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OVERVIEW
Hollow,compositepartspresentauniquemanufacturingchallenge.
Cores are used to create the hollow features in composite
structures when smooth internal surface finish and seam-free
construction are required. Some cores can be easily removed
because of the part’s design geometry, but any configuration that
traps a core or mandrel inside it requires special, often sacrificial
tooling (Figure 1).
Typically, sacrificial cores are made from eutectic salt, ceramic or
urethane. These options present several challenges:
• Can limit part geometry
• Requires machined tooling to make
• Uses harsh removal procedures
• Difficult to handle, particularly fragile components
For these reasons, composites are more commonly laid up in
clamshell tooling. If there is sufficient access to the interior of a
closed clamshell tool, composite material is put into the mold and
pressed against the cavity walls (Figure 2). For more complex
geometries where access is a problem, the part must be cured
in two halves and bonded together. This results in a seam that
weakens the part.
APPLICATION OUTLINE
Sacrificial cores yield several performance advantages when used
in place of clamshell tooling. For example, because the composite
fabric is laid up on a male core, it can be favorably oriented and
overlapped to create a seam-free part with optimal mechanical
properties (Figure 3). Using a male tool also eliminates interior
wrinkles, and provides control over interior accuracy and surface
finish.
FDM®
is an additive manufacturing process that builds plastic parts
layer by layer, using data from computer-aided design (CAD) files.
Sacrificial cores made with FDM technology use the same soluble
material that’s used as support structure for FDM parts. However,
unlike other core materials that require harsh methods for removal
from the composite, FDM soluble cores are easily washed away in
a detergent solution (Figure 4). This reduces the risk of damaging
the part during core extraction. Additionally, FDM provides a much
higher level of design freedom than other types of technologies.
This allows the creation of more robust, complex cores that result
in composite parts with improved performance and functionality
(Figure 5).
FDM soluble cores are strong enough to withstand the temperatures
and pressures associated with composite manufacturing processes.
And, because the core is produced in an automated process and the
composite can be laid up directly on the soluble core, much of the
tooling and labor is eliminated. This yields substantial reductions in
lead time and cost.
Figure 1: Composite performance
racing part with hollow ports and
chambers.
APPLICATION BRIEF:
FDM SACRIFICIAL CORES AND
MANDRELS FOR COMPOSITE LAYUPS
BENEFITS OF FDM
Average lead time savings:
•	 50% – 85%
-- From design to final part
Average cost savings:
•	 75% – 95%
-- From design to final part
Reduced labor:
•	 Less tooling and setup
•	 No bonding of composite sections
•	 Hands-free core manufacturing
Improved composite parts:
•	 Single-piece construction
•	 More features, including integrated
hardware
•	 Control over surface finish and
accuracy
-- Core only: part’s internal surfaces
-- Core and mold: part’s internal and
external surfaces
Lower risk:
•	 Minimal investment
•	 Easier to modify
•	 Greater durability
•	 Improved consistency
•	 Higher part yield
FDM IS A BEST FIT
Part geometry:
•	 Complex, hollow parts
-- Requires multi-piece molds
-- Bonding that yields a seam
•	 Replace other core/mandrel
production methods
Part requirements:
•	 Quantities: 1 to 100s
•	 Seamless
•	 Wrinkle-free
•	 Good internal surface finish
and accuracy
Composite manufacturing:
•	 Initial cure temperature:
-- < 121 °C (250 °F)
-- Can post-cure to higher
temperature
•	 Consolidation pressure:
-- < 550 kPa (80 psi)
Figure 2: Two-piece clamshell tooling
and composite duct.
Figure 3: Composite layup over soluble
core (SR-30).
ULTEM®
9085 Resin Support for Sacrificial Cores
ULTEM 9085 resin is a strong, high-temperature thermoplastic that uses a support material which may
be used for sacrificial cores. Exposing it to acetone embrittles the material, allowing it to be extracted.
