Additive Manufacturing for Repair and Restoration in Remanufacturing: An Overview from Object Design and Systems Perspectives
Abstract
:1. Introduction
2. Systematic Literature Review
Application of Screening Criteria
3. Results and Discussion
3.1. Bibliographic Analysis and Type of Industry
3.2. Focus of Previous Study
3.2.1. AM Technology for Repair and Restoration
3.2.2. Product or Object Material
3.2.3. AM Material
3.2.4. AM Machine Setting
3.2.5. Geometrical Complexity of Product
3.2.6. Pre-Processing
3.2.7. Engineering Tolerance
3.2.8. Material Compatibility
4. Conclusions
Author Contributions
Funding
Acknowledgments
Conflicts of Interest
References
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Producers | Output Value (in USD) |
---|---|
Japan [23] | 4,800,000,000 |
United Kingdom [13] | 7,280,000,000 |
USA [24] | 75,000,000,000 |
American Standard Testing and Materials (ASTM) Category | Basic Principles | Example of AM Technology |
---|---|---|
Binder Jetting (BJ) | Liquid printing binder deployed onto specific coordinate layer-by-layer of material powder that sticks at the particle until it becomes a 3D object. | 3D inkjet technology |
Direct Energy Deposition (DED) | Deposition of powder material coincides with focused thermal energy to melt it through the targeted spot. | Electron Beam Laser Engineered Net Shaping (LENS) Plasma Arc Melting Laser cladding (LC) |
Material Extrusion (ME) | Precipitation of build materials droplets through a heated nozzle. | 3D inkjet technology Fused Deposition Modeling (FDM) |
Powder Bed Fusion (PBF) | The fusion of a specific coordinate in a small region of the powder bed of the build material using focused thermal energy | Direct Metal Laser Sintering (DMLS) Electron beam melting (EBM) Selective Laser Sintering/Melting (SLS/SLM) |
Sheet Lamination (SE) | Attachment of sheets/foils of materials. | Ultrasound consolidation/Ultrasound Additive Manufacturing (UC/UAM) Laminated Object Manufacturing (LOM) |
Vat Photo Polymerization (VP) | Focused light-curing towards liquid polymer in a vat | Digital Light Processing (DLP) Stereo Lithography (SLA) |
Cold Spray | Injected powder at high velocity to build-up material, caused by adhesion | Multi-Metal Deposition |
Issues in AM Restoration | Research Questions |
---|---|
How does AM technology conduct repair and restoration? | What are the recommendations for effective repair and restoration using AM technology from an object design and systems perspective? |
Bibliographic Data and Field of Industry | ||
Author | Who is the author of the publication? | Xu Lei, Cao Huajun, Liu Hailong, Zhang Yubo |
Year | In what year is the work issued? | 2016 |
Title | What is the title of the publication? | Study on laser cladding remanufacturing process with FeCrNiCu alloy powder for thin-wall impeller blade. |
Type of Publication | What kind of publication? | Journal |
Name of Publication | What is the name of journal/proceeding/book/report? | International Journal of Advanced Manufacturing Technology |
Field of Industry | What is the industrial field categorizing the product? | Marine and offshore |
Focus and Content of the Publication | ||
AM technology Determination | Which AM technology is used in this study, according to the object of restoration? | Laser Cladding (DED) |
Motivation | What is the reason for conducting the study? | To conduct restoration on the thin wall of a centrifugal compressor impeller. |
Goal | What is the goal of the study? | To ascertain the use of FeCrNiCu alloy powder in the restoration process |
Product or object material | What is the material of the restored product and AM? | Metal-based product and FeCrNiCu alloy powder |
AM machine setting | What is the AM machine setting used in this study? | 4 axis robotic arm to aid the extrusion process 4 kW laser −140~+320 mesh size of powder material 5 mm/s laser speed 8.0 g/min powder feed rate 3 mm laser spot diameter 150 L/h carrier flow |
Geometrical complexity | What is the geometrical complexity of the restored object? | Impeller blade has a thin wall, which limits the optimization of the LC scanning path. |
