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Condition Assessment of Kevlar Condition Assessment of Kevlar Composite Materials Using Raman Composite Materials Using Raman Spectroscopy Spectroscopy Glenn Washer Glenn Washer Thomas Brooks Thomas Brooks Civil & Civil & Environmental Environmental Engineering Department Engineering Department University of Missouri University of Missouri Columbia Columbia https://ntrs.nasa.gov/search.jsp?R=20070032686 2020-03-27T04:31:38+00:00Z
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Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Mar 20, 2020

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Page 1: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Con

ditio

n A

sses

smen

t of K

evla

r C

ondi

tion

Ass

essm

ent o

f Kev

lar

Com

posi

te M

ater

ials

Usi

ng R

aman

C

ompo

site

Mat

eria

ls U

sing

Ram

an

Spec

trosc

opy

Spec

trosc

opy

Gle

nn W

ashe

rG

lenn

Was

her

Thom

as B

rook

sTh

omas

Bro

oks

Civ

il &

C

ivil

& E

nviro

nmen

tal

Envi

ronm

enta

l Eng

inee

ring

Dep

artm

ent

Engi

neer

ing

Dep

artm

ent

Uni

vers

ity o

f Mis

sour

i U

nive

rsity

of M

isso

uri ––

Col

umbi

aC

olum

bia

https://ntrs.nasa.gov/search.jsp?R=20070032686 2020-03-27T04:31:38+00:00Z

Page 2: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Ove

rvie

wO

verv

iew

••G

oals

& O

bjec

tives

Goa

ls &

Obj

ectiv

es••

Hyp

othe

sis

Hyp

othe

sis

••K

evla

r Com

posi

te M

ater

ial

Kev

lar C

ompo

site

Mat

eria

l••

Ram

an S

pect

rosc

opy

Ram

an S

pect

rosc

opy

••R

evie

w o

f Lite

ratu

reR

evie

w o

f Lite

ratu

re••

Expe

rimen

tal

Expe

rimen

tal

••R

esul

ts &

Dis

cuss

ion

Res

ults

& D

iscu

ssio

n••

Con

clus

ions

Con

clus

ions

Page 3: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Goa

ls a

nd O

bjec

tives

Goa

ls a

nd O

bjec

tives

••G

oal:

To e

valu

ate

Ram

an sp

ectro

scop

y as

a

Goa

l: To

eva

luat

e R

aman

spec

trosc

opy

as a

po

tent

ial N

DE

tool

for t

he d

etec

tion

of

pote

ntia

l ND

E to

ol fo

r the

det

ectio

n of

st

ress

rupt

ure

in K

evla

r. st

ress

rupt

ure

in K

evla

r.

••O

bjec

tive:

Tes

t a se

ries o

f stra

nd sa

mpl

es

Obj

ectiv

e: T

est a

serie

s of s

trand

sam

ples

th

at h

ave

been

age

d un

der v

ario

us

that

hav

e be

en a

ged

unde

r var

ious

co

nditi

ons a

nd e

valu

ate

diff

eren

ces a

nd

cond

ition

s and

eva

luat

e di

ffer

ence

s and

tre

nds i

n th

e R

aman

resp

onse

tre

nds i

n th

e R

aman

resp

onse

Page 4: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Hyp

othe

sis

Hyp

othe

sis

••R

educ

tion

in st

reng

th a

ssoc

iate

d w

ith st

ress

R

educ

tion

in st

reng

th a

ssoc

iate

d w

ith st

ress

ru

ptur

e m

ay m

anife

st fr

om c

hang

es in

the

rupt

ure

may

man

ifest

from

cha

nges

in th

e po

lym

er a

t a m

olec

ular

leve

l. If

so, t

han

poly

mer

at a

mol

ecul

ar le

vel.

