TAPAS. Arnt Offringa Director R&D Fokker Aerostructures Ypenburg, 12 juni 2013

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Annabel Peters
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1 TAPAS Arnt Offringa Director R&D Fokker Aerostructures Ypenburg, 12 juni 2013

2 Wat hebben zij gemeen? 2

3 Product of the Netherlands 3

4 focus op technologieën met groeipotentieel 4

5 Low weight producten door innovatieve materiaalverwerking GLARE tail leading edges/ fuselage panels Thermoplastic wing leading edges 5

6 Product of the Netherlands 6

7 2011: vluchten per dag 2030: vluchten per dag 7

8 8 Vervoer door de lucht is de motor van onze business: 50 jaar groei

9 9 Groeimarkt Azië

10 10 Groen ondanks Groei

11 Ultra-efficient engines 11

12 More powerful & efficient engine higher engine weight strengthened, heavier wing structure less fuel carrying capability lower range 12

13 Materials comparison 13

14 50% of structure weight = carbon composite 14

15 Benefits of composites in aircraft: reduced fuel consumption and CO2 emissions less corrosion & fatigue than for traditional aluminum structure: 787: major overhaul every 13 years instead of every 6 years more comfort through higher moisture content larger windows 15

aluminum structure: 787: major overhaul every 13 years instead of

16 Aerospace OEM objectives: Reduce cost Reduce weight Improve repair and maintenance Environmentally friendly materials and processes 16

17 New products through innovative materials technology (1/4) GLARE 17

18 New products through innovative materials technology (2/4) A380 welded thermoplastic wing fixed leading edge photo Airbus Broughton 18

19 New products through innovative materials technology (3/4) 2013: Dassault SMS 19

20 New products through innovative materials technology (4/4) 20

21 Thermoplastics road map First series production: Fairchild Dornier ribs First primary structure: GV pressure floors First welded assembly: MUC door Fo50 First large scale assembly: Welded fixed wing leading edges A340 A380 outboard fixed leading edge First Induction welded control surfaces G650 CVO TAPAS Primary stiffened skin UD based structure CVO VTP 1990 VTP

22 Project TAPAS Doelen: ontwikkelen thermoplast technologie en bijbehorende demonstrators positioneren Nederland BV voor Airbus en andere opportunities Duur: Budget: Euro 13,2 mio, waarvan 50% overheid 22

23 TAPAS partners fuselage panel demonstrator butt joint, fiber placement, torsion box demonstrator new materials stiffener preforms welding press forming SHM supporting & long term research geen formele partner, wel supporting research, testing 23

24 Project TAPAS thermoplastic technology development: new materials new processes new design concepts design, develop, build & test demonstrators: WP1 fuselage shell (Airbus lead) WP2 torsion box (Fokker lead) 24

25 Material: Ca/UD tape development 25

26 Processes: automation Airborne 26

27 Design concepts: butt joint integrally stiffened skins Technology partly made available to Airbus for development of TAPAS fuselage demonstrator 27

28 Demonstrators Airbus lead 28 Fokker lead

29 Torsion box demonstrator (Fokker lead) 29

30 30

31 MKB deelname Structural Health Monitoring with smart patches Torsion box rib 31

32 Assembly of torsion box demonstrator 32

33 24 juli 2012: failure NLR Photo courtesy NLR 33

34 Project roadmap, torsion box affordable TP UD material Fibre placement Butt Joint Business cases:

35 TAPAS fuselage demonstrator, March 7 th 2013 (to be exhibited on NAG stand at Paris Air Show) 35

business jet tails airliner flaps large airliner rudders,

36 Business opportunities through TAPAS Business case opportunities can now be developed, based on TRL 5/6: business jet tails airliner flaps large airliner rudders, elevators Still needing further development (TRL 3): fuselage structure 36

37 Thermoplastic road map First primary structure: First series Gulfstr production: pressure Fairchild floors Dornier ribs VTP First welded assembly: MUC door Fo50 First large scale assembly: Welded fixed wing leading edges A340 VTP A380 outboard fixed leading edge CVO First Induction welded control surfaces G650 CVO CVO SRP s TAPAS Primary stiffened skin UD based structure TAPAS

38 TAPAS2 business case targets Fuselage Pylons Wet torsion boxes: airliner empennage small wings 38

39 TAPAS2 Duur: Werkpakketten en doelen: Fuselage naar TRL4 Pylons naar TRL 4-6 wet torsion boxes naar TRL 5/6 39

40 TAPAS2 partners 40

41 41 Our dream = thermoplastics 41

42 DE GOUDEN DRIEHOEK IN WERKING TAPAS SAMENWERKING: PPS EN EEN KLANT 42

43 TAPAS-2 in HTSM roadmap 43

44 Tot slot: automotive 44

45 JEC Paris 2013: 80% automotive 45

46 Trend in automotive drive to limit CO2 emissions more electric cars weight reduction through new materials these must be: recyclable affordable thermoplastic composites: processing with cycles times shorter than 1 minute lower cost matrices (PP, PA) 46

47 47

48 Ondanks een andere wereld 48

49 automotive meets aviation 49

50 Dank voor uw aandacht 50

CLIQUEZ POUR MODIFIER LE STYLE DU TITRE

CLIQUEZ POUR MODIFIER LE STYLE DU TITRE Thermoplastic and stabilized dry fiber with automated fiber placement Davy Leboucher, Ing. Dipl 1/28 I. Company Profile SUMMARY II. Current robotic fiber placement III. Thermosets and Aerospace Applications