Low Cost, High Quality Composite Tooling Utilizing Additive Manufacturing Processes

Size: px
Start display at page:

Download "Low Cost, High Quality Composite Tooling Utilizing Additive Manufacturing Processes"

Transcription

1 Low Cost, High Quality Composite Tooling Utilizing Additive Manufacturing Processes Bill Macy, Stratasys SME Tooling for Composites Charleston, SC Oct 24 th 2011

2 My Apologies for the bait and switch Depot Repair Project Postponed Funds & resources diverted to higher priority repairs Project Plan 180 C cure, 1.2m x 0.5m x 15cm thick tool Track cost metrics for FDM vs. traditional Low Cost Assessment Digitize tools and parts throughout process High Quality Assessment Stay Tuned We will bring you these results in a future presentation

3 Overview Study to expand FDM Core to 180 C Parts Utilize flexible cure resins/prepreg Two stage cure Core provides form during first stage cure Core is non structural during post cure Identify and characterize FMD material options Testing Oven testing Material 180 C Layup cure tests

4 180 C Cure FDM Cores Question If a flexible cure epoxy resin was used Lower initial cure temperatures netting self supporting composite part Followed by 180 C secondary post cure How could FDM cores be utilized? Opportunities Lower initial cure temperatures Minimize FDM CTE compensation factors Maximize core strength Post cure temperature Can we take advantage of FDM Tg to melt out core with secondary post cure?

5 Prepreg UMECO MTM 45-1 Initial Cure: Three OoA cure cycle >28inHg vacuum pressure Option 1: C Option 2: C Option 3: C Post Cure: C

6 Composite Tooling Application FDM Composite Applications Patterns Lay Up / Cure Tools Consumable Cores Digitally Coordinated Tool Families Masters Pre Layup Consolidation Tools Low Temp High Temp Bonding Fixtures Intensifiers Caul Plates Soluble Cores Net Shaped Cores Integrated Interfaces Trim Tool Drill Tool Check Fixture

7 Composite Tooling Application FDM Composite Applications Patterns Lay Up / Cure Tools Consumable Cores Digitally Coordinated Tool Families Masters Pre Layup Consolidation Tools Low Temp High Temp Bonding Fixtures Intensifiers Caul Plates Soluble Cores Net Shaped Cores Integrated Interfaces Trim Tool Drill Tool Check Fixture

8 FDM Tool Material Selection Service FDM Temp Materials ABS AMB 80 C 120 C 175 C AMB 180 F 250 F 350 F Low Temp Tools Low Temp Consumable Cores Master Patterns SR30/SR100 SR30 Soluble Cores SR100 Soluble Cores PC ULTEM Low Temp Cure Tools & Consumable Cores Master Patterns Trim & Drill Tools Med Temp Cure Tools & Consumable Cores High Strength Trim & Drill Tools With Caution PPSF High Temp Tools & Consumable Cores ABS Master & Tooling Composites High Temp CTE Matched Tools 200 C (400 F) Max ABS Master & Nevada Composites High Temp CTE Matched Tools High Temp CTE Matched Soluble Cores +300 C (600 F)

9 FDM Tool Material Selection Service FDM Temp Materials ABS AMB 80 C 120 C 175 C AMB 180 F 250 F 350 F Low Temp Tools Low Temp Consumable Cores Master Patterns SR30/SR100 SR30 Soluble Cores SR100 Soluble Cores PC ULTEM Low Temp Cure Tools & Consumable Cores Master Patterns Trim & Drill Tools Med Temp Cure Tools & Consumable Cores High Strength Trim & Drill Tools With Caution PPSF High Temp Tools & Consumable Cores ABS Master & Tooling Composites High Temp CTE Matched Tools 200 C (400 F) Max ABS Master & Nevada Composites High Temp CTE Matched Tools High Temp CTE Matched Soluble Cores +300 C (600 F)

10 FDM Tool Material Selection Service FDM Temp Materials ABS AMB 80 C 120 C 175 C AMB 180 F 250 F 350 F Low Temp Tools Low Temp Consumable Cores Master Patterns SR30/SR100 SR30 Soluble Cores SR100 Soluble Cores PC ULTEM Low Temp Cure Tools & Consumable Cores Master Patterns Trim & Drill Tools Med Temp Cure Tools & Consumable Cores High Strength Trim & Drill Tools With Caution PPSF High Temp Tools & Consumable Cores ABS Master & Tooling Composites High Temp CTE Matched Tools 200 C (400 F) Max ABS Master & Nevada Composites High Temp CTE Matched Tools High Temp CTE Matched Soluble Cores +300 C (600 F)

11 Application Trade Offs Cycle Time Savings Trade cure time vs. initial cure temp Accuracy CTE growth vs. initial cure temp Cost Savings Lower cost materials vs. higher performance materials Cure Cycle Cure Temp ( C) Cure Time (hrs) Compatible FDM Material FDM Service Temp ( C) FDM Material Tg ( C) Option SR30/ABS Option SR100/PC Option ULTEM Support Post Cure 180 2

12 180 C Behavior Test Materials tested: Ultem Support 1 Polycarbonate ABS M30 SR100 soluble support SR30 soluble support Test part Geometry: 3 diameter cylinder 4 tall wall thickness All parts utilized Insight sparse double dense build style PC SR30 Ultem S1 ABSM30 SR100

13 Test Setup

14 Results Following 2 hour exposure at 180 C Simulating resin post cure cycle

15 Results continued ABSM30 PC Ultem S1 SR30 SR100

16 Results Summary Cure Temperatures ULTEM Support PC & SR100 ABS & SR30 80 C Structural Structural Structural 120 C Structural Structural 130 C 180 C 2 Hour Exposure Structural Did not melt still breaks down with acetone Melted Melted

17 ULTEM Support Breakdown Part must be at room temperature or cooler Part is then wet with acetone Note: Spray or misting of acetone will not work Acetone will then embrittled the support structure enabling crushing/breaking of the support structure by hand

18 Layup Test Samples PC SR100 ULTEM S1

19 Sample Prep Surface Prep Sanded PC ULTEM Support Left SR100 as is Release Treatment Frekote Layup 10 plies MTM45 5mm (.200 ) thick