If so

, tha

n th

ese

chan

ges m

ay e

ffec

t the

th

ese

chan

ges m

ay e

ffec

t the

vib

ratio

nal

vibr

atio

nal

char

acte

ristic

s of t

he m

ater

ial,

and

char

acte

ristic

s of t

he m

ater

ial,

and

cons

eque

ntly

the

Ram

an sp

ectra

pro

duce

d co

nseq

uent

ly th

e R

aman

spec

tra p

rodu

ced

from

the

mat

eria

l fr

om th

e m

ater

ial

Page 5: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Prob

lem

Sta

tem

ent

Prob

lem

Sta

tem

ent

••K

evla

r com

posi

te o

ver

Kev

lar c

ompo

site

ove

r --w

rapp

ed p

ress

ure

wra

pped

pre

ssur

e ve

ssel

s (ve

ssel

s (C

OPV

sC

OPV

s ) o

n th

e sp

ace

shut

tles a

re

) on

the

spac

e sh

uttle

s are

gr

eate

r tha

n 25

yea

rs o

ldgr

eate

r tha

n 25

yea

rs o

ld••

Stre

ss ru

ptur

e ph

enom

ena

is n

ot w

ell

Stre

ss ru

ptur

e ph

enom

ena

is n

ot w

ell

unde

rsto

od fo

r un

ders

tood

for C

OPV

sC

OPV

s••

Oth

er

Oth

er C

OPV

sC

OPV

sar

e pl

anne

d fo

r hyd

roge

nar

e pl

anne

d fo

r hyd

roge

n --fu

eled

fu

eled

ve

hicl

es u

sing

Car

bon

com

posi

te m

ater

ial

vehi

cles

usi

ng C

arbo

n co

mpo

site

mat

eria

l

Page 6: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

CO

PVso

n Sh

uttle

Orb

iter

Kev

lar y

arn

Kev

lar/e

poxy

com

posi

te st

rand

Page 7: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

CO

PVso

n Sh

uttle

Orb

iter

•Com

posi

tes u

sed

prim

arily

for t

he h

igh

stre

ngth

-to-w

eigh

t rat

io

Page 8: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Stre

ss R

uptu

re P

heno

men

aSt

ress

Rup

ture

Phe

nom

ena

••M

ater

ial u

nder

con

stan

t loa

d ov

er lo

ng p

erio

ds o

f M

ater

ial u

nder

con

stan

t loa

d ov

er lo

ng p

erio

ds o

f tim

e fa

ils w

ithou

t an

incr

ease

in th

e lo

adtim

e fa

ils w

ithou

t an

incr

ease

in th

e lo

ad••

Fibe

rs a

re st

rain

ed a

t a m

olec

ular

leve

l unt

il ru

ptur

e Fi

bers

are

stra

ined

at a

mol

ecul

ar le

vel u

ntil

rupt

ure

with

ass

ocia

ted

cree

p (e

xact

mec

hani

sm o

f mat

eria

l w

ith a

ssoc

iate

d cr

eep

(exa

ct m

echa

nism

of m

ater

ial

wea

keni

ng is

not

kno

wn)

wea

keni

ng is

not

kno

wn)

