can be used accordingly for simulating mixing tank problem. PART [III] Computational Fluid Mixing using Rotating Impeller; A Case Study using OpenFOAM Introduction: In this case study, CFD modelling methods have been applied to predict the fluid flow fields in a mixing tank. The aim of the study is to predict the mean velocity, mixing time, power required by the impeller. The geometry of the mixing tank consists of a cylindrical vessel with Rushton turbine and baffles. The cylinder is 1 meter long and 1 meter of radius (not standard) as shown in Fig. 4.  The fluid in the tank is water only. For the analysis, open-source OpenFOAM CFD tool has been utilized which is widely recommended in scientific community due to its customization ability. Here, also, the base code has been modified to calculate the mixing time by adding scalar transport equation to the main source code. The study includes mesh generation, modelling approach and post processing. The turbulence model selection has already been discussed above in PART [II]. Figure 4. Mixing Vessel with Ruston Turbine Mesh Generation: For the analysis the meshing has been done using snappyHexMesh tool comes with OpenFOAM, which is purely 3D finite volume mesh generator supports hexahedra and split-hexahedra mesh. For the current analysis the volume cells restricted around ~100000 but practical industrial applications demand is multiple of it. Due to large variable gradients nearby blades and other rotating parts, the mesh is dense nearby the blades as shown in Fig. 5 and coarser away from it.  Typically, using coarser mesh mean flow velocity can be predicted well but for turbulence parameter mesh resolution needs to be increased in step wise manner nearby the rotating regions. Here, the mesh nearby the rotating region is more than 45% accommodates volume less than 25 %. Finally, the grid independent study is must before jumping on to main simulation setup. Figure 5. Generated Mesh for Mixing Tank Numerical Methods: The convective terms discretized using second order upwind scheme and temporal parameters using second order backward Euler scheme. Before using second order discretization schemes 1st order schemes used for few iteration steps for the sake of stability. K-Omega SST model has been selected for the current analysis due to its ability to work nicely with curvature/swirling flow along with Sliding Mesh Approach to represent rotating impeller. To resolve pressure-velocity coupling combination of PISO & SIMPLE i.e. PIMPLE algorithm has been selected. Reducing Simulation Time: In practice, it is possible to reduce the simulation time maintaining greater accuracyDifferent approaches for solving rotating impeller problems have already been discussed. The MRF method provides good predictions of the flow field, however it is not possible to calculate mixing time. Whereas Sliding Mesh Method provides all the information we need however, it has high computational cost. To reduce the simulation time following steps are preferable:
  • Work with coarser Mesh using MRF Method for initial few iterations.
  • Then apply the developed flow fields to fine mesh and run for few iterations using MRF method.
  • Finally, switch to Sliding Mesh Method.
  • If turbulence parameters are not converging then let the field be developed using laminar flow and then switch to turbulence model.
Results & Discussion: Soon will be updated

Perfecting Expansion Bellow Design for your Heat Exchanger

Expansion bellows are applicable to fixed tube sheet heat exchanger which help in reducing the longitudinal stresses or tube to tubesheet joint loads by allowing the axial displacement between shell and tubes. RCB-8 flexible Shell Elements (FSE) of TEMA standards deals with the calculation of spring rate and stresses induced in the FSE by using Finite Element Analysis method.

Historically for expansion bellow design, engineers used to calculate the stresses and spring rate using the plate and beam theory nut due to limitations in the plate and beam theory Finite Element Analysis method is the most widely used method for calculating the spring rate and stressed induced in the FSE.

Now let us take practical example of flexible shell element (FSE) for calculation of the spring rate – 

Typical Thick Expansion Bellow used in Heat Exchanger 

Spring rate calculation as per TEMA RCB – 8.5 will be carried out as per following steps – 

  • The flexible shell element (FSE) will be modelled as per section RCB-8.2 & RCB-8.3 i.e. Axi Symmetric model will be created for Finite Element Analysis. Meshing is done in such a way that there much be at least 8 elements across the length of the flexible shell element.
  • An axial load Faxial as described in RCB-8.42 shall be applied at the smaller end of end FSE. 

Faxial will be calculated as per (p/4) x G2 x 100 lbf/in2. We need to model dummy flange at the smaller end by considering the shell up to the minimum length of 2.5SQRT(RT) of the FSE to reduce the stress concentration factor in the stresses induced.

  • Finite Element Analysis will be performed and displacement in the axial direction (d) shall be noted for the applied force (Faxial).
  • The spring rate of the axi symmetric FSE, KAS will be computed as force applied (Faxial) / displacement induced (d).
  • The Spring rate of the entire FSE is KFSE = KAS/2
  • When only one FSE is present then the spring rate is given by K FSE above. When multiple FSE’s are present, the spring rate is given by 

KE = 1/ ((1/KFSE1) + (1/KFSE2) + …. (1/KFSEn))

Where KE is the equivalent spring rate of the entire system.

Most important – Spring calculation to be done for nominal and minimum condition of thickness for corroded and un-corroded condition.

EXPANSION BELLOW SPRING STIFFNESS CALCIULATION (NOMINAL-UNCORRODED)

Preliminary analyses based on the application of a unit axial load as per above steps is carried out to evaluate spring rate of the bellow. 

Un-corroded condition at design temperature

SHELL ID          840                  mm

axial                382091.5365   N


Axisymmetric Geometry of Bellow (Un-Corroded) as TEMA RCB 8
expansion bellow design FEA meshed model.
FEA Meshed Model as per TEMA RCB 8
Loading & Boundary condition plot for Bellow (Un-Corroded)
Axial Deflection plot (Un-Corroded)

SHELL ID          840                  mm

axial                382091.5365   N

Deflection       1.0585 mm (refer above figure)

KFEA = 360974.5266 N/mm

KFSE = ¼ * KFEA = 90243.63166/mm ( for Nominal Un-Corroded )

Similarly, Calculate spring rate for all remaining cases i.e. nominal corroded case, minimum un-corroded and minimum corroded case.

 Nominal  Un-corrodedNominal CorrodedMinimum Un-corrodedMinimum Corroded
Stiffness (N/mm)90243.6316666455.672467929.7995444986.70738