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

TAPAS

Arnt Offringa Director R&D

Fokker Aerostructures Ypenburg, 12 juni 2013

Wat hebben zij gemeen?

TAPAS & TAPAS2, Juni 2013 2


Product of the Netherlands

4

focus op technologieën met groeipotentieel

TAPAS & TAPAS2, Juni 2013


GLARE® tail leading edges/

fuselage panels

Thermoplastic wing

leading edges

Low weight producten door

innovatieve materiaalverwerking


Product of the Netherlands

2011: 84.000 vluchten per dag

2030: 170.000 vluchten per dag

7 TAPAS & TAPAS2, Juni 2013

Vervoer door de lucht is de motor van onze

business: 50 jaar groei


Groeimarkt Azië


“Groen” ondanks Groei



Ultra-efficient engines


• higher engine weight

• strengthened, heavier wing structure

• less fuel carrying capability

• lower range

• More powerful & efficient engine

Materials comparison


50% of structure weight = carbon

composite



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


Aerospace OEM objectives:

• Reduce cost

• Reduce weight

• Improve repair and maintenance

• Environmentally friendly materials

and processes


GLARE®

New products through innovative

materials technology (1/4)


photo Airbus Broughton

A380 welded thermoplastic

wing fixed leading edge




2013: Dassault SMS






http://imagebank.tencate.com/~imagebank/pages/view.php?ref=1688&search=&offset=0&order_by=relevance&sort=DESC&archive=0&k=


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


• 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


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


• 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


Material: Ca/UD tape development


Processes: automation

Airborne


Design concepts: ‘butt joint’ integrally

stiffened skins

Technology partly made available

to Airbus for development of

TAPAS fuselage demonstrator


Demonstrators

Airbus lead Fokker lead


Torsion box demonstrator

(Fokker lead)


Structural Health Monitoring

with smart patches

MKB deelname

Torsion box

rib

Assembly of torsion box demonstrator


24 juli 2012:

failure test @ NLR


Photo courtesy NLR


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)


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

37

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

TAPAS & TAPAS2, Juni 2013

‘TAPAS2’

37

TAPAS2 business case targets

• Fuselage

• Pylons

• Wet torsion boxes:

– airliner empennage

– small wings


TAPAS2

• Duur:

2013 – 2017

• Werkpakketten en doelen:


Fuselage

naar TRL4 Pylons naar

TRL 4-6

wet torsion boxes

naar TRL 5/6


TAPAS2 partners

41

Our dream

= thermoplastics


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


TAPAS-2 in HTSM roadmap



Tot slot: automotive


JEC Paris 2013: 80% automotive

• drive to limit CO2 emissions

• more electric cars

• weight reduction through new materials

• these must be:

– recyclable

– affordable


Trend in automotive

• thermoplastic composites:

– processing with cycles times shorter than 1 minute

– lower cost matrices (PP, PA)


Ondanks een andere wereld …

automotive meets aviation



Dank voor

uw

aandacht

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

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