Innovation for a Sustainable Aviation in a Global Environment

Similar documents
FINAL PUBLISHABLE REPORT

Integrated Tool for Simulation of Textile Composites

INDUSTRIAL WOVEN NON-CRIMP MULTILAYER FABRICS FOR BETTER IMPACT PROPERTIES

LIBA Multi Compact Fabric Ein neues Textil stellt sich vor

EFFECTS OF STITCH PATTERN ON THE MECHANICAL PROPERTIES OF NON-CRIMP FABRIC COMPOSITES

Press Release 19 December 2017

NEW APPROACHES IN TEXTILE AND IMPREGNATION TECHNOLOGIES FOR THE COST EFFECTIVE MANUFACTURING OF CFRP AEROSPACE COMPONENTS

Textile Production Technologies for Multi- Material-Lightweight Components

3D Fabrics for Composites

Position Paper. On the mid-term review of the 2011 White Paper on Transport

concrete Apolo MEA Befestigungssysteme GmbH Industriestraße Aichach DEUTSCHLAND Apolo MEA Befestigungssysteme GmbH, Plant2 Germany

This document is a preview generated by EVS

A New Lamb-Wave Based NDT System for Detection and Identification of Defects in Composites

Introducing Expleo Through the Lens

DEUTSCHE NORM DIN EN ISO 10447

Meeting the volumes, cost and technical challenges for further penetration of composites in airframes

Generic Experimental Cockpit (GECO)

The Composites Market

Supporting EU Access to Canadian Research and Innovation Programs. Nadia Khelef Institut Pasteur. FP7 Health Infoday May 29th 2012

ASSESSMENT OF COMPOSITES REINFORCED WITH INNOVATIVE 3D WOVEN HOLLOW FABRICS

German Society for Intelligent Transport Systems ITS Germany


INTELLECTUAL PROPERTY FINANCIAL SUPPORT

BUILDING AN EUROPEAN ECOSYSTEM FOR PROTOTYPE MANUFACTURING IN THE AEROSPACE INDUSTRY

M. Bücker*, M. Magin. Institute for Composite Materials, Erwin-Schrödinger-Straße 58, Kaiserslautern, Germany

English Version EUROPEAN COMMITTEE FOR STANDARDIZATION COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG

Research DG. European Commission. Sharing Visions. Towards a European Area for Foresight

Plywood Limningskvalitet Del 1: Provning. Plywood Bonding quality Part 1: Test methods

This document is a preview generated by EVS

EXPERIMENTAL INVESTIGATION OF FATIGUE BEHAVIOUR IN COMPOSITE BOLTED JOINTS

0226/18-V1-02 IMTEC HR. High mechanical Resistance fastener for composite materials

European Technical Assessment. ETA-09/0338 of 18 June English translation prepared by DIBt - Original version in German language.

OPTICAL PERMEABILITY MEASUREMENTS OF NCF: INFLUENCE OF MATERIALPROPERTIES ON THE 2D PREFORM PERMEABILITY

Design of mode selective actuators for Lamb wave excitation in composite plates

Klaus-Fischer-Straße Waldachtal DEUTSCHLAND EAD This version replaces ETA-15/0352 issued on 12 April 2016

THE OPTIMISED POST-FITTED FOAM SANDWICH INSERT

European Technical Assessment. ETA-18/0861 of 12 November English translation prepared by DIBt - Original version in German language

SHAPING PRODUCTIVITY IN AEROSPACE

Artemis for researchers? Werner Damm Chairman Artemis Center of Innovation Excellence for Transportation Chairman SafeTRANS

3D Terahertz Imaging of Hidden Defects in Oxide Fibre Reinforced Ceramic Composites

Executive Board. Innovations for tomorrow. Meet your needs with DLR s potential

Finite-Element-Analysis of Mechanical Characteristics of RTM-Tools

The Aerospace Industry - an integral part of Innovative Sweden. Aerodays Vienna

EFFECT OF YARN CROSS-SECTIONAL SHAPES AND CRIMP ON THE MECHANICAL PROPERTIES OF 3D WOVEN COMPOSITES

RapidScan II Application Note General Composite Scanning

SAMPE Europe Symposium 2012 (SEMAT 12) Symposium on Automation of Advanced Composites and its Technology

MSc in Aerospace Engineering,TU Delft, Cum Laude

Monitoring damage growth in composite materials by FBG sensors

This document is a preview generated by EVS

Kissing bonds monitoring using nonlinear vibro-acoustic wave modulations

ANCHORING TECHNOLOGY CAST-IN CHANNELS PEC-TA

Fästelement Sexkanthålsskruvar med sänkhuvud (ISO 10642:2004) Hexagon socket countersunk head screws (ISO 10642:2004)

Injection containers and accessories Part 1: Injection vials made of glass tubing (ISO :2003)

Västra Götaland pilot project (I)

Mr. Wolfgang Metzen was trained as a mechanical

English version. Steel and steel products Location and preparation of samples and test pieces for mechanical testing (ISO 377:1997)

Aeronautics Supply Chain in Greece Public Private partnership. The missing link Professor Vassilis KOSTOPOULOS

International Research Collaboration. - Why do it?

