Additive Manufacturing for Large Structures · Topology and process optimization prof. van den...

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1 1 Additive Manufacturing for Large Structures Dr Marcel Hermans Dr Constantinos Goulas Prof. Ian Richardson Department of Materials Science and Engineering Delft University of Technology 2 2 Contents Introduction Basic idea History Control Examples Ambitions & Challenges Images courtesy Cranfield University

Transcript of Additive Manufacturing for Large Structures · Topology and process optimization prof. van den...

Page 1: Additive Manufacturing for Large Structures · Topology and process optimization prof. van den Boogaard, U. Twente 34 The AiM2XL Programme Project 2: From structure to properties

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Additive Manufacturing for Large Structures

Dr Marcel HermansDr Constantinos Goulas

Prof. Ian Richardson

Department of Materials Science and EngineeringDelft University of Technology

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Contents

• Introduction

• Basic idea• History• Control

• Examples

• Ambitions & Challenges

Images courtesy Cranfield University

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Metal Additive ManufacturingAlso known as

• Additive (Layer) Manufacture (A(L)M)• (Laser) Cladding• Buttering• Digital manufacture• Direct Light Fabrication• Direct Metal Casting (DMC)• Direct Metal (Laser) Deposition (DM(L)D)• Laser Direct Casting or Deposition• Laser casting• Laser cladding • Laser Engineered Net Shaping (LENS)• Lasform• Laser melting• (Metal) Rapid Prototyping• Net shape manufacture• Net shape engineering• Shaped deposition manufacturing• Shaped melting• Selective Laser Melting (SLM)• Shaped Metal Deposition (SMD)• Shape Melting Technology (SMT)• Shape welding• Solid freeform fabrication (SFF)

Very Simply

Melting ⇒ Welding

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Basics of metal AM systems

For a single axisymmetric energy source at maximum melting efficiency build rate depends on the square of the layer height

Build

rate

kg/

hr

layer height (mm)1 2

1

4

0.1

0.01

0.225

0.5 3

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WAAM

Blown powder

Powder bed

High build rate wire processes

Resolution depends on the exact width to height ratio and on several other factors but is usually about 1.5 times the layer height

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Metal Additive Manufacture - History

• 1926 Baker – patented “The use of an electric arc as a heat source to generate 3D objects depositing molten metal in superimposed layers”

• 1971 Ujiie (Mitsubishi) Pressure vessel fabrication using SAW, electroslag and TIG, also multi-wire with different wires to give functionally graded walls

• 1983 Kussmaul used Shape Welding to manufacture high quality nuclear structural steel (20MnMoNi5 5) parts – deposition rate 80kg/hr – total weight 79 tonnes

This idea has been around awhile!

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• 1993 Prinz and Weiss patent combined weld material build up with CNC milling – called Shape Deposition Manufacturing (SDM)

• 1994-99 Cranfield University develop Shaped Metal Deposition (SMD) for Rolls Royce for engine casings, various processes and materials were assessed – still in production

800 mm

Metal Additive Manufacture - History

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Images courtesy Cranfield University

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Arc Based Deposition Processes

Gas Metal Arc

Gas Tungsten Arc

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Deposition Gas Metal Arc Welding

Globular transfer

Short circuiting transfer Pulsed transfer

Streaming transfer

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Thermal History

3 mm10 mm30 mm50 mm

70 mm

Properties depend on material composition and thermal history (time, temperature, cooling rate).

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Microstructure field

Increased travel speedCross section, steel weldFusion Zone, Heat Affected Zone

Seijffers

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Microstructure field

• Solidification

• Uni-directional heat flow

• Metallurgical effects (solidification microstructure, segregation, solid state transformations, grain size, precipitation, tempering, etc..)

