Managing composite materials information - working with complex multistage process histories and test results. Granta Design

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1 Managing composite materials information - working with complex multistage process histories and test results Granta Design FEIPLAR COMPOSITES, Sao Paulo, Brazil. November 2014

2 Overview Project partners Characteristics of composites data and how they differ from that for metallics Typical data flow schematic Meta data Raw test data Statistically backed design data

3 The project partners The Materials Data Management Consortium ASM International NASA-Glenn Research Center AWE NASA-Marshall Space Flight Center Baker Hughes Northrop Grumman Boeing Oak Ridge National Laboratory GE - Aviation and GE - Energy Raytheon Granta Design Rolls-Royce Eurocopter Sandia National Labs Honeywell US Army Research Labs Lockheed Martin US Naval Surface Warfare Center Los Alamos National Laboratory United Technologies Corp

4 Focus on composites data How do composite materials vary from metals? Composites materials cannot be created independently from components Composite materials cannot be characterized independent of processing Composites cannot be fabricated, tested and then subsequently formed into a component Composite materials are manufactured by involved multi-step processes Process histories for composites are important, complex and very varied

5 Focus on composites data How do composite materials vary from metals? Performance and property data for composites are similar to that for metals and other materials Mature, well designed materials information management systems sustain composite materials data Some complexity added by conditioning and multi-stage tests (eg CAI) Multiple taxonomies are needed depending on the data Eg Design data: type / matrix / reinforcement / reinforcement structure / layup / conditioning / Test data includes direction, many more examples,

6 Focus on composites data The complexity lies in the processing history Data might be captured at each and every step Property data and processing parameters must be tagged to a specified location in the processing route No one aspect of the data or meta data is more important than another Multiple taxonomies are possible

7 Composites data Reference data Braid Conditioning Test results Resin Fabric Laminate Chopped Fiber Test conditions Continuous Fiber Prepreg Supplier info Processing Design data Nominal values

8 Composites database concept REPORTS Full text original pdf files COMPOSITE SYSTEM General materials information - a record to matrix/reinforcement combo MATERIAL PEDIGREE Raw materials and process data Constituent materials and process data Intermediaries characterisation and process data Laminate processing and lay-up data Compiled reference data Linked to Composite system and Test Results TEST RESULTS Raw test data for each specimen Can accommodate CAI and other 2-stage tests Conditioning data stored with test data DESIGN DATA Statistically backed A and B Basis Linked to test and pedigree

9 Composite Data Flow

10 Traceability and processing history Resin: Batch 1242 Polymer Matrix Fibers: Batch Reinforcement Prepreg: Batch Intermediaries Panel: Laminate AITR1392-PWC2-CAI1-A-MH1

11 Resin: Batch 1242 Polymer Matrix Traceability and processing history Intermediaries Laminate Reinforcement

12 Traceability and processing history Resin: Batch 1242 Polymer Matrix Reinforcement Prepreg: Batch Intermediaries Laminate

13 Traceability and processing history Resin: Batch 1242 Polymer Matrix Fibers: Batch Reinforcement Prepreg: Batch Intermediaries Laminate

14 Traceability and processing history Resin: Batch 1242 Polymer Matrix Fibers: Batch Reinforcement Prepreg: Batch Intermediaries Panel: Laminate AITR1392-PWC2-CAI1-A-MH1

15 Resin: Batch 1242 Polymer Matrix Fibers: Batch Reinforcement Prepreg: Batch Intermediaries Panel: Laminate AITR1392-PWC2-CAI1-A-MH1

16 Test results and Design data Specimen: A0NKA111A

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18 Test results and Design data Specimen: A0NKA111A ACG MTM45-1 CF0526A-36%RW, 3K Plain Weave G Fabric, 25%(0 ) / 50%(±45 ) / 25%(90 ), RTD

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20 Granta MI for Composites A mature materials information management system: Used and developed over many years in conjunction with key customers, technology and partners MDMC; especially the Composites sub-committee Boeing, Northrop Grumman, NASA, Raytheon, Rolls-Royce, Customers; Eurocopter, Astruim Space Transportation, Astrium Satellites, Airbus, and many others Specialized features and capabilities to manage the complexities of composite materials Composites schema Specific composites reference data and tools AGATE, NCAMP, CMH-17, Firehole composites STAT-17 statistical tools from CMH-17 Others

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