Pre-processing | What is the pre-processing of the restoration process preparation? | This experiment uses ANSYS software as a simulated heat source, Pro/E software as 3D-remanufactured impeller model builder. |
Engineering Tolerance | What is the geometric tolerance of the restoration process? | 1.5 mm. |
Material compatibility | How was the material compatibility of the restoration process? | The AM material was compatible to be used to repair the object material |
Repaired Object | AM Technology | Focus of Study and Repair |
---|---|---|
Turbine Blade of Aircraft component [64] | Laser Energy Deposition (DED) | A geometric reconstruction algorithm for repairing turbine airfoils. |
Gas Turbine Blade of Power Plant [65] | Laser Aided Additive Manufacturing (DED) | Analysis of a restoration process using Laser Aided AM onto turbine blade knife edges. |
Sprocket Mining [66] | Laser Cladding (DED) | Ascertaining the optimum process parameters of LC for sprocket reparation. |
Automotive Die [67] | Laser Cladding (DED) | Studying the effect of material on the heat treatment of Vanadis Extra 4. |
Steam Turbine Rotor of Power Plant [68] | Laser Cladding (DED) | Analyzing the effect of different widths of LC on the Total Indicated Runout. |
Crankshaft of Marine Engine [60] | Laser Cladding (DED) | Comparison between uncladded and cladded flat specimens towards crankpin journal surface. |
Yoke plate Cylinder Guide [30] | FDM | Analysis of specific strategies for Maintenance Repair Overhaul optimization. |
Sprocket Mining [66] | Laser Cladding (DED) | Application of the LC process in sprocket restoration. |
Aerospace [28] | Laser Metal Deposition (DED) | Analysis of appropriate geometries towards the remanufacturing process. |
Marine [27] | Laser Cladding (DED) | Constructing the system for onboard reparation using LC on the engine housing of marine. |
Aerospace [69] | Laser Cladding (DED) | Analysis of fatigue and fracture of AerMet 100 powder application for LC repair process. |
Railways [70] | Laser Cladding (DED) | Analysis of the wear and Rolling Contact Fatigue (RCF) performance of the LC process for rail applications. |
Aircraft [71] | Scanning Laser Epitaxy (DED) | Development of a model for melting and solidification of EQ Alloy IN100 in Scanning Laser Epitaxy. |
Railways [72] | Laser Cladding (DED) | Analysis of surface coating for R260 rail steel. |
Industrial Gas Turbine Burner [73] | PBF | Analysis of the environmental impact of the reparation process using PBF for gas turbine burner. |
Repaired Object | AM Technology | Additive Material |
---|---|---|
Composite materials [32] | DED | Ti6Al4V |
Die [82] | DED | Inconel 625 |
Steam turbine rotor [68] | DED | Stainless Steel |
AISI 1045 steel rod bar [83] | DED | Cr–Ni alloy |
Centrifugal compressor impeller [79] | DED | FeCrNiCu Alloy |
Sprocket [66] | DED | AISI 4140 & Fe based powder |
Aerospace component [69] | DED | AerMet Powder |
Gas turbine burner [28] | DED | Nickel-based alloy Inconel 718 |
Cylinder’s guide yoke plate [30] | FDM | Polylactic Acid (PLA) |
Ti6Al4V based aero engine blade material [84] | DED | Ti6AlV |
Turbine blade [64] | DED | Stainless Steel 316 L powder |
Rails [72] | DED | Stellite 6 powder |
Cast iron and low carbon steel [85] | DED | Metco 15 E Colmony 88 VIM CRU 20 |
Author | AM Technology | Additive Material | AM Machine Setting |
---|---|---|---|
Zhang et al. [88] | DED | Inconel 625 | Laser power: 600 W Scan speed: 220 mm/min Powder feed rate: 4 g/min |
Guo et al. [68] | DED | Stainless Steel | Laser power: 1800 W Laser spot diameter: 4 mm Powder feed rate: 10 g/min |
Zhang and Liu [89] | DED | Cr–Ni alloy | Laser power: 3000 W Scan speed: 5.1 mm/s Powder feed rate: 450 g/min |
Lei et al. [79] | DED | FeCrNiCu Alloy | Laser power: 1100 W Powder size: −140∼+320 mesh Scan speed: 5 mm/s Powder feed rate: 8 g/min Laser spot diameter: 3 mm Carrier flow: 150 L |
Liu et al. [66] | DED | AISI 4140 & Fe based powder | Laser power: 1000–2000 W Powder feed rate: 2.21–2.81 g/min Scanning speed: 800–1200 mm/min |
Lourenço et al. [69] | DED | AerMet Powder | Laser power: 800 W Laser spot size: 1.3 mm Powder flow rate: 5.15 g/min |
Petrat et al. [28] | DED | Nickel-base alloy Inconel 718 | Laser power: 800–1600 W Spot diameter: 1–2.2 mm Powder flow rate: 5–15 g/min |