20 First Stage Cure Test PC & SR C, 1-3 ramp rate Parts maintained shape PC SR100

21 Post Cure Test PC & SR C, 1-3 ramp rate SR100 PC

22 Observations PC Melted 50% of the way out Was fully released Part could easily come free if PC had melted in its entirety Consider fixturing or bagging strategy to promote better melt flow out of part Part maintained shape

23 Observations SR100 Delaminated from itself Did not release from the part SR100 cracking occurred Part is not usable but maintained shape

24 Cure Test ULTEM Support First stage C, 1-3 ramp rate Post cure C, 1-3 ramp rate

25 Observations ULTEM Support Maintained shape Readily released from part Was easily removed with typical composite scraper Only 3oz of acetone was needed

26 Summary/Conclusion ABS/SR30 Could be used but significantly extends cure time, 22 hrs PC Limited value do to melt flow constraints SR100 Can be used, but would still require tank washout Total cure time would be 6 hrs ULTEM Support Supports minimum cure time of 4 hrs Was surprisingly easy to remove Would be geometry limited Requires acetone for removal Using two stage process reduces CTE compensation issues by 30% (delta temp of C)

27 Next Steps Large scale core test in work 1m x 0.5m x 1m tall Material: ULTEM Support Gather mechanical properties for ULTEM Support CTE Dynamic Flex Tensile, Compression

28 Questions?

29 Thank you! Bill Macy, Stratasys

Manufacturing Solutions. John F Dobstetter Business Development Manager Direct Digital Manufacturing

Manufacturing Solutions. John F Dobstetter Business Development Manager Direct Digital Manufacturing Manufacturing Solutions John F Dobstetter Business Development Manager Direct Digital Manufacturing 1 Overview Additive overview Tooling applications End use part applications Tooling for composites 2

More information

Soluble Cores & Mandrels for Hollow Composite Parts

Soluble Cores & Mandrels for Hollow Composite Parts Soluble Cores & Mandrels for Hollow Composite Parts There are many manufacturing options for composite part production. Composites are made by winding, wrapping, molding and laying-up various combinations

More information

The advanced composites industry has a continual need for innovative tooling solutions.

The advanced composites industry has a continual need for innovative tooling solutions. AND DESIGN FLEXIBILITY Timothy Schniepp Head of Tooling Solutions The advanced composites industry has a continual need for innovative tooling solutions. Conventional tooling is typically heavy, costly

More information

The advanced composites industry has a continual need for innovative tooling solutions.

The advanced composites industry has a continual need for innovative tooling solutions. AND DESIGN FLEXIBILITY Timothy Schniepp Head of Tooling Solutions The advanced composites industry has a continual need for innovative tooling solutions. Conventional tooling is typically heavy, costly

More information

Sacrificial Tools with Stratasys FDM Technology

Sacrificial Tools with Stratasys FDM Technology THE 3D PRINTING SOLUTIONS COMPANY Sacrificial Tools with Stratasys FDM Technology DAVIDE FERRULLI davide.ferrulli@stratasys.com Carrara, 7 Aprile 2016 Cell. 348-766 9675 Stratasys For more than 25 years,

More information

Additive Manufacturing 101 Advanced Applications

Additive Manufacturing 101 Advanced Applications Additive Manufacturing 101 Advanced Applications Presented by: James Janeteas, Cimetrix Solutions Inc, Who we are Founded in 1993 Full Line Stratasys Partner for Canada Strong Design / Manufacturing background

More information

TECHNICAL APPLICATION GUIDE FDM Sacrificial Cores And Mandrels For Composite Layups

TECHNICAL APPLICATION GUIDE FDM Sacrificial Cores And Mandrels For Composite Layups Hollow composite parts present a unique manufacturing challenge. Straight-pull tube shapes and straight-walled cavities are easily addressed, but configurations that trap a mandrel need an alternative

More information

FDM Sacrificial Tooling for Composite Part Fabrication USING ADDITIVE MANUFACTURING FOR SACRIFICIAL COMPOSITE TOOL PRODUCTION

FDM Sacrificial Tooling for Composite Part Fabrication USING ADDITIVE MANUFACTURING FOR SACRIFICIAL COMPOSITE TOOL PRODUCTION By Ross Jones, Stratasys Composite Tooling Team Additive manufacturing (AM), or 3D printing as it is more commonly known, has seen an explosion of material options in recent years. With these new material

More information

Recently acquired by. Recently acquired by

Recently acquired by. Recently acquired by Umeco Raw Materials Production Intermediate Processing Parts Manufacture Reinforcement Fibre Preparation Glass Aramid Carbon Unidirectional Woven Chopped Mat Prepregging Moulding (Layup) Resin Curing Basic

More information

Major player in the 3D Printing Market

Major player in the 3D Printing Market Major player in the 3D Printing Market PolyJet FDM High- Performance Resins Production-Grade Thermoplastics High Feature Detail & Finish Highly Durable Parts Multi-Material Printing Functional Parts Makerbot

More information

Company profile. The world s leading provider of 3D printing and manufacturing systems taking visions from idea to reality

Company profile. The world s leading provider of 3D printing and manufacturing systems taking visions from idea to reality Company profile The world s leading provider of 3D printing and manufacturing systems taking visions from idea to reality Dual headquarters Israel and US Global workforce of over 1,600 employees Strong

More information

LEAD-FREE ASSEMBLY COMPATIBLE PWB FABRICATION AND ASSEMBLY PROCESSING GUIDELINES.

