UROP- Annealed 3D printed parts- Final Write up Michael Rosplock Abstract



Similar documents
Tensile Testing Laboratory

Objectives. Experimentally determine the yield strength, tensile strength, and modules of elasticity and ductility of given materials.

TENSILE TESTING PRACTICAL

Investigating Methods of Prototyping with ABS

METU DEPARTMENT OF METALLURGICAL AND MATERIALS ENGINEERING

M n = (DP)m = (25,000)( g/mol) = 2.60! 10 6 g/mol

Tensile Testing of Steel

Objective To conduct Charpy V-notch impact test and determine the ductile-brittle transition temperature of steels.

CH 6: Fatigue Failure Resulting from Variable Loading

Uniaxial Tension and Compression Testing of Materials. Nikita Khlystov Daniel Lizardo Keisuke Matsushita Jennie Zheng

PROPERTIES OF MATERIALS

LABORATORY EXPERIMENTS TESTING OF MATERIALS

SD-0150 GENERAL PURPOSE ABS (Acrylonitrile Butadiene Styrene) (TA)

3D PRINTING OF CONTINUOUS FIBER REINFORCED PLASTIC

Stress Strain Relationships

The mechanical properties of metal affected by heat treatment are:

HW 10. = 3.3 GPa (483,000 psi)

Modern Construction Materials Prof. Ravindra Gettu Department of Civil Engineering Indian Institute of Technology, Madras

Description of mechanical properties

Strengthening. Mechanisms of strengthening in single-phase metals: grain-size reduction solid-solution alloying strain hardening

Solution for Homework #1

CERAMICS: Properties 2

Experiment: Fatigue Testing

3. Test Methods for Evaluation of ESCR of Plastics

Unit 6: EXTRUSION. Difficult to form metals like stainless steels, nickel based alloys and high temperature metals can also be extruded.

ENZYME KINETICS ENZYME-SUBSTRATE PRODUCTS

Chapter Outline Dislocations and Strengthening Mechanisms

Sample Feasibility Study XYZ Company Widget Part Design

North American Stainless

ME 612 Metal Forming and Theory of Plasticity. 3. Work Hardening Models

MIME 3330 Mechanics Laboratory LAB 5: ROTATING BENDING FATIGUE

ATI 2205 ATI Technical Data Sheet. Duplex Stainless Steel GENERAL PROPERTIES. (UNS S31803 and S32205)

Chapter Outline Dislocations and Strengthening Mechanisms

Impact testing ACTIVITY BRIEF

Case Neck Annealing Kit

Mechanical Properties of Metals Mechanical Properties refers to the behavior of material when external forces are applied

CALCULATIONS & STATISTICS

University of Portland School of Engineering LABORATORY OUTLINE: TENSILE TESTING OF STEEL & ALUMINUM ALLOYS (ASTM E8)

Environmental Stress Crack Resistance of Polyethylene Pipe Materials

Naue GmbH&Co.KG. Quality Control and. Quality Assurance. Manual. For Geomembranes

TIE-31: Mechanical and thermal properties of optical glass

Master of Simulation Techniques. Lecture No.5. Blanking. Blanking. Fine

CHAPTER 7 DISLOCATIONS AND STRENGTHENING MECHANISMS PROBLEM SOLUTIONS

CHARACTERIZATION OF POLYMERS BY TMA. W.J. Sichina, National Marketing Manager

AMPLITUDE AND FORCE PROFILING: STUDIES IN ULTRASONIC WELDING OF THERMOPLASTICS

TA INSTRUMENTS DIFFERENTIAL SCANNING CALORIMETER (DSC) Insert Nickname Here. Operating Instructions

LAB 6: GRAVITATIONAL AND PASSIVE FORCES

AUSTENITIC STAINLESS DAMASCENE STEEL

TECHNICAL BULLETIN TECHNICAL DESCRIPTION DESCRIPTION OVERVIEW PROGRAMS. Data Sheet. Pilkington Toughened Safety Glass

CORRELATION BETWEEN HARDNESS AND TENSILE PROPERTIES IN ULTRA-HIGH STRENGTH DUAL PHASE STEELS SHORT COMMUNICATION

Mechanical Properties and Fracture Analysis of Glass. David Dutt Chromaglass, Inc.

INJECTION MOLDING COOLING TIME REDUCTION AND THERMAL STRESS ANALYSIS

MEASURES OF VARIATION

Printrbot Getting Started Guide. For models: Printrbot Plus (v2) Printrbot LC (v2) Printrbot jr

Introduction to Solid Modeling Using SolidWorks 2012 SolidWorks Simulation Tutorial Page 1

ME 354, MECHANICS OF MATERIALS LABORATORY

Solid Mechanics. Stress. What you ll learn: Motivation

April Report Prepared By: Phil Brindley, Dr Ruth Goodridge, Mark East & Prof Richard Hague Loughborough University, Loughborough, UK

Injection molding equipment

4 Thermomechanical Analysis (TMA)

North American Stainless

Whether plastic, rubber, wood, metal or ceramic,

different levels, also called repeated, alternating, or fluctuating stresses.

