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Direct rections: 1) 1) Dele lete te th this is te text t bo box 2) Ins 2) nsert ert des desired red pict cture e here here Automated Design and Optimization of a Centrifugal Pump Chad Custer, PhD Technical Specialist Outline


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Direct rections: 1) 1) Dele lete te th this is te text t bo box 2) 2) Ins nsert ert des desired red pict cture e here here

Automated Design and Optimization of a Centrifugal Pump

Chad Custer, PhD Technical Specialist

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Background Optimization objective Analysis tools Results

Outline

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Pumps are designed to:

– Move a certain volume of liquid – Produce a certain exit pressure, which is measured in meters of head

Background

H

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Reducing the power required to drive the pump:

– Allows for a smaller motor

  • Reduces operating cost

A small reduction in required power translates to large cost savings

Background

grundfos.com

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Objective 1. Reduce the power required to drive the pump Constraints Redesign only the impeller blades (not the casing) Maintain the specified volumetric flow rate Maintain the specified outlet pressure

Optimization Statement

Existing Design

Flow rate = 400 m3/h Pressure head = 30 m Power required = 38.4 kW

?

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SLIDE 6

Objective 2. Obtain a set of pump designs that require the least power for any given outlet pressure Constraints Redesign only the impeller blades (not the casing) Maintain the specified volumetric flow rate

Optimization Statement

Unfeasible Wasteful Best Possible

Possible Design Lower Power Design

x Head [m]

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The optimization of two competing factors (mass flow and power) is Pareto optimization All points on the “Pareto Front” are the best possible designs

Optimization Algorithm

Unfeasible Wasteful Pareto Front

Head [m]

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Design and Analysis Tools

HEEDS Multidisciplinary Design Optimization (MDO)

– Process Automation

  • Automate the Virtual Prototype Build Process
  • Enable Scalable Computation across platforms

– Design Exploration

  • Efficient Exploration (Optimization, Sweeps, DOE)
  • Sensitivity & Robustness Assessment

HEEDS Analysis Design

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Typical Optimization Process

Bui uild B Bas asel eline ne Model

  • del

Define O ne Optimizat ation P

  • n Problem

em

Standard Procedure

Propo

  • posed S

d Sol

  • lut

ution

  • n

Satisfied? Sel elec ect O Opt ptimization A n Algor gorithm hm and and Set et T Tuni uning P g Par aram ameters Optimized S d Solut ution

  • n
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SLIDE 10

Bui uild B Bas asel eline ne Model

  • del

Define O ne Optimizat ation P

  • n Problem

em Propo

  • posed S

d Sol

  • lut

ution

  • n

Satisfied? Sel elec ect O Opt ptimization A n Algor gorithm hm and and Set et T Tuni uning P g Par aram ameters Optimized S d Solut ution

  • n

Modern Optimization Process HEEDS Procedure

SH SHER ERPA

  • Hybrid
  • Adaptive
  • No Tuning

Parameters

  • No Optimization

Expertise Required

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SLIDE 11

Design and Analysis Tools

CFturbo Turbomachinery Design

– Interactive design tool

  • Rapid design of high-quality turbomachinery components
  • Integration of established turbomachinery design theory
  • Comfortable, reliable and user friendly
  • Direct interfaces for many CAE-software packages

HEEDS Analysis Design CFturbo

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Turbomachinery design tool that allows for automatic or manual design of machines HEEDS will optimize the design based on 16 design parameters

CFturbo Design

Number of Parameters Control 1 Number of blades 2 Leading edge position 4 Leading edge shape 3 Leading edge incidence angle 1 Leading edge curvature 1 Trailing edge position 3 Trailing edge incidence angle 1 Trailing edge curvature 16 Total

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CFturbo Design Parameters: Leading Edge Position

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Design and Analysis Tools

STAR-CCM+ Multi-physics Analysis

– First-principles computational fluid dynamics focused analysis tool – Integrated environment for:

  • Geometry handling
  • Meshing
  • Solving
  • Post-processing

HEEDS Analysis Design CFturbo STAR-CCM+

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Integrated environment for pre-processing, meshing, solving and post-processing is ideally suited to optimization analysis