LEAD-FREE ASSEMBLY COMPATIBLE PWB FABRICATION AND ASSEMBLY PROCESSING GUIDELINES. LEAD-FREE ASSEMBLY COMPATIBLE PWB FABRICATION AND ASSEMBLY PROCESSING GUIDELINES. TECHNICAL BULLETIN As the industry has moved to lead-free assembly processing, the performance demands on the lead free

More information

TECHNICAL DATA NEAT RESIN MECHANICAL PROPERTIES

TECHNICAL DATA NEAT RESIN MECHANICAL PROPERTIES TYPICAL APPLICATIONS Marine Structures Dielectric Structures Aerospace Structures PRODUCT FORMS Unitape to 24 Inches Wide Fabric Prepreg to 50 Inches Wide TYPICAL CURE PARAMETERS (If Aerospace applications

More information

RM-3002 BISMALEIMIDE (BMI) PREPREG FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS

RM-3002 BISMALEIMIDE (BMI) PREPREG FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS RM-3002 BISMALEIMIDE (BMI) PREPREG FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS RM-3002 Bismaleimide (BMI) Prepreg Product Information Developed using state-of-the-art formulating technologies, RM-3002

More information

Srinivasan Lakshmanan Research Scholar, Noorul Islam University, Kanyakumari District, Tamil Nadu, India.

Srinivasan Lakshmanan Research Scholar, Noorul Islam University, Kanyakumari District, Tamil Nadu, India. An Experimental Analysis of Delamination Factor of a GFRP Composite Material on Radial Drilling Machine Nageswara Rao Manchi M.Tech, Department of Mechanical Engineering, NRI Institute of Technology, Hyderabad,

More information

SPECIALTY MATERIALS, INC.

SPECIALTY MATERIALS, INC. Hy-Bor for Advanced Hat-stiffened Aircraft Structures A design and verification study was undertaken by the Boeing Phantom Works, St. Louis, MO to evaluate the potential structural benefits and cost impact

More information

Question: Are RO4000 materials compatible with lead-free processes? Answer:

Question: Are RO4000 materials compatible with lead-free processes? Answer: Question: Are RO4 materials compatible with lead-free processes? Answer: RO4 cores and prepregs are among the most temperature stable products available. They easily meet or exceed all expectations for

More information

Lightweight Composites for Defense Applications COMPOSITE MATERIALS. Defense / 1

Lightweight Composites for Defense Applications COMPOSITE MATERIALS. Defense / 1 Lightweight Composites for Defense Applications COMPOSITE MATERIALS Defense / 1 Solvay has a rich history in delivering solutions across an ever increasing variety of defense applications. Solvay s prepregs,

More information

Designed for bonding prepreg skins to honeycomb and certain cores. Compatible with SE 84LV, SE 91 & SE 85 prepregs & ST 93 SPRINT products

Designed for bonding prepreg skins to honeycomb and certain cores. Compatible with SE 84LV, SE 91 & SE 85 prepregs & ST 93 SPRINT products General Datasheet SA 80 TOUGHENED EPOXY ADHESIVE FILM Low temperature cure Designed for bonding prepreg skins to honeycomb and certain cores Compatible with SE 84LV, SE 91 & SE 85 prepregs & ST 93 SPRINT

More information

FAA Bonded Structures Workshop 06/17/04 1

FAA Bonded Structures Workshop 06/17/04 1 FAA Bonded Structures Workshop Certifying Bonded Structure Adam Aircraft s Experience Pierre Harter, Structures Project Engineer Adam Aircraft Industries Englewood, CO 80112 FAA Bonded Structures Workshop

More information

This presentation is courtesy of

This presentation is courtesy of This presentation is courtesy of Adhesive Design Considerations Originally presented at: Assembly Tech Expo 2004 Chicago, IL Courtesy 1 Agenda The Three P s Types of Force Width vs. Overlap Effect of Gap

More information

Resource for Composite Tooling and Parts Fabrication Since 2000

Resource for Composite Tooling and Parts Fabrication Since 2000 RJM Corporation Resource for Composite Tooling and Parts Fabrication Since 2000 (Our mission is to provide our customers with quality products on time at competitive prices) RJM Corporation 3220 C Street

More information

CYCOM PREPREG TECHNICAL DATA SHEET

CYCOM PREPREG TECHNICAL DATA SHEET TECHNICAL DATA SHEET is a toughened epoxy resin prepreg system designed for vacuum-bag-only (VBO) or out of autoclave (OOA) manufacturing of primary structural parts. Because of its lower temperature curing

More information

CYCOM X5320. Innovative Approach to Out-of-Autoclave Processing. September 9, Approved for Public Release, WPAFB , DISTAR 12056

CYCOM X5320. Innovative Approach to Out-of-Autoclave Processing. September 9, Approved for Public Release, WPAFB , DISTAR 12056 CYCOM X5320 Innovative Approach to Out-of-Autoclave Processing September 9, 2008 Report Documentation Page Form Approved OMB No. 0704-0188 Public reporting burden for the collection of information is estimated

More information

ULTEM 1010 Resin FDM MATERIAL GUIDE REFERENCE MATERIALS. Overview

ULTEM 1010 Resin FDM MATERIAL GUIDE REFERENCE MATERIALS. Overview FDM MATERIAL GUIDE ULTEM 1010 Resin Overview ULTEM 1010 resin is a flame-retardant, high-performance thermoplastic for direct digital manufacturing and rapid prototyping. ULTEM 1010 offers good chemical

More information

CYCOM Epoxy Resin System

CYCOM Epoxy Resin System T E C H N I C A L D A T A S H E E T CYCOM 9773 EPOXY RESIN SYSTEM CYCOM 9773 Epoxy Resin System DESCRIPTION CYCOM 9773 is a 350 F (177 C) curing resin. It is a toughened epoxy resin with 350 F (177 C)

More information

Overview of composite manufacturing technologies

Overview of composite manufacturing technologies Composite technology BMEGEPT AGE1 Overview of composite manufacturing technologies Gergely Czél Spring 2018 Composites- Structure Lamina, ply, layer Matrix Fibre Interface Laminate Stacking/lay-up sequence

More information

FILM ADHESIVES NOMINAL CURE TEMP F (C ) / TIME. 250 (121) / 60 min Cream. 250 (121) / 60 min Cream. 250 (121) / 60 min Cream. 260 (126) / 20 min Cream