This option is ideal when molding or curing temperatures exceed the limits of FDM soluble support
materials, or when parts contain aluminum inserts that may be corroded by the support removal solution.
© 2014 Stratasys. All rights reserved. Stratasys and FDM are registered trademarks of Stratasys Inc. SR-30 is a trademark of Stratasys, Inc.
ULTEM®
is a registered trademark of SABIC or affiliates. All other trademarks are the property of their respective owners, and Stratasys assumes
no responsibility with regard to the selection, performance, or use of these non-Stratasys products. Product specifications subject to change
without notice. Printed in the USA. AB-FDM-SolubleCores-10-14-EN
For more information about Stratasys systems, materials and applications, contact Stratasys Application Engineering at
1-855-693-0073 (toll free), +1 952-294-3888 (local/international) or ApplicationSupport@Stratasys.com.
7665 Commerce Way
Eden Prairie, MN 55344
+1 888 480 3548 (US Toll Free)
+1 952 937 3000 (Intl)
+1 952 937 0070 (Fax)
2 Holtzman St.
Science Park, PO Box 2496
Rehovot 76124, Israel
+972 74 745-4000
+972 74 745-5000 (Fax)
ISO 9001:2008 Certified
Stratasys | www.stratasys.com | info@stratasys.com
PROCESS OVERVIEW
The first step is to design a 3D model of the core geometry. During
pre-processing of the digital data, there are two modifications required
to ensure ease of core removal. First, the core is produced with an
internal structure that makes it mostly hollow. Second, the soluble
material normally used for support structures replaces the standard
FDM thermoplastic.
Integrating FDM soluble cores into the composite manufacturing
process is straightforward with minimal modifications. The composite
curing cycle is unchanged as long as the cure temperatures and
pressures are within the specifications of the FDM material. After
curing, simply wash away the core by soaking the part in a support
removal bath.
CUSTOMER STORY
Champion Motorsport’s legacy of performance on the racetrack drives
the performance of its aftermarket products. The Le Mans-winning
team develops, perfects and proves its technology on the track and
then leverages it to create aftermarket Porsche equipment.
When manufacturing a turbo inlet duct for the Porsche 997 Turbo,
Champion used sacrificial FDM cores to overcome the challenges of
making this high-performance carbon fiber part (Figure 6).
“We substantially improved the quality of carbon fiber turbo inlet ducts
and other aftermarket parts by making them with FDM soluble cores,”
said Chris Lyew, lead mechanical engineer for Champion Motorsport.
Lyew adds, “The use of FDM soluble cores makes it possible to mold
the duct in a single piece that is much stronger than parts produced
by bonding. Every FDM soluble core is exactly the same so it’s easy
to maintain the internal finish of the duct. Also, FDM soluble cores are
produced in less time and at a lower cost than sand cores because they
don’t require a mold.”
Companion and reference materials:
• Technical application guide
- Document
• Application brief
- Document
• Video
- Commercial
- Success story
- How It’s Used
• Referenced processes
-	 Best Practice: Removing
	 Soluble Supports
-	 Best Practice: Bonding
-	 Best Practice: CAD to STL
Application compatibility: (0 – N/A, 1 – Low, 5 – High)
• FDM: Idea (0), Design (0), Production (5) • PolyJet™: Design (0), Production (0)	
CUSTOMER PROFILE
Forward-thinking designers,engineers and
manufacturers of composite parts for:
•	 Aerospace, automotive, marine,
robotics
•	 Performance sports
•	 Medical prosthetics/orthotics
Characteristics:
•	 Low-volume manufacturing
-- Challenging, hollow composite parts
•	 Open to change or seeking innovation
Traditional technology obstacles:
•	 High labor demands
-- Limited design freedom
-- Configured to allow core removal
•	 Tooling
-- High cost
-- Long lead time
-- Many mold components
-- Cores hard to work with
-- Inconsistent core features
-- Difficult core removal processes
•	 Reduced part strength with clamshell
molding
REFERENCE
COMPANIES
Figure 4: Soluble core dissolves in a
support removal bath (SR-30).
