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DELIVERING THE FUTURE OF COMPOSITE SOLUTIONS AEROSPACE QUALIFIED PREPREGS PRODUCT INFORMATION : AEROSPACE QUALIFIED PREPREGS [email protected] www.gurit.com

AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

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Page 1: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

DELIVERING THE FUTURE OF COMPOSITE SOLUTIONS

AEROSPACE QUALIFIED PREPREGS

PRODUCT INFORMATION : AEROSPACE QUALIFIED PREPREGS

[email protected]

www.gurit.com

Page 2: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

1

Gurit offers four resin chemistries:

CHEMISTRY DESCRIPTION PAGE

RE

SIN

CH

EM

ISTR

IES

PHENOLIC Phenolic based chemistry is well established within the aerospace and rail industries where ultimate fire retardancy, low smoke emission and low smoke toxicity (FST) properties are required. Phenolic prepregs are therefore commonly used in interior aircraft components such as side walls and flooring.

2

EPOXY Gurit has a range of fire-retardant epoxy systems suitable for applications where increased mechanical properties are required. They generally exhibit good flame spread properties and can be used in more structural components compared to phenolics such as flooring panels. Where the optimum blend of FST and mechanical properties is required, Gurit epoxy prepregs also can be co-cured with phenolic prepregs. This is an established approach to the manufacture of aerospace flooring sandwich panels.

4

CYANATE ESTER Cyanate ester prepregs provide excellent FST properties and can be used in thermally demanding applications due to their high glass transition temperatures (>200oC). Laminates constructed with cyanate ester prepregs demonstrate very low gas permeability and are volatile-free, resulting in low void and porous free components. This together with their excellent FST and high Tg properties make them ideal for air-conditioning ducting construction in aerospace applications.

6

BENZOXAZINE Gurit’s Benzoxazine prepregs represent the next generation of fire-retardant chemistry where similar FST properties to phenolics are required. An advantage of Benzoxazine chemistry is that it is phenol and formaldehyde free meeting the latest environmental standards. Additionally, during cure, Benzoxazine prepregs are volatile-free resulting in low void and porus-free components, therefore eliminating costly reworking processes associated with the manufacture of phenolic-based prepreg components.

7

ADVANCED COMPOSITE MATERIALS FOR THE AEROSPACE INDUSTRY

Gurit has developed a broad range of strong, light and fire-retardant aerospace materials which

are ideally suited for interior or structural components such as passenger and cargo floor panels,

cabin linings, ceiling panels, air ducts, plenums, overhead compartments, lavatories, galleys, bars,

wardrobes, partitions, seats, flap track and belly fairings, winglets and fins, landing gear doors,

trailing edges and brackets.

COMPONENTS TYPICAL APPLICATIONS PAGE

AE

RO

SPA

CE

AP

PLI

CAT

ION

S A. SECONDARY STRUCTURES, LAMINATES AND SANDWICHES

Belly Fairing, Flap Track Fairing, APU Air Intake and Fairing, D-Nose (leading Edge) Vertical Tail Plane

8

B. INTERIOR 1. ENVIRONMENTAL CONTROL SYSTEM / AIRDUCTS 9

2. PASSENGER INTERIOR Lining, Dado, Ceiling, Lavatories, Galleys

10

3. PASSENGER FLOOR 11

4. CARGO LINING

125. CARGO FLOOR

6. INTERIOR GALLEYS

7. HELICOPTER INTERIOR 13

DUCTINGFLOORING INTERIORS

Front cover image courtesy of Pilatus Aircraft Ltd.

Page 3: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

PF8

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Page 4: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

54

PR

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uced

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r A

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licat

ions

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mit

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oxim

atel

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ual t

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g

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137

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nsity

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sin

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w

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BD

003

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ual

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¬

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S 5

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S 0

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54

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it Zu

llwil

Page 5: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

PR

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ir co

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NAT

E E

STE

R R

ES

IN P

RE

PR

EG

SY

STE

MS

Not

es:

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nfor

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acc

ordi

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o cu

stom

er s

peci

ficat

ions

- Wid

ths

of p

repr

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100

0, 1

270

or u

p to

155

0 m

m (6

1’’)

for

fabr

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pre

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re r

equi

rem

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er li

mit

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o Tg

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catio

n on

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g

PR

OD

UC

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AIN

FE

ATU

RE

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E P

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FOR

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NC

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MM

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DE

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STE

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76

Page 6: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

CH

EM

ISTR

YR

ES

INS

PE

CIF

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SP

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IFIC

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98

Page 7: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

CH

EMIS

TRY

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SPEC

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0 (K

s)

/ PF8

00

(Zu)

AIM

S 05

-10-

001

(A

BS

5047

-07)