FILM ADHESIVES NOMINAL CURE TEMP F (C ) / TIME. 250 (121) / 60 min Cream. 250 (121) / 60 min Cream. 250 (121) / 60 min Cream. 260 (126) / 20 min Cream FILM ADHESIVES LC-E220 LC-E221 LC-E221ET LC-E221FR LC-E221QC LC-E222 LC-E23 LC-E224 LC-E225 Elevated Tg vs. LC-E221 Additional vs LC-E221 with Accelerated Cure Cycle vs LC-E221 Optically Clear, Low Temp

More information

ULTRATHIN CARBON FIBRE LAMINATES IN SPACE APPLICATIONS

ULTRATHIN CARBON FIBRE LAMINATES IN SPACE APPLICATIONS ULTRATHIN CARBON FIBRE LAMINATES IN SPACE APPLICATIONS Per Wennhage KTH Christopher Cameron RISE SICOMP Timothy Murtagh RUAG Space AB NRFP 3 Slutseminarium 15-16 Nov 2018 Solna SATELLITE SEPARATION SYSTEMS

More information

A Novel Material for High Layer Count and High Reliability Printed Circuit Boards

A Novel Material for High Layer Count and High Reliability Printed Circuit Boards A Novel Material for High Layer Count and High Reliability Printed Circuit Boards Jie Wan, Junqi Tang, Xianping Zeng Shengyi Technology Co., Ltd. No.5 Western Industry Road, North Industry District SSL

More information

TenCate TC380 PRODUCT DATA SHEET

TenCate TC380 PRODUCT DATA SHEET DESCRIPTION TenCate TC380 sets a new benchmark for toughened epoxy prepreg systems. TC380 is extremely tough with an excellent balance of OHC, OHT, CAI, and GIC/GIIC properties. It features low moisture

More information

Materials and Structures. Indian Institute of Technology Kanpur

Materials and Structures. Indian Institute of Technology Kanpur Introduction to Composite Materials and Structures Nachiketa Tiwari Indian Institute of Technology Kanpur Lecture 11 Manufacturing of Thermoset Composites Bag molding technique works well with wet forming

More information

COMPARATIVE CHARACTERIZATION OF THE TC-250 OUT-OF-AUTOCLAVE MATERIAL MADE BY HAND LAY-UP AND AUTOMATED FIBER PLACEMENT PROCESSES

COMPARATIVE CHARACTERIZATION OF THE TC-250 OUT-OF-AUTOCLAVE MATERIAL MADE BY HAND LAY-UP AND AUTOMATED FIBER PLACEMENT PROCESSES COMPARATIVE CHARACTERIZATION OF THE TC-250 OUT-OF-AUTOCLAVE MATERIAL MADE BY HAND LAY-UP AND AUTOMATED FIBER PLACEMENT PROCESSES A. Naghashpour 1, K.S. Madhok 1, S.V. Hoa 1 1 Department of Mechanical and

More information

Document No.: NMS 451/12, Revision A, 9/26/2012

Document No.: NMS 451/12, Revision A, 9/26/2012 NATIONAL INSTITUTE FOR AVIATION RESEARCH Wichita State University Document No.: NMS 451/12, Revision A, 9/26/2012 NCAMP Material Specification This specification is generated and maintained in accordance

More information

DIRECT RAPID MANUFACTURING WITH REAL PRODUCTION PLASTICS USING FUSED DEPOSITION MODELING (FDM)

DIRECT RAPID MANUFACTURING WITH REAL PRODUCTION PLASTICS USING FUSED DEPOSITION MODELING (FDM) DIRECT RAPID MANUFACTURING WITH REAL PRODUCTION PLASTICS USING FUSED DEPOSITION MODELING (FDM) Presented at the 4 th annual Euro-uRapid Conference, Frankfurt, December 3, 2002 by S. Scott Crump, Stratasys

More information

Special Inspections for Externally Applied FRP: How Much is Enough? Peter B. Larson P.E. SECB

Special Inspections for Externally Applied FRP: How Much is Enough? Peter B. Larson P.E. SECB Special Inspections for Externally Applied FRP: How Much is Enough? Peter B. Larson P.E. SECB FRP Special Inspections Why even talk about this stuff? Because FRP Special Inspections are expensive.sometimes

More information

MTM49 series of prepregs is based on C ( F) curing toughened epoxy matrix resins designed for the manufacture of components.

MTM49 series of prepregs is based on C ( F) curing toughened epoxy matrix resins designed for the manufacture of components. ACG MTM 49 SERIES COMPONENT PREPREGS Product Description MTM49 series of prepregs is based on 80-160 C (176-320 F) curing toughened epoxy matrix resins designed for the manufacture of components. The series

More information

North Composites Engineering

North Composites Engineering North Composites Engineering Specialists in Composite training, manufacture, processing and repair equipment supply. North Composites Engineering Ltd is a world class specialist in composite training for

More information

PRODUCT DATA SHEET TYPICAL NEAT RESIN PROPERTIES. Dielectric Constant at 10 Ghz on 4581 quartz Loss Tangent at 10 Ghz on 4581 quartz...0.

PRODUCT DATA SHEET TYPICAL NEAT RESIN PROPERTIES. Dielectric Constant at 10 Ghz on 4581 quartz Loss Tangent at 10 Ghz on 4581 quartz...0. PRODUCT TYPE 250 F (121 C) Cure Epoxy TYPICAL APPLICATIONS Secondary Aircraft Structures Radomes with Spectra, Glass, Quartz & Kevlar Reflectors Sporting Goods Knee Braces and Other Related Medical Items

More information

Highland Composites. Expandable on-site to ~188k sq. ft. (expansion area purchased and graded).