Figure 5: Composite duct — no seams,
no interior wrinkles.
Figure 6: Carbon fiber turbo inlet
duct (black) for Porsche engine with
matching soluble core (SR-30).

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FDM Sacrificial Cores for Composite Parts

  • 1. OVERVIEW Hollow,compositepartspresentauniquemanufacturingchallenge. Cores are used to create the hollow features in composite structures when smooth internal surface finish and seam-free construction are required. Some cores can be easily removed because of the part’s design geometry, but any configuration that traps a core or mandrel inside it requires special, often sacrificial tooling (Figure 1). Typically, sacrificial cores are made from eutectic salt, ceramic or urethane. These options present several challenges: • Can limit part geometry • Requires machined tooling to make • Uses harsh removal procedures • Difficult to handle, particularly fragile components For these reasons, composites are more commonly laid up in clamshell tooling. If there is sufficient access to the interior of a closed clamshell tool, composite material is put into the mold and pressed against the cavity walls (Figure 2). For more complex geometries where access is a problem, the part must be cured in two halves and bonded together. This results in a seam that weakens the part. APPLICATION OUTLINE Sacrificial cores yield several performance advantages when used in place of clamshell tooling. For example, because the composite fabric is laid up on a male core, it can be favorably oriented and overlapped to create a seam-free part with optimal mechanical properties (Figure 3). Using a male tool also eliminates interior wrinkles, and provides control over interior accuracy and surface finish. FDM® is an additive manufacturing process that builds plastic parts layer by layer, using data from computer-aided design (CAD) files. Sacrificial cores made with FDM technology use the same soluble material that’s used as support structure for FDM parts. However, unlike other core materials that require harsh methods for removal from the composite, FDM soluble cores are easily washed away in a detergent solution (Figure 4). This reduces the risk of damaging the part during core extraction. Additionally, FDM provides a much higher level of design freedom than other types of technologies. This allows the creation of more robust, complex cores that result in composite parts with improved performance and functionality (Figure 5). FDM soluble cores are strong enough to withstand the temperatures and pressures associated with composite manufacturing processes. And, because the core is produced in an automated process and the composite can be laid up directly on the soluble core, much of the tooling and labor is eliminated. This yields substantial reductions in lead time and cost. Figure 1: Composite performance racing part with hollow ports and chambers. APPLICATION BRIEF: FDM SACRIFICIAL CORES AND MANDRELS FOR COMPOSITE LAYUPS BENEFITS OF FDM Average lead time savings: • 50% – 85% -- From design to final part Average cost savings: • 75% – 95% -- From design to final part Reduced labor: • Less tooling and setup • No bonding of composite sections • Hands-free core manufacturing Improved composite parts: • Single-piece construction • More features, including integrated hardware • Control over surface finish and accuracy -- Core only: part’s internal surfaces -- Core and mold: part’s internal and external surfaces Lower risk: • Minimal investment • Easier to modify • Greater durability • Improved consistency • Higher part yield FDM IS A BEST FIT Part geometry: • Complex, hollow parts -- Requires multi-piece molds -- Bonding that yields a seam • Replace other core/mandrel production methods Part requirements: • Quantities: 1 to 100s • Seamless • Wrinkle-free • Good internal surface finish and accuracy Composite manufacturing: • Initial cure temperature: -- < 121 °C (250 °F) -- Can post-cure to higher temperature • Consolidation pressure: -- < 550 kPa (80 psi) Figure 2: Two-piece clamshell tooling and composite duct. Figure 3: Composite layup over soluble core (SR-30). ULTEM® 9085 Resin Support for Sacrificial Cores ULTEM 9085 resin is a strong, high-temperature thermoplastic that uses a support material which may be used for sacrificial cores. Exposing it to acetone embrittles the material, allowing it to be extracted. This option is ideal when molding or curing temperatures exceed the limits of FDM soluble support materials, or when parts contain aluminum inserts that may be corroded by the support removal solution.
