Low Cost, High Quality Composite Tooling Utilizing Additive Manufacturing Processes
|
|
- Veronica Perkins
- 6 years ago
- Views:
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 1 Overview Additive overview Tooling applications End use part applications Tooling for composites 2
More informationSoluble 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 informationThe 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 informationThe 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 informationSacrificial 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 informationAdditive 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 informationTECHNICAL 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 informationFDM 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 informationRecently 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 informationMajor 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 informationCompany 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 informationLEAD-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 informationTECHNICAL 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 informationRM-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 informationSrinivasan 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 informationSPECIALTY 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 informationQuestion: 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 informationLightweight 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 informationDesigned 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 informationFAA 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 informationThis 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 informationResource 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 informationCYCOM 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 informationCYCOM 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 informationULTEM 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 informationCYCOM 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 informationOverview 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 informationFILM 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 informationULTRATHIN 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 informationA 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 informationTenCate 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 informationMaterials 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 informationCOMPARATIVE 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 informationDocument 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 informationDIRECT 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 informationSpecial 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 informationMTM49 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 informationNorth 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 informationPRODUCT 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 informationHighland 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 informationSYSTEMS 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 informationFDM 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 informationCYCOM 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 informationNOVEL 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 informationSYSTEMS 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 informationNylon 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 informationRM-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 informationHONEYCOMB 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 informationVT-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 informationCOMPOSITES 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 informationFDM 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 informationLOW 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 informationHigh 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 informationDocument 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 informationVACUUM 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 informationUMECO 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 informationShelf 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 informationCycom 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 informationHierarchical 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 informationComposite 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 informationNewport 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 informationRAKU-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 informationCURVATURE 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 informationComposite 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 informationChopped 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 informationabcdef 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 informationDrape 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 informationManufacturing 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 informationAn 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 informationQUANTIFICATION 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 informationDocument 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 informationABS-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 informationComposite 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 informationGuide 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 informationCURING 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 informationDocument 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 informationSHEAR 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 informationRAKU-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 informationAncamine 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 informationUSA. 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 informationFDM - 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 informationTenCate 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 informationST 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 informationEliminating 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 informationST 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 informationTCO 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 informationANALYSING 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 informationInfluence 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 informationSTELIA 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 informationFlexural 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 informationTIMBER 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 informationFrom 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 informationJuly 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 informationProducing 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 informationCase 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 informationMultek 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 informationLeading 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 informationDocument 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 informationProducing 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 informationPRODUCT 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