Highland Composites. Expandable on-site to ~188k sq. ft. (expansion area purchased and graded). Highland Composites New state-of-the-art ~63k sq. ft. facility including 4k+ sq. ft. clean assembly room, 2k+ sq. ft. quality lab, ample shipping with dock and ramp loading. Expandable on-site to ~188k

More information

SYSTEMS AND MATERIALS OVERVIEW. FDM 3D Printers

SYSTEMS AND MATERIALS OVERVIEW. FDM 3D Printers SYSTEMS AND MATERIALS OVERVIEW FDM 3D Printers FDM 3D Printers Advancements in additive manufacturing See the Results. FDM (fused deposition modeling) 3D Printers offer unparalleled versatility to turn

More information

FDM Nylon 12 PRODUCTION-GRADE THERMOPLASTIC FOR FORTUS 3D PRODUCTION SYSTEMS

FDM Nylon 12 PRODUCTION-GRADE THERMOPLASTIC FOR FORTUS 3D PRODUCTION SYSTEMS FDM Nylon 12 FDM Nylon 12 is the first material in Stratasys new family of nylon offerings, complementing the current portfolio of FDM materials and enabling new applications requiring: repetitive snap

More information

CYCOM E773 EPOXY PREPREG

CYCOM E773 EPOXY PREPREG DESCRIPTION CYCOM E773/E773FR resins are controlled flow epoxy systems with a large processing window. They exhibit excellent high temperature performance up to 180 F (82 C) wet service temperature. The

More information

NOVEL TOUGHENED EPOXY SYSTEMS FOR DAMAGE TOLERANT COMPOSITE PRESSURE VESSELS. SAMPE Brazil - 6 November 2018 Benjamin Benz

NOVEL TOUGHENED EPOXY SYSTEMS FOR DAMAGE TOLERANT COMPOSITE PRESSURE VESSELS. SAMPE Brazil - 6 November 2018 Benjamin Benz NOVEL TOUGHENED EPOXY SYSTEMS FOR DAMAGE TOLERANT COMPOSITE PRESSURE VESSELS SAMPE Brazil - 6 November 2018 Benjamin Benz Presentation Outline Olin Composites An Overview Filament Winding Composite Pressure

More information

SYSTEMS AND MATERIALS OVERVIEW. FDM 3D Printers

SYSTEMS AND MATERIALS OVERVIEW. FDM 3D Printers SYSTEMS AND MATERIALS OVERVIEW FDM 3D Printers FDM 3D Printers Advancements in additive manufacturing See the Results. FDM (fused deposition modeling) 3D Printers offer unparalleled versatility to turn

More information

Nylon 12 FDM BEST PRACTICE. Overview. 1. Printing Recommendations And Tips SOFTWARE / PRODUCT / FINISHING

Nylon 12 FDM BEST PRACTICE. Overview. 1. Printing Recommendations And Tips SOFTWARE / PRODUCT / FINISHING FDM BEST PRACTICE Nylon 12 SOFTWARE / PRODUCT / FINISHING Overview Nylon 12 is a semi-crystalline, FDM thermoplastic. As with other semi-crystalline materials used in traditional manufacturing processes,

More information

RM-3004 OUT OF AUTOCLAVE PROCESSABLE BISMALEIMIDE (BMI) PREPREG FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS

RM-3004 OUT OF AUTOCLAVE PROCESSABLE BISMALEIMIDE (BMI) PREPREG FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS RM-3004 OUT OF AUTOCLAVE PROCESSABLE BISMALEIMIDE (BMI) PREPREG FOR HIGH PERFORMANCE AEROSPACE APPLICATIONS RM-3004 Out of Autoclave (OOA) Processable Bismaleimide (BMI) Prepreg Product Information Developed

More information

HONEYCOMB TOOLING PANELS HCL-180

HONEYCOMB TOOLING PANELS HCL-180 HONEYCOMB TOOLING PANELS HCL-180 For use with low-temperature, composite tooling applications. This fabricated tooling panel is built from fiberglass and epoxy skins with a perforated and corrosion-resistant

More information

VT-45PP VT-47PP VT-447PP

VT-45PP VT-47PP VT-447PP & Prepreg General Information Ventec provides a series of and Prepregs with different glass style and resin content. These products have good bonding and thermal performance in applications of heat sink

More information

COMPOSITES LAB MANUAL

COMPOSITES LAB MANUAL COMPOSITES LAB MANUAL Version 1 Lab 2: Health concerns and safety procedures The original version of this manual was a one student senior design project written by Katherine White, the Composite lab assistant,

More information

FDM 3D Printers SYSTEMS AND MATERIALS OVERVIEW

FDM 3D Printers SYSTEMS AND MATERIALS OVERVIEW FDM 3D Printers SYSTEMS AND MATERIALS OVERVIEW FDM 3D Printers Advancements in additive manufacturing See the Results. FDM (fused deposition modeling) 3D Printers offer unparalleled versatility to turn

More information

LOW TEMPERATURE CURE HIGH TOUGHNESS EPOXY PREPREG SYSTEM. Excellent balance of mechanical properties and toughness

LOW TEMPERATURE CURE HIGH TOUGHNESS EPOXY PREPREG SYSTEM. Excellent balance of mechanical properties and toughness General Datasheet SE 70 LOW TEMPERATURE CURE HIGH TOUGHNESS EPOXY PREPREG SYSTEM Low temperature 70 C (158 F) curing Faster cycle times at elevated temperature Excellent balance of mechanical properties

More information

High Temperature Potting Compounds

High Temperature Potting Compounds High Temperature Potting Compounds Hysol EA 9820 & EA 9825 Henkel Aerospace Bay Point, CA Product Overview Content Description & Application Attributes & Features Packaging Configurations Offered Physical

More information

Document No.: NMS 451/4, Revision A, 9/27/2012

Document No.: NMS 451/4, Revision A, 9/27/2012 NATIONAL INSTITUTE FOR AVIATION RESEARCH Wichita State University Document No.: NMS 451/4, Revision A, 9/27/2012 NCAMP Material Specification This specification is generated and maintained in accordance

More information

VACUUM INFUSION AND CURING OF CARBON FIBER/BENZOXAZINE COMPOSITES FOR HIGH TEMPERATURE APPLICATIONS

VACUUM INFUSION AND CURING OF CARBON FIBER/BENZOXAZINE COMPOSITES FOR HIGH TEMPERATURE APPLICATIONS VACUUM INFUSION AND CURING OF CARBON FIBER/BENZOXAZINE COMPOSITES FOR HIGH TEMPERATURE APPLICATIONS Amol Ogale 1, David Leach 2, Ehsan Barjasteh 2, Helder Barros-Abreu3, Dale Brosius 4, Jens Schlimbach