••C

urre

ntly

ther

e is

no

know

n m

etho

d to

det

ect s

tress

C

urre

ntly

ther

e is

no

know

n m

etho

d to

det

ect s

tress

ru

ptur

e by

non

dest

ruct

ive

mea

nsru

ptur

e by

non

dest

ruct

ive

mea

ns••

Ram

an sp

ectro

scop

y m

ay b

e a

solu

tion

to th

is

Ram

an sp

ectro

scop

y m

ay b

e a

solu

tion

to th

is

prob

lem

prob

lem

Page 9: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Fibe

r Fai

lure

Fibe

r Fai

lure

••In

fibe

r com

posi

te m

ater

ial,

once

a fi

ber

In fi

ber c

ompo

site

mat

eria

l, on

ce a

fibe

r fa

ils th

e st

ress

is tr

ansf

erre

d to

the

adja

cent

fa

ils th

e st

ress

is tr

ansf

erre

d to

the

adja

cent

fib

ers

fiber

s––

This

can

star

t a c

hain

reac

tion

that

end

s in

a Th

is c

an st

art a

cha

in re

actio

n th

at e

nds i

n a

cata

stro

phic

failu

re o

f the

ent

ire c

ompo

site

cata

stro

phic

failu

re o

f the

ent

ire c

ompo

site

••Lo

cal v

aria

tions

in th

e st

ate

of st

ress

/stra

inLo

cal v

aria

tions

in th

e st

ate

of st

ress

/stra

in

••St

rain

ass

ocia

ted

with

cre

ep m

ay m

odify

the

Stra

in a

ssoc

iate

d w

ith c

reep

may

mod

ify th

e R

aman

spec

tra o

f a fi

ber

Ram

an sp

ectra

of a

fibe

r

Page 10: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

••Fi

bers

may

als

o de

grad

e by

cha

in sc

issi

onFi

bers

may

als

o de

grad

e by

cha

in sc

issi

on––

Bre

akin

g of

B

reak

ing

of in

tera

tom

icin

tera

tom

icbo

nds

bond

s––

Res

ultin

g in

cha

nges

in

Res

ultin

g in

cha

nges

in v

ibra

tiona

lvi

brat

iona

lch

arac

teris

tics

char

acte

ristic

s

Fibe

r Fai

lure

Fibe

r Fai

lure

•Gen

eral

loss

of o

rder

in th

e K

evla

r pol

ymer

–ch

ain

cros

s-lin

king

–– Res

ultin

g in

cha

nges

in

Res

ultin

g in

cha

nges

in v

ibra

tiona

lvi

brat

iona

l cha

ract

eris

tics

char

acte

ristic

s

Page 11: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Ram

an S

pect

rosc

opy

Ram

an S

pect

rosc

opy

••La

ser t

echn

ique

that

is se

nsiti

ve to

La

ser t

echn

ique

that

is se

nsiti

ve to

m

olec

ular

inte

ract

ions

in m

ater

ials

such

as

mol

ecul

ar in

tera

ctio

ns in

mat

eria

ls su

ch a

s K

evla

r, gr

aphi

te a

nd c

arbo

nK

evla

r, gr

aphi

te a

nd c

arbo

n••

Mea

sure

s cha

nges

in fr

eque

ncy

Mea

sure

s cha

nges

in fr

eque

ncy

(wav

elen

gth)

resu

lting

from

inel

astic

(w

avel

engt

h) re

sulti

ng fr

om in

elas

tic

scat

terin

g pr

oces

ses

scat

terin

g pr

oces

ses

Page 12: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Scat

tere

d Li

ght

••R

ayle

igh

scat

tere

d lig

ht (e

last

ic)

Ray

leig

h sc

atte

red

light

(ela

stic

)••

Ram

an sc

atte

red

light

(ine

last

ic)

Ram

an sc

atte

red

light

(ine

last

ic)

Ram

an M

olec

ular

Inte

ract

ion

Page 13: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,
Page 14: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Ram

an S

pect

rosc

opy

Ram

an S

pect

rosc

opy

••Th

e sh

ifts i

n fr

eque

ncy

of th

e in

cide

nt li

ght r

elat

es

The

shift

s in

freq

uenc

y of

the

inci

dent

ligh

t rel

ates

to

the

to th

e vi

brat

iona

lvi

brat

iona

l pro

perti

es o

f the

mol

ecul

epr

oper

ties o

f the

mol

ecul

e––

Vib

ratio

nal

Vib

ratio

nal m

odes

of a

mol

ecul

e ca

n be

mod

eled

and

m

odes

of a

mol

ecul

e ca

n be

mod

eled

and

R

aman

scat

terin

g pr

edic

ted

Ram

an sc

atte

ring

pred

icte

d ••

Pola

rizab

ility

Pola

rizab

ility

of th

e m

olec

ule

of th

e m

olec

ule

••In

tera

tom

icIn

tera

tom

icfo

rces

bet

wee

n at

oms

forc

es b

etw

een

atom

s––

Peak

shift

s dep

end

on

Peak

shift

s dep

end

on

••St

rain

Stra

in••

Cry

stal

linity

Cry

stal

linity

••M

olec

ular

stru

ctur

eM

olec

ular

stru

ctur

e••

Tem

pera

ture

Tem

pera

ture

Page 15: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Vib

ratio

nal

Vib

ratio

nal m

odes

ass

ocia

ted

with

m

odes

ass

ocia

ted

with

pe

aks f

ound

in th

e R

aman

spec

tra

peak

s fou

nd in

the

Ram

an sp

ectra

Fr

eque

ncy

/ cm

-1

Assi

gnm

ent

630,

732

, 786

rin

g vi

brat

ions

84

5 C

-H o

ut-o

f-pla

ne b

endi

ng

863

ring

vibr

atio

ns

1103

C

-H in

-pla

ne b

endi

ng

1181

, 127

7, 1

327,

151

4 C

-C ri

ng s

tretc

hing

13

18

C-H

in-p

lane

ben

ding

15

69

amid

e II

(60%

N-H

ben

ding

; 40%

C-N

stre

tchi

ng

1610

C

-C ri

ng s

tretc

hing

1648

am

ide

I (80

% C

=O s

tretc

hing

; 10%

C-N

st

retc

hing

10%

N-H

ben

ding

) B

. H. S

tuar

t, Po

lym

er B

ulle

tin 3

5,72

7-73

3 (1

995)