Wits et al. [30] | FDM | Polylactic Acid (PLA) | Ultimaker machine Heated bed & nozzle: 2.85 mm Heat: 210 °C Print speed: 50 mm/s |
Raju et al. [84] | DED | Ti6AlV | Laser power: 1500 W Scan speed: 600 mm/min Powder size: 45–100 μm Spot diameter: 2 mm |
Wilson et al. [64] | DED | Stainless Steel 316L powder | Laser carrier: Optomec LENS® 750 Laser power: 500 W Powder size: 44 μm |
Clare et al. [72] | DED | Stellite 6 powder | Laser power: 1600 W Powder flow rate: 0.25–0.5 g/s |
Lestan et al. [85] | DED | Metco 15 E Colmony 88 VIM CRU 20 | Laser carrier: Optomec LENS 850-R Laser power: 360–400 W Laser spot diameter: 0.8 mm Powder feed rate: 3.5–3.8 g/min |
Repaired Object | Geometrical Complexity |
---|---|
Manufacturing Die [88] | Reconstructing the convex chipped part at the edge of the die. |
Turbine Blade of Aircraft component [64] | Reconstructing the chipped part of the blade tip. |
Gas Turbine Blade of Power Plant [65] | Building up a thin wall of the turbine blade. |
Sprocket Mining [66] | Reconstructing a sprocket tooth of the conveyor. |
Manufacturing Die [74] | Overlaying the surface of a die. |
Automotive Die [67] | Surface coating of die (surface was machined before laser treatment). |
Steam Turbine Rotor of Power Plant [68] | The curved surface of the shaft. |
Crankshaft of Marine engine [60] | Overlaying the surface of the marine crankshaft. |
Yoke plate Cylinder Guide [92] | Rebuilding yoke plate using FDM machine. |
Aerospace [28] | A hollow cylinder of gas turbine burner with varies thickness between 7.20 and 7.34 mm. |
Marine [27] | Overlay wearing in the surface of the crankshaft. |
Industrial Gas Turbine Burner [73] | A hollow cylinder of gas turbine burner. |
Repaired Object | Challenge of Repair Process |
---|---|
Sprocket Mining [66] | The optimum parameter of LC machine should be determined to obtain the optimum result of repair |
Aerospace [69] | The use of ultra-high-strength steels in aircraft, which is susceptible to fatigue resulting in brittle fracture, must be repaired using the appropriate material powder for LC repair |
Aerospace [28] | Finding the optimum parameter of LC to build three different single hollow cylinders with varying wall thicknesses |
Marine [27] | Building an onboard LC repair tool |
Industrial Gas Turbine Burner [73] | Determining the precise location of the object for repair using the LBM machine |
Manufacturing Die [88] | Building a reconstruction algorithm to model worn out parts for LC repair process. |
Gas Turbine Blade of Power Plant [65] | Finding the appropriate heat input for the deposition of Laser Aided Additive Manufacturing to avoid crack after process completion |
Sprocket Mining [66] | Ascertaining the different parameters of the LC machine (i.e., laser power, scanning speed, and powder feed rate) as they affect surface profile characteristics, microstructure, and micro-hardness |
Manufacturing Die [74] | Analyzing the optimum laser power towards CPM powder burst on H13 tool steel. |
Automotive Die [67] | Determining the appropriate choice of CPM 10V and Vanadis 4 Extra steel powder deposited into heat-treated Vanadis 4 plate |
Steam Turbine Rotor of Power Plant [68] | Determining the optimum diameter and laser cladding width to solve wear reparation. |
Yoke plate Cylinder Guide [92] | Constructing the appropriate process flow for MRO strategies. |
© 2019 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).
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Rahito; Wahab, D.A.; Azman, A.H. Additive Manufacturing for Repair and Restoration in Remanufacturing: An Overview from Object Design and Systems Perspectives. Processes 2019, 7, 802. https://doi.org/10.3390/pr7110802
Rahito, Wahab DA, Azman AH. Additive Manufacturing for Repair and Restoration in Remanufacturing: An Overview from Object Design and Systems Perspectives. Processes. 2019; 7(11):802. https://doi.org/10.3390/pr7110802
Chicago/Turabian StyleRahito, D. A. Wahab, and A. H. Azman. 2019. "Additive Manufacturing for Repair and Restoration in Remanufacturing: An Overview from Object Design and Systems Perspectives" Processes 7, no. 11: 802. https://doi.org/10.3390/pr7110802