More information

UMECO LTM 210 SERIES TOOLING PREPREGS

UMECO LTM 210 SERIES TOOLING PREPREGS UMECO LTM 210 SERIES TOOLING PREPREGS Product Description The Umeco LTM210 series of prepreg systems are based upon proprietary low temperature cure epoxy based formulations which may be postcured to produce

More information

Shelf life at -18 C. Tack life at +23 C

Shelf life at -18 C. Tack life at +23 C 1 3 Shelf life at -18 C Tack life at +23 C 4 5 6 Indicator name Value Reinforcing filler UD Twill 2x2 Twill 2x2 Fiber type T700-12К Т300-3К T700-12К Areal weight, g/m² 200 200 600 Resin content, % 36

More information

Cycom Modified Cyanate Prepreg System

Cycom Modified Cyanate Prepreg System TECHNICAL DATA SHEET AEROSPACE MATERIALS Cycom 55-2 Modified Cyanate Prepreg System DESCRIPTION The Rigidite 55-2 Prepreg System is a 350 F (177 C) curing modified cyanate ester resin. This system has

More information

Hierarchical Sensing System Combining Optical Fiber Network and Distributed Built-In CVM Sensors: Delamination Monitoring of CFRP Structure

Hierarchical Sensing System Combining Optical Fiber Network and Distributed Built-In CVM Sensors: Delamination Monitoring of CFRP Structure 6th European Workshop on Structural Health Monitoring - Tu.4.A.3 More info about this article: http://www.ndt.net/?id=14116 Hierarchical Sensing System Combining Optical Fiber Network and Distributed Built-In

More information

Composite materials for wind turbine blades. Department of Mechanical, Chemical and Materials Engineering University of Cagliari, Italy

Composite materials for wind turbine blades. Department of Mechanical, Chemical and Materials Engineering University of Cagliari, Italy Composite materials for wind turbine blades 1 Wind turbine blades Wind turbine blades are complex structures whose design involves the two basic aspects of Selection of the aerodynamic shape Structural

More information

Newport 307. Description: Application: Benefits/Features: Recommended Processing Conditions:

Newport 307. Description: Application: Benefits/Features: Recommended Processing Conditions: Newport 307 Description: Newport 307 is a 250 F (121 C) to 300 F (149 C) cure, highly toughened, controlled flow epoxy resin system. Versatile processing, excellent mechanical properties, and long out

More information

RAKU-TOOL. Product Overview. Product Overview All RAKU-TOOL products at a glance.

RAKU-TOOL. Product Overview. Product Overview All RAKU-TOOL products at a glance. RAKU-TOOL Product Overview GB www.rampf-gruppe.de Product Overview All RAKU-TOOL products at a glance. RAMPF Tooling RAKU-TOOL Product Overview Epoxy Systems 2 Epoxy Resin Epoxy Hardener Mix ratio (pbw)

More information

CURVATURE EFFECTS ON THE DAMAGE TOLERANCE OF IMPACT DAMAGED COMPOSITE SANDWICH PANELS

CURVATURE EFFECTS ON THE DAMAGE TOLERANCE OF IMPACT DAMAGED COMPOSITE SANDWICH PANELS CURVATURE EFFECTS ON THE DAMAGE TOLERANCE OF IMPACT DAMAGED COMPOSITE SANDWICH PANELS R. Clifton Moody, James S. Harris, and Anthony J. Vizzini Composites Research Lab Department of Aerospace Engineering

More information

Composite Materials: Advantages and Cost Factors

Composite Materials: Advantages and Cost Factors Composite Materials: Advantages and Cost Factors Clifford Lester and Dr. Steven Nutt * March 21, 2018 I INTRODUCTION Fiber reinforced composites have been in use for over fifty years, but only recently

More information

Chopped Prepregs - A Compelling Performance and Cost Alternative Material Form

Chopped Prepregs - A Compelling Performance and Cost Alternative Material Form Chopped Prepregs - A Compelling Performance and Cost Alternative Material Form Tencate Advanced Composites CCS Composites, LLC 2450 Cordelia Road - Fairfield, CA 94534 info@tcac-usa.com www.tencateadvancedcomposites.com

More information

abcdef ACG MTA 240 VERSATILE CURE FILM ADHESIVE Product Description Features Instructions for use

abcdef ACG MTA 240 VERSATILE CURE FILM ADHESIVE Product Description Features Instructions for use ACG MTA 2 VERSATILE CURE FILM ADHESIVE Product Description MTA2 is a structural film adhesive suitable for bonding both aluminium and composite substrates either to themselves or to honeycomb core materials.

More information

Drape and tackiness optimised for excellent handling. Excellent balance of mechanical performance and toughness

Drape and tackiness optimised for excellent handling. Excellent balance of mechanical performance and toughness Full General Datasheet ST 94 SINGLE SIDED SPRINT Drape and tackiness optimised for excellent handling Ideal for complex or vertical mouldings Excellent balance of mechanical performance and toughness and

More information

Manufacturing Tooling with FDM Technology Application Benefits, Solution Fitment, Best Practices

Manufacturing Tooling with FDM Technology Application Benefits, Solution Fitment, Best Practices Manufacturing Tooling with FDM Technology Application Benefits, Solution Fitment, Best Practices Fred Fischer Director Applications, Products, Technology 1 APPLICATIONS DESIGN STEADY GROWTH * MANUFACTURING

More information

An onboard camera enables a remote and real time control of the tape laying operation. A remote operator

An onboard camera enables a remote and real time control of the tape laying operation. A remote operator es can be drawn or cut in the entire NTPT THINPREG 135 DATA SHEET looking to reduce costs, reduce material wastage, ThinPreg 135 is a breakthrough product combining high strength and high toughness in

More information

QUANTIFICATION OF PROCESSING PARAMETERS FOR WIND TURBINE BLADES

QUANTIFICATION OF PROCESSING PARAMETERS FOR WIND TURBINE BLADES AIAA-2003-0694 QUANTIFICATION OF PROCESSING PARAMETERS FOR WIND TURBINE BLADES Douglas Cairns, John Mandell, and Daniel Samborsky Montana State University Bozeman, Montana, 59717 ABSTRACT All materials