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA MECHANICAL PRINCIPLES OUTCOME 2 ENGINEERING COMPONENTS TUTORIAL 1 STRUCTURAL MEMBERS

Effect of Temperature and Aging Time on 2024 Aluminum Behavior

2(H 2 O 2 ) catalase 2H 2 O + O 2

Developments in Low Temperature Testing of Rubber Materials

TENSILE AND CREEP DATA OF 316L (N) STAINLESS STEEL ANALYSIS

9. TIME DEPENDENT BEHAVIOUR: CYCLIC FATIGUE

Fracture and strain rate behavior of airplane fuselage materials under blast loading

Figure 1: Typical S-N Curves

Experiment 1: Colligative Properties

FATIGUE CONSIDERATION IN DESIGN

PIEZOELECTRIC FILMS TECHNICAL INFORMATION

LAB 6 - GRAVITATIONAL AND PASSIVE FORCES

A Guide to Thermoform Processing of Polypropylene. Introduction

Statgraphics Getting started

Fatigue. 3. Final fracture (rough zone) 1. Fatigue origin. 2. Beach marks (velvety zone)

TWISTING OF FIBRES IN YARNS FOR NATURAL FIBRE COMPOSITES

STRAIN-LIFE (e -N) APPROACH

Lecture 9: Annealing and Tempering

Sheet metal operations - Bending and related processes

T A B L E T 1 T E S T S A N D I N S P E C T I O N C A B L E P C U T A N D P C U T - A

Chapter Outline. Mechanical Properties of Metals How do metals respond to external loads?

X15TN TM. A high hardness, corrosion and fatigue resistance martensitic grade CONTINUOUS INNOVATION RESEARCH SERVICE.

Massachusetts Institute of Technology Department of Mechanical Engineering Cambridge, MA 02139

A Comparison of the Measured Magnetic Field Strength Using Ampere-Turns (AT) and millitesla (mt)

The Mechanical Properties of Glass

FEM analysis of the forming process of automotive suspension springs

MENG 302L Lab 1: Hardness Testing

Using Freezing-Point Depression to Find Molecular Weight

Materials Issues in Fatigue and Fracture

INFLUENCE OF THERMOMECHANICAL TREATMENT ON THE STEEL C45 FATIGUE PROPERTIES

SPECIFICATIONS, LOADS, AND METHODS OF DESIGN

Torsion Tests. Subjects of interest

Analytical Test Method Validation Report Template

KALPANA INDUSTRIES LTD. TECHNICAL DATA SHEET

Transcription:

UROP- Annealed 3D printed parts- Final Write up Michael Rosplock Abstract The purpose of this study was to examine the effects of a basic annealing process on 3D printed tensile test samples. Several different materials and annealing processes were used to determine the effect on the mechanical properties of 3D printed samples. With temperatures ranging from 170 to 200 F and times ranging from 10 to 60 minutes, over 100 samples were tested to create a large sample set. These samples were then tested in an Instron tensile testing machine to determine their tensile behavior. The overall results from the experiment showed very little affect from the annealing process, with an average increase close to 10% for tensile strength for ABS and about 5% for PLA. The change in the strain at failure showed a large amount of variation. The ABS samples displayed no real correlation for change in strain at failure. The PLA samples had a slight trend, leading to an average decrease of about 14% for the strain at failure. If anything the study showed that there is no real benefit to annealing 3D printed parts, and that they have a large variation in quality. Introduction After finding past research into the topic of annealing 3D printed parts, it seemed reasonable to study this topic even further with this UROP project. The basic idea behind annealing an object is to favorably change the mechanical properties of the material to better suit the needs of a design. In this case either stiffening or softening the part would have been desirable traits. Stiffer samples would lead to stronger but more brittle parts, which have application in some instances. Softening the part would have increased ductility while decreasing the overall tensile strength. This should lead to a tougher part that is less susceptible to fracture when dropped, repeatedly loaded, etc. This was the result that was originally predicted for the two materials tested. Method Two different materials were examined: PLA (polylactic acid) and ABS (acrylonitrile butadiene styrene). These materials were purchased from ProtoParadigm, an online 3D printing filament retailer. The printer used was a solidoodle 3 in stock configuration. The samples were a model of a flat dog bone designed to be 1x10mm in cross sectional area. The pull section was 75mm long with widened tabs for the jaws to clamp to.