AB

S 50

47 /

AIM

S 05

-10-

000

E-G

lass

PHG

600-

68-3

7 / P

F800

-68-

3740

±3

296

8HS

DA

N 4

07-0

7 / D

AN

100

3.1

AIM

S 05

-10-

002

(A

BS

5047

-08)

PH

G60

0-68

-50

/ PF8

00-6

8-50

50 ±

3

296

8HS

DA

N 4

07-0

8 / D

AN

100

3.2

(AIM

S 05

-10-

004+

)PF

800-

G23

1-32

32 ±

326

5O

pen

Wea

ve

AIM

S 05

-10-

008

(A

BS

5047

-02)

PHG

600-

44-5

0 / P

F800

-44-

5050

±3

10

51x

3 C

row

foot

(4H

S)D

AN

407

-02

/ DA

N 1

000.

2

AIM

S 05

-10-

009

(A

BS

5047

-01)

PHG

600-

44-3

7 / P

F800

-44-

3740

±3

105

1x3

Cro

wfo

ot (4

HS)

DA

N 4

07-0

1 / D

AN

100

0.1

AIM

S 05

-10-

010

(A

BS

5047

-04)

PHG

600-

48-5

0 / P

F800

-48-

5050

±3

16

32x

2 Tw

illD

AN

407

-04

/ DA

N 1

001.

2

AIM

S 05

-10-

018

(A

BS

5047

-03)

PH

G60

0-48

-37

/ PF8

00-4

8-37

40 ±

316

32x

2 Tw

illD

AN

407

-03

/ DA

N 1

001.

1

PH83

1

AIM

S 05

-10-

018

(A

BS

5047

-03)

PH

F831

-48-

3740

±3

163

2x2

Twill

DA

N 4

07-0

3 / D

AN

100

1.1

AIM

S 05

-10-

001

(A

BS

5047

-07)

PHG

831-

68-4

040

±3

296

8HS

DA

N 4

07-0

7 / D

AN

100

3.1

AIM

S 05

-10-

003

(A

BS

5047

-41)

PHG

831-

68-4

0 (T

0)40

±3

296

8HS

Cru

shed

Cor

e

AIM

S 05

-10-

009

(A

BS

5047

-01)

PH83

1-44

-40

40 ±

310

51x

3 C

row

foot

(4H

S)D

AN

407

-01

/ DA

N 1

000.

1

AIM

S 05

-10-

012

(A

BS

5047

-39)

PHG

831-

44-4

0

40 ±

3

105

1x3

Cro

wfo

ot (4

HS)

Cru

shed

cor

e

PF80

8

AIM

S 05

-10-

008

(A

BS

5047

-02)

PF80

8-44

-53

50 ±

3

105

1x3

Cro

wfo

ot (4

HS)

DA

N 4

07-0

2 / D

AN

100

0.2

AIM

S 05

-10-

002

(A

BS

5047

-08)

PF

808-

68-5

3 50

±3

29

68H

SD

AN

407

-08

/ DA

N 1

003.

2

AIM

S 05

-10-

009

(A

BS

5047

-01)

PF80

8-44

-40

40 ±

310

51x

3 C

row

foot

(4H

S)D

AN

407

-01

/ DA

N 1

000.

1

AIM

S 05

-10-

010

(A

BS

5047

-04)

PF80

8-48

-53

50 ±

3

163

2x2

Twill

DA

N 4

07-0

4 / D

AN

100

1.2

PF81

1

AIM

S 05

-10-

025

(A

BS

5047

-44)

PF

811-

G22

5-40

40

±3

22

02x

2 C

row

foot

For A

380

PF81

2-G

225-

40

40 ±

3

220

2x2

Cro

wfo

otFo

r A38

0

FMS

2401

FMS

2401

PF81

1-76

28-4

3

43 ±

3 20

0Pl

ain

Wea

ve

PF81

1-44

-50

50

±3

10

51x

3 C

row

foot

PF81

1-68

-40

40

±3

29

68H

S

NTA

624

67N

TA 6

2467

PF81

1-68

-40

40 ±

329

68H

SA

leni

a (S

ukho

i)

PF81

1-44

-50

50 ±

3

105

1x3

Cro

wfo

otA

leni

a (S

ukho

i)

AIM

S 05

-10-

023

(A

BS

5047

-45)

AB

S 50

47 /

AIM

S 05

-10-

000

S2-G

lass

PF81

1-G

226-

4040

±3

190

8HS

For A

380

PF81

2PF

812-

G22

6-40

40

±3

19

08H

SFo

r A38

0

AIM

S 05

-10-

021

(AB

S 50

34-D

)

AB

S 50

34 /

AIM

S 05

-10-

000

Car

bon

PF81

2-C

15-4

5

45 ±

3

193

Plai

n W

eave

A38

0

PF81

1

AIM

S 05

-10-

026

(AB

S 50

34-E

)