More information

Document No.: NMS 451/7, Revision -, January 08, 2019

Document No.: NMS 451/7, Revision -, January 08, 2019 NMS 451/7 Rev - Date: January 08, 2019 Document No.: NMS 451/7, Revision -, January 08, 2019 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard

More information

ABS-M30 PRODUCTION-GRADE THERMOPLASTIC FOR FDM 3D PRINTERS

ABS-M30 PRODUCTION-GRADE THERMOPLASTIC FOR FDM 3D PRINTERS ABS-M30 PRODUCTION-GRADE THERMOPLASTIC FOR FDM 3D PRINTERS ABS-M30 is up to 25 to 70 percent stronger than standard ABS and is an ideal material for conceptual modeling, functional prototyping, manufacturing

More information

Composite Materials for Automotive Applications

Composite Materials for Automotive Applications Composite Materials for Automotive Applications COMPOSITE MATERIALS more performance. Advanced material solutions for the manufacture of lightweight, high performance and complex structures. A world leader

More information

Guide to Primary Post-Printing Processes for FDM 3D Models. How to improve aesthetic and mechanical properties of printed 3D parts

Guide to Primary Post-Printing Processes for FDM 3D Models. How to improve aesthetic and mechanical properties of printed 3D parts Guide to Primary Post-Printing Processes for FDM 3D Models How to improve aesthetic and mechanical properties of printed 3D parts DOC-01862 Rev. A Copyright Copyright 2016 Stratasys Ltd. All rights reserved.

More information

CURING OF COMPOSITE MATERIALS USING THE RECENTLY DEVELOPED HEPHAISTOS MICROWAVE M. Kwak 1 *, P. Robinson 2, A. Bismarck 2, R.

CURING OF COMPOSITE MATERIALS USING THE RECENTLY DEVELOPED HEPHAISTOS MICROWAVE M. Kwak 1 *, P. Robinson 2, A. Bismarck 2, R. 18 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS CURING OF COMPOSITE MATERIALS USING THE RECENTLY DEVELOPED HEPHAISTOS MICROWAVE M. Kwak 1 *, P. Robinson 2, A. Bismarck 2, R. Wise 1 1 Advanced Materials

More information

Document No.: NMS 451/12, Revision C, August 15, 2018

Document No.: NMS 451/12, Revision C, August 15, 2018 Date: August 15, 2018 Document No.: NMS 451/12, Revision C, August 15, 2018 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures,

More information

SHEAR BOND STRENGTH TEST

SHEAR BOND STRENGTH TEST Test Procedure for SHEAR BOND STRENGTH TEST TxDOT Designation: Tex-249-F Effective Date: December 2017 1. SCOPE 1.1 This test determines the shear strength between two bonded pavement layers. Specimens

More information

RAKU-TOOL Boards USA. There is a solution for every challenge: RAKU-TOOL. Distributed By:

RAKU-TOOL Boards USA. There is a solution for every challenge: RAKU-TOOL.  Distributed By: USA RAKU-TOOL Boards There is a solution for every challenge: RAKU-TOOL. Distributed By: ThyssenKrupp Materials NA w We find solutions for your applications Performance proven solutions with RAKU-TOOL.

More information

Ancamine 2167 & 2264 Curing Agents

Ancamine 2167 & 2264 Curing Agents & Curing Agents Description and epoxy curing agents exhibit some of the beneficial properties of both cycloaliphatic and aromatic amines. These curing agents are an ideal alternative to aromatic diamines

More information

USA. RAKU-TOOL Boards. There is a solution for every challenge: RAKU-TOOL.

USA. RAKU-TOOL Boards.   There is a solution for every challenge: RAKU-TOOL. USA RAKU-TOOL Boards www.rampf-gruppe.de There is a solution for every challenge: RAKU-TOOL. RAKU-TOOL Boards 2 3 We find solutions for your applications Performance proven solutions with RAKU-TOOL. RAMPF

More information

FDM - FUSED DEPOSITION MODELING

FDM - FUSED DEPOSITION MODELING FDM - FUSED DEPOSITION MODELING 3 D P R I N T I N G & A D VA N C E D M A N U FA C T U R I N G BUILD STABLE AND ROBUST Produce parts with the most demanding requirements, ready for tough testing and harsh

More information

TenCate BT250E-1 PRODUCT DATA SHEET

TenCate BT250E-1 PRODUCT DATA SHEET DESCRIPTION TenCate s BT250E-1 resin system is a 121 C (250 F) cure epoxy prepreg system with excellent toughness and strength. It provides an outstanding surface finish under vacuum bag/oven cure only.

More information

ST 95 STRUCTURAL SPRINT. Good balance of mechanical properties. Excellent laminate quality. Extremely low void content. Drape-able and conformable

ST 95 STRUCTURAL SPRINT. Good balance of mechanical properties. Excellent laminate quality. Extremely low void content. Drape-able and conformable Full General Datasheet ST 95 STRUCTURAL SPRINT Good balance of mechanical properties Excellent laminate quality Extremely low void content Drapeable and conformable Good tack Fast layup No debulk necessary

More information

Eliminating Voids in FDM Processed Polyphenylsulfone, Polycarbonate, and ULTEM 9085 by Hot Isostatic Pressing. Prepared by: Mary Elizabeth Parker

Eliminating Voids in FDM Processed Polyphenylsulfone, Polycarbonate, and ULTEM 9085 by Hot Isostatic Pressing. Prepared by: Mary Elizabeth Parker Eliminating Voids in FDM Processed Polyphenylsulfone, Polycarbonate, and ULTEM 9085 by Hot Isostatic Pressing Prepared by: Mary Elizabeth Parker Faculty Advisors: Dr. Michael West REU Site Director, Department

More information

ST 95 STRUCTURAL SPRINT. Good balance of mechanical properties. Excellent laminate quality. Extremely low void content. Drape-able and conformable

ST 95 STRUCTURAL SPRINT. Good balance of mechanical properties. Excellent laminate quality. Extremely low void content. Drape-able and conformable Full General Datasheet ST 95 STRUCTURAL SPRINT Good balance of mechanical properties Excellent laminate quality Extremely low void content Drapeable and conformable Good tack Fast layup No debulk necessary

