Additive Manufacturing is used in a wide range of industries. Since its origins as a prototyping technology in the 80s it has come a long way. Today, applications can be found across the entire value chain, from prototyping to spare parts and repair.
We want to give a brief overview of the benefits of using AM in different areas, followed by one case study for each of these areas.
The use of AM for prototyping during the product development phase is the oldest and most widely used area. While especially low-cost technologies such as stereolithography or extrusion processes are often used for prototyping, basically every technology can be used. Depending on the development stage, prototyping includes simple visual models but also functional prototypes, e.g. for flow testing.
The possibility to quickly produce designs with no need for tooling can save significant time and cost during the development of new components.
The application areas for AM within tooling are diverse. These include pressing and forming tools produced in metal, injection moulding tools with optimized conformal cooling channels, or simple jigs & fixtures that are used during the assembly process.
Besides the design freedom of AM, advantages usually include the cost-effective production of parts in low volumes and short leadtimes.
Over the last years, Additive Manufacturing has developed from a tool that was mostly used for prototyping to a manufacturing technology for end use applications in almost all industries.
While many companies aim at using AM to reduce manufacturing costs, the biggest potential can be realized when completely redesigning a product for its function. The design freedom can then significantly improve the performance of a part.
Additive Manufacturing enables the production of spare parts in small quantities and are a great fit for the technology.
Some of the advantages of using AM are shorter leadtimes, reduced need for keeping parts on stock and no need for tooling. At the same time, the qualification process for spare parts is often less demanding than for serial applications.
Instead of simply building entirely new components from scratch, AM can be used to repair and build upon existing components. While there are some cases of companies realizing repair applications with Powder Bed Fusion technologies, Directed Energy Deposition (DED) enables the easy application of material on existing parts.
This offers great potential to reduce costs and shorten lead times. At the same time, repairing components reduces waste and helps companies improve their carbon footprint.
This case study by GE AVIATION shows how they are using AM to completely rethink their turboprop engine. Some of the benefits they hope to achieve are 20% increased fuel efficiency, 33% time increase between overhauls, and a more stable performance. Using AM, they could combine over 800 individual parts into 12 components.
The objective was to completely re-design an advanced turboprop (ATP) engine using the full potential of Additive Manufacturing.
The goal was to increase the performance of the engine and reduce the number of components while maintaining a short design- and production lead time.
The engine has been completely re-designed from a blank sheet of paper. Additive Manufacturing was used as a main production technology and could be used to create parts that were otherwise impossible to produce.
The engine is produced using several AM technologies, among them metal Laser Powder Bed Fusion (L-PBF) and Directed Energy Deposition (DED).
“The uniqueness of Additive is, as we went through this engine we took about 800+ parts and distilled it down to 12 parts.”
Paul Corkery | GE ATP Program | GENERAL ELECTRIC
Video courtesy of www.Avweb.com. Filmed in 2017.
With the increase of robots in manufacture and assembly lines, the production of grippers is on the rise. Production lines need to be as flexible as possible and changes, e.g. for maintenance, must be performed as quickly as possible.
In this case the goal is to completely eliminate assembly operations and to ensure quick changes of gripping fingers during maintenance.
The gripper should be produced in a flexible material to enable the gripping mechanism and should withstand a sufficient amount of gripping operations.
While grippers can be produced with a range of AM technologies we present 2 different grippers produced with a ME printer by the French company POLLEN AM.
The first design is a suction cup that is produced in one component in a very low hardness TPE. The material used is airtight and can be manufactured in one part.
The second part is a gripping finger that has been printed in two materials – ABS for toughness and TPU 33 Shore D to ensure flexibility.
Both parts were printed in an extrusion printer from pellets that are typically used for injection molding.
Weight reduction is one of the main drivers for the use of Additive Manufacturing within aviation. The hydraulic manifold, which was produced by LIEBHERR AEROSPACE for an AIRBUS A380 is a great example for this.
The objective was to replace a conventionally manufactured high-pressure hydraulic valve block with an additively manufactured one. The component is produced by LIEBHERR AEROSPACE.
The primary flight control component moves the spoiler of an AIRBUS A380 aircraft to the desired position during take-off and landing and must thus meet highest quality standards.
The original component is machined from a forged block with several drillings and assembly operations. This leads to limited design freedom and long lead times.
The design was optimized based on the installation space and the goal to keep short connections to interfaces. Material was then only added where necessary, resulting in 35% less weight.
The part was produced on an EOS M290 in titanium. After printing, a heat treatment as well as a treatment of the internal channels was performed.
The printed part fulfilled all certification requirements and has been successfully used on a test flight of the AIRBUS A380 aircraft.