The annealing process was carried out in an electric home oven. For this experiment, two temperatures (185 and 200F) and three lengths of time (10, 30, and 60 minutes) were chosen for the ABS samples. Due to the lower melt temperature of PLA, only one temperature was used (170F) with the same three time intervals used for the ABS samples. For each set, ten samples were tested, all going through the

exact same process. Ten samples were also created for each material that didn t undergo any treatment to act as control. All the samples were reviewed carefully before being selected to check for obvious flaws to deal with issues found in previous tests. The samples were placed onto a metal tray in the oven. Each set experienced a 3 minute ramp up period where the temperature increased linearly. After the annealing time, the oven was turned off and the samples were left to cool slowly in the oven for an hour. After the cool down time the samples were removed from the oven and labeled for testing. These samples were brought to the polymer research lab in Amundson Hall to be tested. An Instron testing machine was used to pull the samples at 10mm/min. Each sample was loaded identically into the machine. The stress versus strain curve was recorded into an excel spreadsheet for each sample. This data was then processed to determine the results of the study.

Results The data was from the tests was then placed into graphs showing stress vs. strain for each data set.

ABS Control

UTS (Mpa) Strain AB difference ABS control 2.8180 0.0761 UTS (Mpa) Strain AB ABS 10min 185F 3.0880 0.0687 0.2700-0.0074 ABS 10min 200F 3.1280 0.0619 0.3100-0.0142 ABS 30min 185F 3.0680 0.0567 0.2500-0.0194 ABS 30min 200F 3.0470 0.0701 0.2290-0.0060 ABS 60min 185F 3.1300 0.0634 0.3120-0.0127 ABS 60min 200F 2.7990 0.0808-0.0190 0.0047 percent change 185 strain 200 strain UTS (Mpa) Strain AB -9.69-18.69 9.58-9.69-25.51-7.85 11.00-18.69-16.64 6.14 8.87-25.51 185 strength 200 strength 8.13-7.85 9.58 11.00 11.07-16.64 8.87 8.13-0.67 6.14 8.13-0.67 Standard Dev. Samples UTS (Mpa) Percent SD Strain AB Percent SD ABS 10min 185F 0.2163 7.00 0.0239 34.83 ABS 10min 200F 0.1225 3.92 0.0163 26.34 ABS 30min 185F 0.1921 6.26 0.0107 18.94 ABS 30min 200F 0.2103 6.90 0.0236 33.69 ABS 60min 185F 0.2427 7.75 0.0160 25.25 ABS 60min 200F 0.2018 7.21 0.0119 14.69

UTS (Mpa) Strain AB difference percent change PLA control 5.205 0.0415 UTS (Mpa) Strain AB UTS (Mpa) Strain AB PLA 10min 170F 5.646 0.0367 0.4410-0.0048 7.8108-11.6358 PLA 30min 170F 5.447 0.0358 0.2420-0.0058 4.4428-13.8689 PLA 60min 170F 5.502 0.0349 0.2970-0.0066 5.3980-15.8516 Standard Dev. Samples UTS (Mpa) Percent SD Strain AB Percent SD PLA 10min 170F 0.2205 3.91 0.0019 5.11 PLA 30min 170F 0.2675 4.91 0.0016 4.38 PLA 60min 170F 0.4448 8.08 0.0027 7.62 Discussion As one can see from both the graphs and tables for ABS, there was a huge amount of variation within the data, especially when looking at the strain at break. Standard deviation was translated to percent to make better sense of the incredibly small number. With standard deviation units as high as 35% of the entire value for strain, it s nearly impossible to pull any reliable or meaningful data from these results, though there was a trend that the ductility decreased from the annealing process. While there was a huge amount of variation for the strain at break, the ultimate tensile strengths for the samples were relatively stable, leading to much more consistent data. In almost all cases, a slight increase in tensile strength (about 10% compared to the control group) resulted from all the annealing processes, except for the 60min at 200F samples which were outliers. There was no time dependence related to either tensile strength or strain at break as the data had no related trends. One strong conclusion that can be drawn from the ABS test is that the quality of the parts vary greatly. This could lead to issues when reliability between parts is required for a design. After processing the PLA data, an interesting change in consistency occurs. Instead of the huge variation seen in the ABS samples, the PLA sets actually have very consistent results. Unfortunately there were very small changes in tensile strength and strain when compared to the control set. Leading to an increase of about 5% in tensile strength with a 15% loss in strain at break. These results show that again, there is little value in annealing 3D printed samples, though it should be noted that PLA has more consistent mechanical properties compared to ABS. Conclusion After this extensive study into the effects of annealing on 3D printed parts mechanical properties, it has been found that there is little value in the process for any purpose. The properties simply didn t change that much after averaging the values over data sets of ten with temperature or length of annealing time. The most interesting part about the experiment was how varied the ABS samples were in general and how consistent the PLA samples were. With further testing this could lead

to the conclusion that ABS is a less stable printing material, yielding less consistent results compared to PLA. This could have a large effect on choice of material when consistency between pieces is required. One theory I came up with to explain the ineffectiveness of the annealing process is that since the part sits on a hot piece of glass in a relatively hot environment, the parts may already be annealed due to the printing process. After being printed for a long time in a hot environment the parts may be annealed to some extent. Making further processing unnecessary.