More information

TCO G Module Perform a Bonded Composite Repair

TCO G Module Perform a Bonded Composite Repair TCO G Module Perform a Bonded Composite Repair G1: Demonstrate/apply common drying and surface preparation techniques, and how to inspect for acceptability Proper drying and surface preparation are essential

More information

ANALYSING THE FATIGUE LIFE ON WOVEN GLASS FIBER / EPOXY POLYMER COMPOSITE LAMINATE

ANALYSING THE FATIGUE LIFE ON WOVEN GLASS FIBER / EPOXY POLYMER COMPOSITE LAMINATE International Journal of Engineering Research And Advanced Technology (IJERAT) ISSN:2454-6135 [Volume. 03 Issue.6, June 2017] www.sretechjournal.org ANALYSING THE FATIGUE LIFE ON WOVEN GLASS FIBER / EPOXY

More information

Influence of Angle Ply Orientation on Tensile Properties of Carbon/Glass Hybrid Composite

Influence of Angle Ply Orientation on Tensile Properties of Carbon/Glass Hybrid Composite Journal of Minerals and Materials Characterization and Engineering, 2013, 1, 231-235 http://dx.doi.org/10.4236/jmmce.2013.15036 Published Online September 2013 (http://www.scirp.org/journal/jmmce) Influence

More information

STELIA AEROSPACE NORTH AMERICA

STELIA AEROSPACE NORTH AMERICA STELIA AEROSPACE NORTH AMERICA SPACE QUALIFIABLE BONDED JOINTS BETWEEN CARBON FIBER REINFORCED POLYMER (CFRP) AND ALUMINUM SOHEILA MAHDAVI Outline 1 2 Stelia Presentation Carbon Fiber Reinforced Polymer

More information

Flexural Behaviour of Sandwich Composite Panels Fabricated Through Different Vacuum Bagging Techniques

Flexural Behaviour of Sandwich Composite Panels Fabricated Through Different Vacuum Bagging Techniques Journal of Materials Science & Surface Engineering Vol. 3 (4), 2015, pp 293-297 Contents lists available at http://www.jmsse.org/ Journal of Materials Science & Surface Engineering Flexural Behaviour of

More information

TIMBER REPAIRS WITH FRP

TIMBER REPAIRS WITH FRP TIMBER REPAIRS WITH FRP by Vijaya (VJ) Gopu, Ph.D., P.E Associate Director External Programs, LTRC Matthew G. Stuller Endowed Professor, UL Lafayette Formosa Plastic Endowed Professor Emeritus, LSU 2018

More information

From Carbon Fiber to Carbon Fiber Reinforced ThermoPlastics

From Carbon Fiber to Carbon Fiber Reinforced ThermoPlastics SAMPE Brazil Conference 2012 November 6, 2012 From Carbon Fiber to Carbon Fiber Reinforced ThermoPlastics Mr. Joe Spangler Technical Services Manager Toho Tenax America Dr. Anatole Gilliot - Aerospace

More information

July 16, 2007 NPS Rev A Page 1 of 10

July 16, 2007 NPS Rev A Page 1 of 10 Page 1 of 10 Table of Contents 1. SCOPE...3 1.1 Purpose...3 1.2 Health and Safety...3 2. APPLICABLE DOCUMENTS...3 2.1 NCAMP Publications...3 2.2 ISO Publications:...4 2.3 US Government Publications:...4

More information

Producing composite mouldings using prepreg

Producing composite mouldings using prepreg Unit 844 Producing composite mouldings using pre-preg laminating components UAN: L/600/5943 Level: Level 2 Credit value: 14 GLH: 64 Relationship to NOS: This unit has been derived from national occupational

More information

Case Studies DOMESTIC POTABLE WATER TANKS

Case Studies DOMESTIC POTABLE WATER TANKS DOMESTIC POTABLE WATER TANKS YEAR OF Domestic Potable Water Tanks Plasmate JSC South East Asia Auspreg UV MTT 911 UV Curable PE Double Bias 450 2009 A manufacturer of 1, 1.5 and 2m 3 water tanks weighing

More information

Multek s lead free compatible and compliant material selection February 01, 2006

Multek s lead free compatible and compliant material selection February 01, 2006 Multek s lead free compatible and compliant material selection Helmut.Kroener@de.multek.com +49 7 463 543 February 0, 2006 Overview I. Introduction II. Project setup III. Tested materials IV. Test vehicle

More information

Leading Composite Material Solutions for the Marine Industry

Leading Composite Material Solutions for the Marine Industry Leading Composite Material Solutions for the Marine Industry COMPOSITE MATERIALS As the supplier of choice for structural and tooling prepregs, and vacuum bagging consumables to the marine industry, Solvay

More information

Document No.: NMS 451/4, Revision C, November 29, 2018

Document No.: NMS 451/4, Revision C, November 29, 2018 Date: November 29, 2018 Document No.: NMS 451/4, Revision C, November 29, 2018 NCAMP Material Specification This specification is generated and maintained in accordance with NCAMP Standard Operating Procedures,

More information

Producing composite mouldings using prepreg laminating techniques

Producing composite mouldings using prepreg laminating techniques Unit 044 Producing composite mouldings using prepreg Level: 2 Credit value: 14 NDAQ number: 500/9514/6 Unit aim This unit covers the skills and knowledge needed to prove the competences required to produce

More information

PRODUCT DATASHEET TENCATE 8020 RAPI-PLY PREPREG BENEFITS/FEATURES TYPICAL LAMINATE PROPERTIES. Tensile Strength RTD EN MPa 148 ksi

PRODUCT DATASHEET TENCATE 8020 RAPI-PLY PREPREG BENEFITS/FEATURES TYPICAL LAMINATE PROPERTIES. Tensile Strength RTD EN MPa 148 ksi PRODUCT DESCRIPTION materials achieve excellent quality laminates from vacuum bag processing. resin is a new generation of toughened epoxy s offering an excellent balance of mechanical properties. The

More information