Page 16: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

4000

0

5000

0

6000

0

7000

0

8000

0

9000

0

1000

00

1100

00

1200

00

600

800

1000

1200

1400

1600

1800

WAV

ENU

MB

ER (c

m-1

)

RELATIVE INTENSITY (counts/sec) 16

13 c

m-1

1649

cm

-1

Page 17: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Che

mic

al S

truct

ure

of K

evla

r

Kev

lar A

ram

idFi

ber

Page 18: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Kaw

agoe

et a

l. (1

999)

Peak

shift

(~16

13 c

mPe

ak sh

ift (~

1613

cm

-- 11) W

ith S

tress

) With

Stre

ss

Scha

dler

et a

l. (1

995)

Rev

iew

of L

itera

ture

Rev

iew

of L

itera

ture

Page 19: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Scha

dler

et a

l. (1

995)

•As a

mat

eria

l is s

train

ed, t

he in

tera

tom

icdi

stan

ce c

hang

es re

sulti

ng in

a c

hang

e in

the

inte

rato

mic

forc

e, a

nd th

us a

cha

nge

in th

e vi

brat

iona

lfre

quen

cy•

The

~161

3 cm

-1pe

ak e

xhib

its th

e hi

ghes

tse

nsiti

vity

with

stre

ss/s

train

Pras

ad e

t al.

(199

0)•R

aman

ban

d br

oade

ning

due

to d

efec

ts in

th

e m

olec

ular

cha

in

•Def

ects

pos

sibl

y fr

om st

ress

or h

arsh

en

viro

nmen

tal c

ondi

tions

Page 20: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Stua

rt (1

995)

•Use

d a

1064

nm

inci

dent

lase

r to

inve

stig

ate

wat

er a

bsor

ptio

n in

Kev

lar

•Fou

nd a

dec

reas

e in

inte

nsity

for t

he 1

613

cm-1

Ram

an b

and

Page 21: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Expe

rimen

tal

Expe

rimen

tal

••R

enis

haw

Ren

isha

wR

aman

R

aman

inV

iain

Via

spec

trom

eter

spec

trom

eter

••FT

Ram

an sy

stem

FT R

aman

syst

em

Page 22: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

•Typ

ical

Mic

ro-R

aman

Spe

ctro

met

er

Page 23: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,
Page 24: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Spec

tra fr

om K

evla

r with

inci

dent

lase

r Sp

ectra

from

Kev

lar w

ith in

cide

nt la

ser

wav

elen

gths

of 6

47, 7

52 a

nd 1

064

nmw

avel

engt

hs o

f 647

, 752

and

106

4 nm

0

2000

00

4000

00

6000

00

8000

00

1000

000

1200

000

1400

000

1600

000

1800

000

2000

000 60

080

010

0012

0014

0016

0018

00W

AVE

NU

MB

ER (c

m-1

)

RELATIVE INTENSITY

01000

0

2000

0

3000

0

4000

0

5000

0

6000

0

7000

0

8000

0

1064

nm

647

nm

752

nm

Page 25: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Spec

tra fr

om K

evla

r with

Inci

dent

lase

r Sp

ectra

from

Kev

lar w

ith In

cide

nt la

ser

wav

elen

gths

of 4

88 n

mw

avel

engt

hs o

f 488

nm

0

5000

0

1000

00

1500

00

2000

00

2500

00

3000

00 600

800

1000

1200

1400

1600

1800

WA

VEN

UM

BER

(cm

-1)

RELATIVE INTENSITY

488

nm la

ser

Page 26: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

0

5000

0

1000

00

1500

00

2000

00

2500

00

3000

00

3500

00 600

800

1000

1200

1400

1600

1800

WAV

ENU

MB

ER (c

m-1

)

RELATIVE INTENSITY (counts/sec)

90°0°

90°

0°Fi

ber

Alig

nmen

t

Page 27: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Com

paris

on o

f Ram

an P

eaks

for

Com

paris

on o

f Ram

an P

eaks

for

Kev

lar

Kev

lar

Penn

, L.,

Mila

novi

ch, F

., Ra

man

Spe

ctro

scop

y of

Kev

lar 4

9 Fi

ber.