R. SeijffersAISI316L/GTAW

Transverse crossSection

Heat flow

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No cooling

Cooling during deposition

CoolingInterpass time 7 s, 16 layers

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Wire Arc Additive Manufacturing (WAAM)

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Video & Images courtesy Cranfield University

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Courtesy: DAMEN & RAMLAB

WAAMpeller Project

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WAAMpeller Project

Place video here pleaseand check the sound level

Please set to start on click

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Courtesy: RAMLAB

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Total weight: 410 kg

• Weight Hub/Cap/Shaft/: 48kg/~5kg/~20kg = 73 kg

• Total welded wire ~ 337 kg

• Total build time: ~300 hours at ~1,6 kg/hour

WAAMpeller project

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Courtesy: RAMLAB

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Courtesy: DAMEN & RAMLAB

WAAMpeller Project

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H. Meigh, Cast and wrought aluminium bronzes, properties, processes and structure. Leeds: Maney Publishing, 2000.

Nickel Aluminum Bronze - Microstructure

• α phase: Cu-rich, FCC• β phase: Cu-rich, BCC

(HCP-martensite)

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β

• α phase: Cu-rich, FCC• β phase: Cu-rich, BCC

(HCP-martensite)• !" : 20-50 μm

Nickel Aluminum Bronze - Microstructure

H. Meigh, Cast and wrought aluminium bronzes, properties, processes and structure. Leeds: Maney Publishing, 2000.

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• α phase: Cu-rich, FCC• β phase: Cu-rich, BCC

(HCP-martensite)• !" : 20-50 μm• !# : 5-10 μm

Nickel Aluminum Bronze - Microstructure

H. Meigh, Cast and wrought aluminium bronzes, properties, processes and structure. Leeds: Maney Publishing, 2000.

β

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• α phase: Cu-rich, FCC• β phase: Cu-rich, BCC

(HCP-martensite)• !" : 20-50 μm• !# : 5-10 μm• !$ : lamellar form

Nickel Aluminum Bronze - Microstructure

H. Meigh, Cast and wrought aluminium bronzes, properties, processes and structure. Leeds: Maney Publishing, 2000.

β

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• α phase: Cu-rich, FCC• β phase: Cu-rich, BCC

(HCP-martensite)• !" : 20-50 μm• !# : 5-10 μm• !$ : lamellar form• !% : 2 μm

Nickel Aluminum Bronze - Microstructure

H. Meigh, Cast and wrought aluminium bronzes, properties, processes and structure. Leeds: Maney Publishing, 2000.

β

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WAAM CuAl8Ni6 - Microstructure

As Cast WAAM deposit

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Anisotropy in mechanical properties of 3D-Printed Bronze

TD WD BDDirections

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• Hooks: critical part of large offshore construction cranes

• Safe Working Loads (SWL): ranging from 100 – 10000 tons

• Conventional production: forging, casting

• Size range: 1m – 5.5m

Case: Large offshore crane hooks

Cast Ramshorn (2-prong) hook

• With size, both delivery time and material quality challenges increase

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Case: Large offshore crane hooks

Cast 4-prong hook

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Weight approx. 1000 kg

Width approx. 1.1 m

Case: Large offshore crane hooks

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AM Technical Challenges• Control of defects

• Extended models for more complex shapes

• Improved process monitoring and error prediction

• Improve process accuracy at smaller length scales

• Integrated machining

• Commercial software

• Commercial hardware

• Turn-key operation

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AM Scientific Challenges• Predict temperature and stress fields

• Influence of energy source• Influence of fluid flow

• Predict and control microstructures• Multiple heating and cooling cycles

• On the basis of the microstructure and thermal-mechanical history, predict mechanical properties

• Build the predictions into the optimisation models to determine build process, strategy etc.

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Offer a new materials-centric approach to additive manufacturing, focusing on large-scale components

Integrate design, microstructure and material properties through physically based models, delivering a unique capability to produce properties on demand

Provide the fundamental knowledge necessary for development and exploitation at the large scale

Additive Manufacturing for Extra Large Components (AiM2XL)

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Controlled and Graded Microstructures

BD

=2000 µm; Map6; Step = 5 µm; Grid1849x129

Zone 2: 950 WCoarse grain

Inconel 718 – laser powder deposition

Popovich et al. 2017

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The AiM2XL Programme

Project 1: Microstructure based topology optimisation for additive manufacturing of very large metal components (1PhD+2PDEng)

prof. van Keulen, TUD

Project 5: Sensing and adaptive Control for quality assurance during large scale additive manufacturingof metal components (1PhD+2PDEng)

