Title presentation 30 pt Bold - Lucht- en Ruimtevaart · 2011: 84.000 vluchten per dag 2030:...

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TAPAS

Arnt Offringa Director R&D

Fokker Aerostructures Ypenburg, 12 juni 2013

Wat hebben zij gemeen?

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Product of the Netherlands

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focus op technologieën met groeipotentieel

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GLARE® tail leading edges/

fuselage panels

Thermoplastic wing

leading edges

Low weight producten door

innovatieve materiaalverwerking

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Product of the Netherlands

2011: 84.000 vluchten per dag

2030: 170.000 vluchten per dag

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Vervoer door de lucht is de motor van onze

business: 50 jaar groei

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Groeimarkt Azië

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“Groen” ondanks Groei

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Ultra-efficient engines

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• higher engine weight

• strengthened, heavier wing structure

• less fuel carrying capability

• lower range

• More powerful & efficient engine

Materials comparison

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50% of structure weight = carbon

composite

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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

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Aerospace OEM objectives:

• Reduce cost

• Reduce weight

• Improve repair and maintenance

• Environmentally friendly materials

and processes

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GLARE®

New products through innovative

materials technology (1/4)

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photo Airbus Broughton

A380 welded thermoplastic

wing fixed leading edge

New products through innovative

materials technology (2/4)

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2013: Dassault SMS

New products through innovative

materials technology (3/4)

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New products through innovative

materials technology (4/4)

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2000 1990 2010

A380

outboard

fixed

leading

edge

First large

scale

assembly:

Welded fixed

wing leading

edges A340

CVO

CVO

First Induction

welded

control

surfaces

G650

First series

production:

Fairchild

Dornier ribs

VTP

First

welded

assembly:

MUC door

Fo50

VTP

First

primary

structure:

GV

pressure

floors

TAPAS

Primary stiffened skin UD

based structure

Thermoplastics road map

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• Doelen:

– ontwikkelen thermoplast technologie en

bijbehorende ‘demonstrators’

– positioneren Nederland BV voor Airbus

en andere opportunities

• Duur:

– 2009 - 2013

• Budget:

– Euro 13,2 mio, waarvan 50% overheid

Project TAPAS

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TAPAS partners

new materials

geen formele partner, wel supporting research, testing

supporting & long term research

SHM

butt joint, fiber placement,

torsion box demonstrator

welding stiffener

preforms press forming

fuselage panel

demonstrator

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• 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)

Project TAPAS

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Material: Ca/UD tape development

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Processes: automation

Airborne

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Design concepts: ‘butt joint’ integrally

stiffened skins

Technology partly made available

to Airbus for development of

TAPAS fuselage demonstrator

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Demonstrators

Airbus lead Fokker lead

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Torsion box demonstrator

(Fokker lead)

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Structural Health Monitoring

with smart patches

MKB deelname

Torsion box

rib

Assembly of torsion box demonstrator

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24 juli 2012:

failure test @ NLR

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Photo courtesy NLR

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affordable TP UD material

Fibre placement

Butt Joint

Business

cases: 2012

Project roadmap, torsion box

TAPAS fuselage demonstrator, March 7th 2013

(to be exhibited on NAG stand at Paris Air Show)

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Business opportunities through TAPAS

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• 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

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Thermoplastic road map

2000 1990 2010

A380

outboard

fixed

leading

edge

First large

scale

assembly:

Welded fixed

wing leading

edges A340

CVO

CVO

First Induction

welded

control

surfaces

G650

First series

production:

Fairchild

Dornier ribs

VTP

First

welded

assembly:

MUC door

Fo50

VTP

First

primary

structure:

Gulfstr

pressure

floors

TAPAS Primary stiffened skin UD

based structure

2020

CVO

SRP’s

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‘TAPAS2’

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TAPAS2 business case targets

• Fuselage

• Pylons

• Wet torsion boxes:

– airliner empennage

– small wings

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TAPAS2

• Duur:

2013 – 2017

• Werkpakketten en doelen:

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Fuselage

naar TRL4 Pylons naar

TRL 4-6

wet torsion boxes

naar TRL 5/6

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TAPAS2 partners

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Our dream

= thermoplastics

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

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TAPAS-2 in HTSM roadmap

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Tot slot: automotive

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JEC Paris 2013: 80% automotive

• drive to limit CO2 emissions

• more electric cars

• weight reduction through new materials

• these must be:

– recyclable

– affordable

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Trend in automotive

• thermoplastic composites:

– processing with cycles times shorter than 1 minute

– lower cost matrices (PP, PA)

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Ondanks een andere wereld …

automotive meets aviation

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Dank voor

uw

aandacht