Poly

mer

, 197

9. 2

0(1)

: p. 3

1-36

.

Kim

, P.K

., C

hang

, C.,

Hsu

, S.L

., N

orm

al V

ibra

tiona

lAna

lysi

s of a

Rig

id R

od P

olym

er: p

oly(

p-ph

enyl

ene

tere

phth

alam

ide)

.Pol

ymer

, 198

6. 2

7(1)

: p. 3

4-46

.

Page 28: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Kev

lar y

arn

Kev

lar y

arn

vsvsco

mpo

site

stra

ndco

mpo

site

stra

nd

0

5000

0

1000

00

1500

00

2000

00

2500

00

3000

00

3500

00

4000

00

4500

00

600

800

1000

1200

1400

1600

WAV

ENUM

BER

(cm

-1)

RELATIVE INTENSITY (counts/sec)

Kevla

r/epo

xy s

trand

Kevla

r yar

n

Page 29: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Stra

nd S

ampl

es

Stra

nd S

ampl

es

XX

Step

ped

isot

herm

al s

trand

s; 1

4o5,

21o

5,

23d5

, 23o

5SI

M K

evla

r Str

ands

XX

4560

den

ier,

cure

d an

d un

cure

dA

TK K

evla

r pre

preg

XX

XSN

032,

pre

ssur

e 50

% ~

4200

psi

Flee

t Lea

der T

ank

SN03

2

XX

S/N

007

, 50%

pre

ssur

e ~

4200

psi

Flee

t Lea

der T

ank

SN00

7

XX

X65

% u

ltst

reng

th (6

5 lb

s) a

t diff

eren

t tim

es

and

tem

pera

ture

sTR

I Cre

ep T

est S

ampl

es

XX

orig

inal

virg

in y

arn,

142

0 de

nier

TRI V

irgin

Kev

lar 4

9 Ya

rn

XX

Xor

igin

al v

irgin

stra

nds,

114

0 de

nier

TRI V

irgin

Kev

lar 4

9 St

rand

s

1064

nm

752

nm64

7 nm

488

nmN

otes

Sam

ple

Type

Page 30: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Stra

nd S

peci

men

s St

rand

Spe

cim

ens

yes

761

2F12

yes

929

2F11

yes

904

2F10

yes

901

2F9

room

0Vi

rgin

yes

929

2F1

Faile

d?Te

mp

(°C

)A

ged

(hrs

)Sp

ecim

en

TRI C

reep

Str

ands

SIM

Stra

nds

Page 31: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,
Page 32: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Full

wid

th a

t hal

f max

imum

(F

WH

M) r

atio

Inte

nsity

ratio

4000

0

5000

0

6000

0

7000

0

8000

0

9000

0

0000

0

1000

0

2000

0 600

800

1000

1200

1400

1600

1800

WAV

ENU

MB

ER (c

m-1

)

RELATIVE INTENSITY (counts/sec)