RL1

Microstructure-properties relationship

RL3Microstructure prediction and

control

RL2

RL1Topology and

process optimization

prof. Römer, U. Twente

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The AiM2XL Programme

Project 3: Microstructure prediction and composition control for the development of tailored properties in additively manufact-ured metallic components (2PhD+1 PDEng)

dr. Hermans, TUD

Project 4: Local and global scale prediction and control of residual stresses and distortion in additively manufactured components (2PhD)

RL2

Microstructure-properties relationship

RL3Microstructure prediction and

control

RL2

RL1Topology and

process optimization

prof. van den Boogaard, U. Twente

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The AiM2XL Programme

Project 2: From structure to properties for large-scale additive manufacturing by wire deposition (2PhD)

prof. Geers, TUE

Project 6: From structure to Properties for large-scale additive manufacturing by powder deposition(1PD)

prof. Pei, U. Groningen

RL3

Microstructure-properties relationship

RL3Microstructure prediction and

control

RL2

RL1Topology and

process optimization

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Fast reeving socket

Marine rudder

Tailhook

Dem

onst

rato

rs

Exploitation

Prod

ucts

Basi

c re

sear

ch

PDEng + Researchers at RAMLAB

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Thank you for your attention!

Questions?

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AiM2XL

1. Properties on demand

Account for path, speed and power variations at the design optimisation stage

Develop optimisation strategies for multiple criteria, including process flow and post processing treatments

2. Topology optimization

Control properties by adapting thermal-mechanical conditions

3. Enhance local microstructures

and properties 4. Tailor graded microstructures

Develop gradient deposition conditions (composition / properties) to avoid sharp interfaces

Scientific Challenges

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AiM2XL

5. Control stress and distortionModel the influence of large numbers of heating/cooling cycles on thermal history and work hardening throughout a component

Establish adaptive closed loop process control to realise on-line product quality control

6. Adaptive closed loop process

control

Develop orientation-dependent strength and fracture behaviour models

7. Investigate material and

component properties

8 Demonstrators

Produce demonstators to explore the accuracy of model predictions

Scientific Challenges

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WAAM - Process features (1)Inclined torch (CMT)

Angled and horizontal walls

Straight near net shape Ti

thin wall

Machined intersections

Medium complexity 2D part

Weight efficient structure

With mixed materials

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Images courtesy Cranfield University

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WAAM Example part - Titanium Spar• 1.2 m long, welded

titanium spar

• 37 hours from digital model to completed part

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Images courtesy Cranfield University

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WAAM - Example part - Landing gear rib

Before(kg)

After(kg)

Buy-to-fly

Waste

Machining 240 21 11.6 91%

AM 24 21 1.15 13%

Deposition time - 24 hoursTitanium

Steel

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Images courtesy Cranfield University

4242

Additive Manufacturing Met. & Mater. Trans. A, [1073-5623] 44A(2), 968 -977, 2013. Courtesy Cranfield University & UMIST

Titanium deposit

No mechanical deformation

75 kNmechanical deformation

Images courtesy Cranfield University

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-300

-200

-100

0

100

200

300

400

500

-5 0 5 10 15 20 25 30 35 40 45

Long

itudi

nal s

tress

(MPa

)

Distance from top of baseplate (mm)

Contour Method Neutron Diffraction

Residual Stresses

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Courtesy Cranfield University

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Fatigue crack growth rate (Ti alloy)

1x10-9

1x10-8

1x10-7

1x10-6

1x10-5

1x10-4

1 10 100

da/d

n (m

m/c

ycle

)

∆K (MPa √m)

NASA

Control H1

Control H2

Control V1

Control V2

Rolled H1

Rolled H2

Rolled V1

Rolled V2

• Rolling has no negative influence on damage tolerance

• Fatigue crack growth rate is isotropic

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Courtesy Cranfield University

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Additive Manufacturing - challengesAM construction is currently process driven and many

limitations exist, including:

Porosity Control

High Residual Stresses

Excessive Distortion

Poor Repeatability

Lack of Predictability

Lack of Reliable Property Control

Variable Process Stability

Lack of Feedstock homogeneity

Absence of Process – Property Models

Difficulties with Up-scaling

Anisotropy

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Courtesy: DAMEN & RAMLAB

WAAMpeller Project