Licensed Copy: RRICTISQ RRICTISQ, ISO/Exchange Russia, 01 December 2004, Uncontrolled Copy, (c) BSI

Design of structural connections for precast concrete buildings

The Effects of Adding Attachments in Conventional Composite Hybrid Joints on Tensile Strength

Fasteners Torque/clamp force testing (ISO 16047:2005)

Product Overview Fastening and Assembly Technology 1190/15.02

Characterization of Damages in Honeycomb Structures Using SonatestDryScan 410D

nuclear science and technology

European Technical Assessment ETA-04/0101 English translation prepared by DIBt. Page 2 of 12 1 March 2018

European Technical Assessment. ETA-18/0045 of 22 February English translation prepared by DIBt - Original version in German language

Braiding Technology: Machine Concepts, Processes and Applications

SHAPING PRODUCTIVITY IN AEROSPACE

Document Change Record

SVENSK STANDARD SS-EN Flexibla tätskikt Bestämning av längd, bredd och rakhet Del 1: Bitumenbaserade tätskikt för tak

four growing market areas are messaging and navigation services, mobility services, video delivery services, and interactive multimedia services.

The cutting edge. High-temperature brazing powder

Final Report. MAASiFiE. Report Nr 1.2 May 2017

Manual for Propeller Type H40F

Track side measuring system: prototype implementation Malching

FiReP GRP Bolts. Bolting systems for mining and tunnelling. Solutions from Materials Technology

Structural Health Monitoring: A Contribution to the Intelligent Aircraft Structure

3D Woven Textiles for Composite Applications. Presented at UMAMI. March 20, Steve Clarke T.E.A.M., Inc.

This document is a preview generated by EVS

Integration of Piezoceramic Modules into Die Castings Procedure and Functionalities

OVERVIEW THE INDONESIA TEXTILE INDUSTRY

Hexagon socket button head screws (ISO 7380:2004)

Innovation in the Aerospace & Defence Industry - A European Perspective

Title of Presentation

Public Private Partnerships & Idea selection

Special Machines. Ultrasonic Technology Automotive Industry

Belysningsstolpar Del 2: Allmänna krav och mått

This document is a preview generated by EVS

SEFEV. Simulation Environment for Fast ERTMS Validation (2011-EU S)

Ergonomiska principer vid utformning av arbetssystem (ISO 6385:2004) Ergonomic principles in the design of work systems (ISO 6385:2004)

EO-MINERS. The EO-MINERS project: Stakeholders needs and gaps in EO information. Copernicus for Raw Materials Workshop Brussels, Sept.

Creating Innovative Solutions

Low Drift Thrust Balance with High Resolution

Licensed Copy: RRICTISQ RRICTISQ, ISO/Exchange Russia, 23 November 2004, Uncontrolled Copy, (c) BSI

DEUTSCHE NORM May Welds - Working positions Definitions of angles of slope and rotation (IS : 1993) English version of DIN EN IS0 6947

European Technology Platforms

Fästelement Sextandhålsskruvar med cylinderhuvud (ISO 14580:2001) Hexalobular socket cheese head screws (ISO 14580:2001)

Near Net Shape Preforming by 3D Weaving Process

Transcription:

Sixth European Aeronautics Days Innovation for a Sustainable Aviation in a Global Environment 30 th March - 1 st April 2011 Madrid (Spain), Palacio Municipal de Congresos http://www.aerodays2011.org/

Modular Joints for Aircraft Composite Structures March 31 st 2011, Madrid Dr. Llorenç LLOPART P. Development Engineer Materials & Processes at MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 2

Overview MOJO: Partners MOJO: Objectives MOJO: Strategy Task 1: Preforming Task 2: Infusion & Assembly Task 3: Quality assurance & Effect of Defects Task 4: Simulation Task 5: Demonstrators MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 3