“A couple of years from now, we believe that metal 3D-printed parts such as the valve block will be manufactured in series at Lieberr- Aerospace and delivered to our customers.”
Alexander Altmann | Lead Engineer Additive Manufacturing, Research & Technology | LIEBHERR AEROSPACE LINDENBERG
Source: EOS
Further information on the case study can be found here.
EVOBUS, a subsidiary of the DAIMLER GROUP, sees increasing challenges in the field of spare parts for their buses. The company’s increasing product portfolio results in over 320,000 spare parts and thus high costs for warehousing and logistics as well as long lead times. In addition, minimum purchase volumes lead to overproduction and often to obsolete parts.
The biggest initial potential for Additive Manufacturing has been identified within polymer components in the interior of the buses.
Several spare parts such as covers and armrests from the interior of the bus have been identified as suitable components for Additive Manufacturing. To imitate the surface of the conventionally produced parts, a textured surface was applied during the printing process. After printing, the parts have been colored in a dyeing process and blasted to create a smoother surface.
Selected parts have been produced in Polyamide 12. The majority of components, however, requires a specific flame-resistant material that has to be authorized for the usage in buses.
“By implementing 3D printing within our CSP business model, we hope to reduce the rising warehousing and tool costs caused by our growing inventory of omnibus spare parts, while also continuing to improve supply performance to our end customers”
Ralf Anderhofstadt, Head of Center of Competence 3D-Printing, DAIMLER BUSES
Source: EOS
Further information on the case study can be found here.
Directed Energy Deposition (DED) technologies, such as Laser Metal Deposition (LMD), are already a mature technology in several industries. Expensive components with high production costs can easily be repaired, meaning that the part or tool is back in use in a short time.
This way, companies not only save time due to long delivery times, but also cost. This is due to the fact that it is usually more cost effective to repair a component than to buy a new one when it comes to expensive materials such as nickel-based alloys. Design changes can also be made on the component.
DED thus allows end users to reduce repair time, save costs and improve the carbon footprint by repairing worn out components instead of producing a new part.
Expensive components, such as compressor seals for gas turbines, are costly to produce and usually come with long lead times. These long lead times are especially costly when a product can not be used during a downtime.
The part on the right is a seal in a gas turbine produced in Inconel 718. Already very low amounts of wear on the edges results in scrap of the entire part.
DED technologies such as Laser Metal Deposition (LMD) can be used to repair worn out components.
The part has been repaired using the LENS technology by OPTOMEC. The repair deposit caused a minor shrinkage of the inside diameters that were subsequently machined to print tolerances. The repaired tool was accepted by the customer. In this example, the cost for the repair was about 45% compared to replacement with a new part.
The sinter-based AM (SBAM) technologies have, as the name suggests, the sintering process in common. In this process, the printed green part is consolidated into a dense part and receives its final properties. The green part can be printed in advance using different technologies.They all have in common that metal powder is bound to the desired shape by a binder. The best-known printing technologies include Binder Jetting and Filament Material Extrusion.
In this section, you learn everything about the sinter-based AM process chain and get an overview of the different printing technologies.
This course is aimed at engineers, designers and other professionals that are working closely with sinter-based AM technologies. The goal is to cover the most important aspects that will enable engineers and designers to fully grasp the capabilities and technical limitations of the printing technologies and the sintering process to succeed in technology selection and part design. Besides going through the course from the beginning until the end, this course can also act as a constant source of knowledge while working on AM projects.
The course is structured into the following sections.
This section will start with an overview of the sinter-based AM process chain and its printing technologies, followed by a technology deep dive into the most important aspects of the BJT technology, followed by a closer look at the debinding and sintering step also including sintering simulation .
The second section will provide an overview of the different materials that are available as well as part characteristics that can be achieved with the BJT process and typical methods for quality assurance. Finally, several common defects in the BJT process are presented.
The last section will act as a guideline for designers. Besides generally describing the process when designing for Additive Manufacturing, actionable restrictions and guidelines for the BJT process are provided. The final section will present several design examples from different industries.
Simulation to compensate the deformation during the sintering step, nesting of parts and definition of printing parameters
Through various printing processes, different feedstocks such as metal powders, filaments, pellets or dispersions are processed into green parts
Unpacking of fragile green parts needs to be done carefully and is typically a manual process.
Debinding describes the process of removing the binder which results in a brown part
To reach the structural integrity of a metal part, a sinter process is required. The powder particles fuse together to a coherent, solid structure via a mass transport that occurs at the atomic scale driven via diffusional forces.
The brown part shrinks ~13-21 % in each direction.
The process chain of sinter-based technologies differs from other AM Technologies. Especially the post-printing processes (debinding and sintering) are crucial to achieve the intended mechanical properties.