PF81

1-C

593-

43

43 ±

3

135

Ope

n W

eave

A38

0

PF81

1-C

15-4

5

45 ±

3

193

Plai

n W

eave

A38

0

AIM

S 05

-20-

004

(AB

S 56

71-2

0)A

BS

5671

/ A

IMS

05-2

0-00

4E-

Gla

ss

/ Car

bon

Hyb

ridPF

811-

F200

38 ±

324

820

0 g/

m²,

12k

UD

48g/

m² E

-gla

ss, P

lain

w

eave

Face

She

et C

once

pt

2. P

asse

ng

er In

teri

or

Typi

cal a

pplic

atio

ns: L

inin

g, D

ado,

Cei

ling,

Lav

ator

ies,

Gal

leys

* K

s =

man

ufac

ture

d at

Gur

it K

asse

l

Zu =

man

ufac

ture

d at

Gur

it Zu

llwil

3. P

asse

ng

er F

loo

r

CH

EM

ISTR

YR

ES

INS

PE

CIF

ICAT

ION

SP

EC

IFIC

ATIO

N F

AM

ILY

FIB

RE

PR

OD

UC

T N

AM

ER

CFA

WR

EIN

FOR

CE

ME

NT

CO

MM

EN

TS%

g/m

²

Epo

xy

EH

250

(Ks)

/ E

P11

2 (Z

u)D

AN

402

E (

WL

8.43

21.1

A)

DA

N 4

02 E

and

DA

N 4

02 F

E-G

lass

Inse

rt: E

HG

250-

68-3

7

40 ±

3

296

8HS

Dia

met

er:

18 –

90

mm

(± 0

.1 m

m)

Thic

knes

s:

5.8

– 16

mm

(± 0

.05

mm

) A

380

EH

420

CD

AN

402

F (

AB

S 50

09-C

40)

Inse

rt: E

HG

420C

-68-

4040

±3

29

68H

S

EP

137

AIM

S 05

-10-

024

(AB

S 56

72-0

1)

AB

S 5

672

/ AIM

S 0

5-10

-000

EP

137-

03-4

0

40 ±

3

48P

lain

Wea

veA

380

EP

121

DA

N 1

180-

02 /

AIM

S 05

-10-

016*

A

BS

500

3 / A

IMS

05-

10-0

00

Car

bon

EP

121-

C15

-53

53

±3

19

3P

lain

Wea

veC

o-C

urin

g w

ith P

F801

IGC

04-

38-1

00

IGC

04-

38-1

00E

P12

1-C

25-4

5

45 ±

3

285

5HS

Coc

kpit

Sec

tion

EP

121-

C57

9-45

45

±3

17

0P

lain

Wea

veC

ockp

it S

ectio

n

EP

137

AIM

S 05

-10-

027

(A

BS

5672

-02)

A

BS

567

2 / A

IMS

05-

10-0

00

S2-

Gla

ss

EP

137-

G22

8-40

40

±3

11

5P

lain

Wea

veA

380

NTA

4365

4N

TA43

654

EP

137-

GR

108/

235-

3232

±3

235

Uni

dire

ctio

nal

Ale

nia

(ATR

)

Car

bon

EP

137-

CR

509/

176-

4949

±3

176

Ale

nia

(ATR

)

EP

137

AIM

S 05

-20-

001

A (

AB

S 56

71-0

1)

AB

S 5

671

/ AIM

S 0

5-20

-000

EP

137-

CR

527/

80-3

5

35 ±

3

80U

nidi

rect

iona

lA

380

AIM

S 05

-20-

001

B (

AB

S 56

71-0

2)

EP

137-

CR

527/

100-

35

35 ±

3

100

Uni

dire

ctio

nal

A38

0

AIM

S 05

-20-

001

C (

AB

S 56

71-0

3)

EP

137-

CR

527/

120-

35

35 ±

3

120

Uni

dire

ctio

nal

A38

0

AIM

S 05

-20-

002

(AB

S 56

71-1

0)

EP

137-

CR

527/

100-

G13

8-50

50

±3

10

0U

nidi

rect

iona

l, 25

g/

scrim

A

380

Phe

nolic

PF8

01

DA

N 1

177-

01 /

AIM

S 05

-10-

019*

(A

BS

5047

-51)

AB

S 5

047

/ AIM

S 0

5-10

-000

E-G

lass

PF8

01-4

4-53

53

±3

10

51x

3 C

row

foot

(4H

S)

Co-

Cur

ing

with

EP

121

DA

N 1

176-

01

(AIM

S 05

-10-

024*

) (D

AN

407

-50)