STAR-CCM+ Simulation

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Meshing Approximately 700,000 cells Unstructured polyhedral cells Body-fitted prism layers for accurate boundary layer prediction

STAR-CCM+ Simulation

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Solving First-principles Navier-Stokes solution Steady, in-place interface Segregated solver Realizable k-ϵ turbulence model

STAR-CCM+ Simulation

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Steps of analysis (which happen automatically) 1. Import new CAD geometry

STAR-CCM+ Simulation

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Steps of analysis (which happen automatically) 1. Import new CAD geometry 2. Generate mesh

STAR-CCM+ Simulation

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Steps of analysis (which happen automatically) 1. Import new CAD geometry 2. Generate mesh 3. Interpolate previous solution onto new mesh

STAR-CCM+ Simulation

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Steps of analysis (which happen automatically) 1. Import new CAD geometry 2. Generate mesh 3. Interpolate previous solution onto new mesh 4. Solve

STAR-CCM+ Simulation

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Steps of analysis (which happen automatically) 1. Import new CAD geometry 2. Generate mesh 3. Interpolate previous solution onto new mesh 4. Solve 5. Export performance prediction

STAR-CCM+ Simulation

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STAR-CCM+ CFturbo SHERPA

Optimization Process

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STAR-CCM+ CFturbo SHERPA

Optimization Process

Violates Constraint High Power Required Optimal Design

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SLIDE 25

Original Design

– Flow Rate: 400 m3/hr – Head: 29.2 m – Power: 38.4 kW

Single Objective Optimization Results

25 25 | Optimized ed Design gn Optimized Design

– Flow Rate: 400 m3/hr – Head: 29.5 m

  • Power: 36.0 kW
  • 6% reduction in power required
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SLIDE 26

Original Design

Single Objective Optimization Results

26 26 | Optimized ed Design gn Optimized Design

  • Flow remains attached
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SLIDE 27

Original Design

Single Objective Optimization Results

27 27 | Optimized ed Design gn Optimized Design

  • Uniform pressure distribution
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Original Design

Single Objective Optimization Results

28 28 | Optimized ed Design gn Optimized Design

  • Reduces torque on blades
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33 Designs found with lower power requirement

Single Objective Optimization Results

29 29 | Optimized ed Design gn

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33 Designs found with lower power requirement Parallel plot shows that improved designs have similar

– Number of blades – Leading location – Trailing edge location

Single Objective Optimization Results

30 30 | Optimized ed Design gn

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Reduced power required 6% Design parameters and number of runs were the only inputs to the optimization algorithm Algorithm produced a case that resulted in:

– Attached flow – Uniform pressure field – Low torque

  • Low power required

Review of Objective #1

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Pareto Optimization Results Pareto optimization performed to understand trade-off between outlet pressure and power required 580 evaluations allowed

Unfeasible Wasteful

Head [m]

Note: It is challenging to increase pressure without changing the diameter of the machine

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Pareto optimization performed to understand trade-off between

  • utlet pressure and power required

580 evaluations allowed

Pareto Optimization Results

33 33

Par areto to F Front

  • nt

Original Design

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SLIDE 34

Pareto Optimization Results

Head ad Power er 8 % Reduc duction

  • n in Power

er 3. 3.4 4 % Inc ncrease in n Hea ead

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SLIDE 35

Pareto Optimization Results

35 35 0.1 % Reduc duction

  • n in Power

er 10. 10.3 % % Inc ncrease in n Hea ead Head ad Power er

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10 optimal pump designs produced Pressure head up to 34 m

Review of Objective #2

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Pump optimization study achieved two objectives: 1. Improve an existing pump design so that the same flow rate and exit pressure is achieved with lower power

Conclusions

Existing Design

Flow rate = 400 m3/h Pressure head = 30 m Power required = 38.4 kW

Optimized Design

Flow rate = 400 m3/h Pressure head = 30 m Power required = 36.0 kW

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SLIDE 38

Pump optimization study achieved two objectives: 2. Found a set of fan designs that require the least power for any given head up to 34m

Conclusions

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Background Optimization objective Analysis tools Results

Outline