  • 2. © 2014 Stratasys. All rights reserved. Stratasys and FDM are registered trademarks of Stratasys Inc. SR-30 is a trademark of Stratasys, Inc. ULTEM® is a registered trademark of SABIC or affiliates. All other trademarks are the property of their respective owners, and Stratasys assumes no responsibility with regard to the selection, performance, or use of these non-Stratasys products. Product specifications subject to change without notice. Printed in the USA. AB-FDM-SolubleCores-10-14-EN For more information about Stratasys systems, materials and applications, contact Stratasys Application Engineering at 1-855-693-0073 (toll free), +1 952-294-3888 (local/international) or ApplicationSupport@Stratasys.com. 7665 Commerce Way Eden Prairie, MN 55344 +1 888 480 3548 (US Toll Free) +1 952 937 3000 (Intl) +1 952 937 0070 (Fax) 2 Holtzman St. Science Park, PO Box 2496 Rehovot 76124, Israel +972 74 745-4000 +972 74 745-5000 (Fax) ISO 9001:2008 Certified Stratasys | www.stratasys.com | info@stratasys.com PROCESS OVERVIEW The first step is to design a 3D model of the core geometry. During pre-processing of the digital data, there are two modifications required to ensure ease of core removal. First, the core is produced with an internal structure that makes it mostly hollow. Second, the soluble material normally used for support structures replaces the standard FDM thermoplastic. Integrating FDM soluble cores into the composite manufacturing process is straightforward with minimal modifications. The composite curing cycle is unchanged as long as the cure temperatures and pressures are within the specifications of the FDM material. After curing, simply wash away the core by soaking the part in a support removal bath. CUSTOMER STORY Champion Motorsport’s legacy of performance on the racetrack drives the performance of its aftermarket products. The Le Mans-winning team develops, perfects and proves its technology on the track and then leverages it to create aftermarket Porsche equipment. When manufacturing a turbo inlet duct for the Porsche 997 Turbo, Champion used sacrificial FDM cores to overcome the challenges of making this high-performance carbon fiber part (Figure 6). “We substantially improved the quality of carbon fiber turbo inlet ducts and other aftermarket parts by making them with FDM soluble cores,” said Chris Lyew, lead mechanical engineer for Champion Motorsport. Lyew adds, “The use of FDM soluble cores makes it possible to mold the duct in a single piece that is much stronger than parts produced by bonding. Every FDM soluble core is exactly the same so it’s easy to maintain the internal finish of the duct. Also, FDM soluble cores are produced in less time and at a lower cost than sand cores because they don’t require a mold.” Companion and reference materials: • Technical application guide - Document • Application brief - Document • Video - Commercial - Success story - How It’s Used • Referenced processes - Best Practice: Removing Soluble Supports - Best Practice: Bonding - Best Practice: CAD to STL Application compatibility: (0 – N/A, 1 – Low, 5 – High) • FDM: Idea (0), Design (0), Production (5) • PolyJet™: Design (0), Production (0) CUSTOMER PROFILE Forward-thinking designers,engineers and manufacturers of composite parts for: • Aerospace, automotive, marine, robotics • Performance sports • Medical prosthetics/orthotics Characteristics: • Low-volume manufacturing -- Challenging, hollow composite parts • Open to change or seeking innovation Traditional technology obstacles: • High labor demands -- Limited design freedom -- Configured to allow core removal • Tooling -- High cost -- Long lead time -- Many mold components -- Cores hard to work with -- Inconsistent core features -- Difficult core removal processes • Reduced part strength with clamshell molding REFERENCE COMPANIES Figure 4: Soluble core dissolves in a support removal bath (SR-30). Figure 5: Composite duct — no seams, no interior wrinkles. Figure 6: Carbon fiber turbo inlet duct (black) for Porsche engine with matching soluble core (SR-30).