PF8

01-0

3-40

40

±3

48

Pla

in W

eave

Co-

Cur

ing

with

EP

121

DA

N 1

178-

02 /

AIM

S 05

-10-

013*

(A

BS

5034

-A02

)A

BS

503

4 / A

IMS

05-

10-0

00C

arbo

nP

F801

-C15

-50

50

±3

19

3P

lain

Wea

veC

o-C

urin

g w

ith E

P12

1

DA

N 1

179-

01 /

AIM

S 05

-10-

014*

(A

BS

5034

-B01

)P

F801

-C08

-43

43 ±

3

160

Pla

in W

eave

Co-

Cur

ing

with

EP

121

Ks

= m

anuf

actu

red

at G

urit

Kas

sel

Zu =

man

ufac

ture

d at

Gur

it Zu

llwil

1110

Page 8: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

j j j j j j j

1312

4. C

arg

o L

inin

g

CH

EM

ISTR

YR

ES

INS

PE

CIF

ICAT

ION

SP

EC

IFIC

ATIO

N F

AM

ILY

FIB

RE

PR

OD

UC

T N

AM

ER

CFA

WR

EIN

FOR

CE

ME

NT

CO

MM

EN

TS%

g/m

²

Phe

nolic

PF8

08

AIM

S 0

5-10

-031

A

(AB

S 5

047-

48A

)

AB

S 5

047

/ AIM

S 0

5-10

-00

0S

2-G

lass

PF8

08-G

218-

40

40 ±

3

190

8HS

A38

0

AIM

S 0

5-10

-031

B

(AB

S 5

047-

48B

) P

F808

-G21

8-50

50

±3

19

08H

SA

380

AIM

S 0

5-10

-032

A

(AB

S 5

047-

49A

) P

F808

-G22

0-40

40

±3

30

58H

SA

380

AIM

S 0

5-10

-032

B

(AB

S 5

047-

49B

) P

F808

-G22

0-50

50

±3

30

58H

SA

380

CH

EM

ISTR

YR

ES

INS

PE

CIF

ICAT

ION

SP

EC

IFIC

ATIO

N F

AM

ILY

FIB

RE

PR

OD

UC

T N

AM

ER

CFA

WR

EIN

FOR

CE

ME

NT

CO

MM

EN

TS%

g/m

²

Epo

xyE

P14

1A

IMS

05-

10-0

34 A

AB

S 5

672

/ AIM

S 0

5-10

-00

0S

2-G

lass

EP

141-

G21

8-40

40

±3

19

08H

SA

380,

col

ored

gr

ey

AIM

S 0

5-10

-034

BE

P14

1-G

218-

50

50 ±

3

190

8HS

A38

0, c

olor

ed

grey

EP

121

AIM

S 0

5-10

-035

BE

P12

1-G

218-

50

50 ±

3

190

8HS

A38

0, c

olor

ed

grey

5. C

arg

o F

loo

r

6. I

nte

rio

r G

alle

ys

CH

EM

ISTR

YR

ES

INS

PE

CIF

ICAT

ION

SP

EC

IFIC

ATIO

N F

AM

ILY

FIB

RE

PR

OD

UC

T N

AM

ER

CFA

WR

EIN

FOR

CE

ME

NT

CO

MM

EN

TS%

g/m

²

Phe

nolic

PH

840

MS

1230

E-G

lass

PH

G60

0-68

-37

40 ±

3

296

8HS

BA

/E G

alle

y

A35

0-E

RS

-015

_BP

HG

840-

7628

-43

Whi

te

43 ±

3

200

Pla

inB

A/E

A35

0 G

alle

yP

HG

840-

68-4

0 40

±3

29

68H

S

PH

600

WO

-302

-001

E-G

lass

PH

G60

0-44

-50

50 ±

3

105

1 x

3 C

row

foot

Zodi

ac-S

ell G

alle

ysP

HG

600-

68-5

029

68H

SP

F808

S-G

lass

PF8

08-G

220-

5030

5

CH

EM

ISTR

YR

ES

INS

PE

CIF

ICAT

ION

SP

EC

IFIC

ATIO

N F

AM

ILY

FIB

RE

PR

OD

UC

T N

AM

ER

CFA

WR

EIN

FOR

CE

ME

NT

CO

MM

EN

TS%

g/m

²

Epo

xyE

P12

1A

WM

S44

-004

E-G

lass

EP

121-

68-4

040

±3

29

68H

SA

gust

a A

W10

9

7. H

elic

op

ter

Inte

rio

r

Page 9: AEROSPACE QUALIFIED PREPREGS - gurit. · PDF fileNew development for A380 Fulfils ¬ ABD 0031 Qualified to ¬ ABS 5047 (glass) ¬ AIMS 05-10-023 ¬ ABS 5034 (carbon) ¬ AIMS 05-10-021

Aero Prepregs Bro-6-0615

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