Binder Jetting is a powder based Additive Manufacturing technology in which a liquid polymer binder is selectively deposited onto the powder bed binding the metal particles and forming a green body.
The metal powder is applied to a build platform in a typical layer thickness of 40 µm to 100 µm. Subsequently a modified 2D print head apply a binder selectively onto the powder bed. Depending on machine technology a hardening or curing process of the binder is performed in parallel for each layer and/or at the end of the whole build. During the in-situ curing process a heat source is used to solidify the binder and form a solid polymer – metal powder composite.
Afterwards the build platform moves downward by the amount of one layer thickness and a new layer of powder is applied. Again, the liquid binder is deposited and hardened in the required regions of the next layer to form the green body. This process is repeated until the complete part is printed. After the complete printing process is finished the parts have to be removed from the “powder cake” meaning the surrounding loose but densified powder. To improve the removal of the excess powder from the green body often brushes or a blasting gun with air pressure are used.
To create a dense metal part the 3D printed green body has to be post-processed in a debinding and sintering process. Similar to the metal injection molding process BJT parts are placed in a high temperature furnace, where the binder is burnt out and the remaining metal particles are sintered together. The sintering results in densification of the 3D printed green body to a metal part with high densities of 97 % to 99,5%, dependent of the material.
In classic Binder Jetting systems such as the ones distributed by EXONE or DIGITAL METAL the liquid binding agent is selectively deposited with a single print head. Meaning the width of the print head does not cover the full width of the powder bed. Therefore, the print head moves multiple times in xy-direction over the powder bed to completely cover the printing area and distributing the polymer binder.
The SINGLE PASS JETTING technology was developed by DESKTOP METAL and HEWLETT PACKARD. The width of the printing head covers the full width of the powder bed. When the printhead passes over the powder bed, binder is released from more than 30,000 small nozzles and the whole powder layer is selectively immersed in binder in one pass. The process is bi-directional which means that the binder deposition takes place in both moving directions of the printhead. With these modifications the printing speed is significantly increased.
A similarly fast technology is the METAL JET process by HEWLETT PACKARD. In a single pass, a liquid printing agent is applied to the powder layer and subsequently partially evaporated to form the binding polymer around the metal powder. After the completion of the print an additional curing to achieve the full green body stability is needed.
3DEO combines the Binder Jetting process with a subsequent machining process. Different from conventional Binder Jetting processes, the binder is not only deposited selectively but onto the entire powder layer. After hardening of the complete layer, the part geometry is shaped through a milling process every couple of layers by cutting the part contour out of the binder powder composite.
Binder Jetting is a powder based Additive Manufacturing technology in which a liquid polymer binder is selectively deposited onto the powder bed binding the metal particles and forming a green body.
The metal powder is applied to a build platform in a typical layer thickness of 40 µm to 100 µm. Subsequently a modified 2D print head apply a binder selectively onto the powder bed. Depending on machine technology a hardening or curing process of the binder is performed in parallel for each layer and/or at the end of the whole build. During the in-situ curing process a heat source is used to solidify the binder and form a solid polymer – metal powder composite.
Binder Jetting is a powder based Additive Manufacturing technology in which a liquid polymer binder is selectively deposited onto the powder bed binding the metal particles and forming a green body.
The metal powder is applied to a build platform in a typical layer thickness of 40 µm to 100 µm. Subsequently a modified 2D print head apply a binder selectively onto the powder bed. Depending on machine technology a hardening or curing process of the binder is performed in parallel for each layer and/or at the end of the whole build. During the in-situ curing process a heat source is used to solidify the binder and form a solid polymer – metal powder composite.
Binder Jetting is a powder based Additive Manufacturing technology in which a liquid polymer binder is selectively deposited onto the powder bed binding the metal particles and forming a green body.
The metal powder is applied to a build platform in a typical layer thickness of 40 µm to 100 µm. Subsequently a modified 2D print head apply a binder selectively onto the powder bed. Depending on machine technology a hardening or curing process of the binder is performed in parallel for each layer and/or at the end of the whole build. During the in-situ curing process a heat source is used to solidify the binder and form a solid polymer – metal powder composite.
Binder Jetting is a powder based Additive Manufacturing technology in which a liquid polymer binder is selectively deposited onto the powder bed binding the metal particles and forming a green body.
The metal powder is applied to a build platform in a typical layer thickness of 40 µm to 100 µm. Subsequently a modified 2D print head apply a binder selectively onto the powder bed. Depending on machine technology a hardening or curing process of the binder is performed in parallel for each layer and/or at the end of the whole build. During the in-situ curing process a heat source is used to solidify the binder and form a solid polymer – metal powder composite.