MOJO: Partners 1. EADS Deutschland GmbH Germany: Ottobrunn, Manching and Augsburg 2. Biteam AB Sweden: Bromma 3. SECAR Technology GmbH Austria: Mürzzuschlag Hönigsberg 4. Kungliga Tekniska högskolan Stockholm (Royal Institute of Technology) Sweden: Stockholm 5. University of Patras UP Greece: Patras 6. Vyzkumny a Zkusebni Letecky Ustav a.s. (Aeronautical Research and Test Institute, Plc.) Check Republic: Prag MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 4

MOJO: Partners 7. Dassault Aviation France: Saint Cloud 8. Eurocopter Deutschland GmbH Germany: Ottobrunn 9. EADS Innovation Works France France: Suresnes 10. Societe Anonyme Belge de Constructions Aeronautiques Belgium: Brussels 11. Deutsches Zentrum für Luft und Raumfahrt (German Aerospace Center) Germany: Braunschweig and Stuttgart 12. Co operative Research Center for Advanced Composite Structures Limited Australia: Melbourne MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 5

MOJO: Objectives Scope of MOJO was to provide synergy between: preform technology low cost resin infusion, and structural adhesive bonding for a specialised composite material design without fasteners Technical objective was to develop a material driven composite design philosophy, new structural design principles, in order to fully utilise fibre related advantages, thus resulting in weight savings. MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 6

MOJO: Strategy Introduction of a modular design concept using advanced preforms and textile methods for 3D reinforcement in combination with bonding by means of a demonstrator structure. The principle of MOJO laid in the design of CFRP joining elements for pure shear load transfer. The activities were complimented with an effects of defect research task in order to assess structural consequences of most common manufacturing faults and in service damages. MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 7

MOJO: Strategy - The mechanical performance of Modular Joints were determined with an extensive testing program according to the Rouchon pyramid (building block approach). Representative structure testing definition Sub element testing definition to test a structural assembly displaying all the isolated features characterised separately earlier in the test program to test an article focused on joint fittings onto other reinforcement elements including bonding methods and profiles tested previously Assembled panel testing definition to produce assembled panels properties with the studied configuration profiles Individual join element testing definition Basic material properties testing definition to produce join element properties with woven profiles to produce basic materials properties of adhesives and composite and evaluate process parameters MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 8

Task 1: Preforming MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 9

MOJO: Preforming Preforming using compacting techniques Redirection of NCF tapes & Positioning Compacting Fixed Preform MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 10

MOJO: Preforming & 3D Reinforcements Analysis for different types of connections, 3D reinforced joints, and design concepts, altering the failure mode hence improving the mechanical performance. MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 11

MOJO: 3D Woven profiles - From the scientific point of view the focus is laid on the application of especially 3D-Woven preforms in order to alter the failure mechanism in favour of higher limit loads and overall improved mechanical performance. MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 12

Task 2: Infusion & Assembly MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 13

MOJO: Infiltration RTM, VAP and VARI process (Vacuum assisted resin infusion) L Profiles Pi profile Cross section of Pi profile MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 14

MOJO: Infiltration by means of pultrusion MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 15

MOJO: Adhesive bonding - Structures bonded with film adhesive - Structures bonded with paste adhesive MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 16

Task 3: Quality assurance & Effect of of Defects MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 17

MOJO: Quality Assurance Basically by means of NDT and Tolerance/ Assembly management MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 18

MOJO: Effect of Defects NDT, mechanical behaviour and simulations 2% 2% MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 19

Task 4: Simulation MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 20

MOJO: Support adhesive bonding process & on Woven structures Tapered 1 Tapered 2 Rounded Insertion Squeeze flow process optimisation 3D Woven structures MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 21

MOJO: Failure analysis on different structure level testing MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 22

Task 5: Demonstrators MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 23

MOJO: Demonstrator One shot PAX Door Demonstrator (Fubacomp); 2004 Reference Structure for MOJO: Quarter Element for Preform Studies ALCAS / MOJO Shear concentration profile MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 24

MOJO: Industrial Applications and Demonstrator choice MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 25

MOJO: Industrial Applications and Demonstrator choice MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 26

Damage tolerant and structural bonded demonstrator MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 27

MOJO: Damage tolerant and structural bonded demonstrator 1 2 3 Disbonding at 7 8mm at many locations MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 28

MOJO: Damage tolerant and structural bonded demonstrator The demonstrator passed successfully the sequence of tests dealing with limit load, fatigue test until 200000 Cycles, limit load and ultimate load The disbonding area in the Pi has propagated and stopped during fatigue testing. MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 29

Thank you for your attention See the Flap Track demonstrator at Booth 18 Thank to all partenrs and the European Commission MOJO Dr. Llorenç Llopart Prieto, Premium AEROTEC GmbH March the 31 st 2011, Madrid 30