~161

3 cm

-1

~164

9 cm

-1~1

278

cm-1

1278

II ii=

χ12

78FW

HM

FWH

Mi

i=

η

Page 33: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Inte

nsity

Var

iatio

ns (r

elat

ive

to 1

278

cmIn

tens

ity V

aria

tions

(rel

ativ

e to

127

8 cm

-- 11) f

or V

irgin

Stra

nds,

) for

Virg

in S

trand

s, 64

7 nm

inci

dent

wav

elen

gth

647

nm in

cide

nt w

avel

engt

h

Var

iatio

ns in

the

inte

nsity

of d

iffer

ent v

irgin

mat

eria

ls

stde

v: 0

.10

Page 34: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Inte

nsity

Var

iatio

ns (r

elat

ive

to 1

278

Inte

nsity

Var

iatio

ns (r

elat

ive

to 1

278

cmcm-- 11) f

or

) for

V

irgin

Stra

nds

Virg

in S

trand

s vsvs

SIM

spec

imen

s, 64

7 nm

SIM

spec

imen

s, 64

7 nm

stde

v: 0

.09

Page 35: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

VIR

GIN

14o5

21o5

23d5

23o5

VIR

GIN

_hig

h

VIR

GIN

_low

23d5

_hig

h

23d5

_low

1613

cm

-1 b

and

VIR

GIN

23

d5

Inte

nsity

Var

iatio

ns (r

elat

ive

to 1

278

Inte

nsity

Var

iatio

ns (r

elat

ive

to 1

278

cmcm-- 11) f

or

) for

V

irgin

Stra

nds

Virg

in S

trand

s vsvs

SIM

spec

imen

s, 64

7 nm

SIM

spec

imen

s, 64

7 nm

Page 36: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Inte

nsity

Var

iatio

ns (r

elat

ive

to 1

278

cmIn

tens

ity V

aria

tions

(rel

ativ

e to

127

8 cm

-- 11) f

or V

irgin

Stra

nds

) for

Virg

in S

trand

s vsvs

Flee

t Lea

der s

peci

men

s, 64

7 nm

inci

dent

wav

elen

gth

Flee

t Lea

der s

peci

men

s, 64

7 nm

inci

dent

wav

elen

gth

stde

v: 0

.08

Page 37: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

VIR

GIN

SN00

7aSN

007b

SN03

2aSN

032b

VIR

GIN

_hig

hV

IRG

IN_l

owSN

032a

_hig

hSN

032a

_low

1613

cm

-1ba

nd

VIR

GIN

SN

032a

Inte

nsity

Var

iatio

ns (r

elat

ive

to 1

278

cmIn

tens

ity V

aria

tions

(rel

ativ

e to

127

8 cm

-- 11) f

or V

irgin

Stra

nds

) for

Virg

in S

trand

s vsvs

Flee

t Lea

der s

peci

men

s, 64

7 nm

inci

dent

wav

elen

gth

Flee

t Lea

der s

peci

men

s, 64

7 nm

inci

dent

wav

elen

gth

Page 38: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

FWH

M (r

elat

ive

to 1

278

cmFW

HM

(rel

ativ

e to

127

8 cm

-- 11) f

or V

irgin

Stra

nds

) for

Virg

in S

trand

s vsvs

Flee

t Fl

eet

Lead

er sp

ecim

ens,

647

nm in

cide

nt w

avel

engt

hLe

ader

spec

imen

s, 64

7 nm

inci

dent

wav

elen

gth

stde

v: 0

.04

Page 39: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

VIR

GIN

SN00

7aSN

007b

SN03

2aSN

032b

VIR

GIN

_hig

hV

IRG

IN_l

owSN

032a

_hig

hSN

032a

_low

1613

cm

-1 b

and

VIR

GIN

SN03

2a

FWH

M (r

elat

ive

to 1

278

cmFW

HM

(rel

ativ

e to

127

8 cm

-- 11) f

or V

irgin

Stra

nds

) for

Virg

in S

trand

s vsvs

Flee

t Fl

eet

Lead

er sp

ecim

ens,

647

nm in

cide

nt w

avel

engt

hLe

ader

spec

imen

s, 64

7 nm

inci

dent

wav

elen

gth

Page 40: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

FT R

esul

ts

FT R

esul

ts ––

Flee

t Lea

der

Flee

t Lea

der

Page 41: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Peak

shift

s for

all

stra

nd sp

ecim

ens

Peak

shift

s for

all

stra

nd sp

ecim

ens

Page 42: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

1613

cm

1613

cm

-- 11Pe

ak S

hift

with

Pe

ak S

hift

with

A

pplie

d Fo

rce,

647

nm

App

lied

Forc

e, 6

47 n

m

y =

-0.1

472x

+ 1

612.

5

1604

1605

1606

1607

1608

1609

1610

1611

1612

1613

1614

010

2030

4050

60FO

RC

E (l

bs)

PEAK POSTION (cm-1

)

Page 43: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Che

mic

al S

truct

ure

of K

evla

r

Def

ects

in m

olec

ular

str

uctu

re-p

erha

ps fo

r hyd

roge

n bo

nds

~161

3 cm

-1

Page 44: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Fibe

r Opt

ic R

aman

Sys

tem

sFi

ber O

ptic

Ram

an S

yste

ms

The

lase

r bea

m is

dire

cted

thro

ugh

a fib

er o

ptic

pro

be

whi

ch c

an b

e ta

ken

out i

n th

e fie

ld fo

r mea

sure

men

ts

Ren

isha

wA

valo

n In

st.

Page 45: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Sum

mar

ySu

mm

ary

••R

aman

spec

trosc

opy

is b

eing

exp

lore

d as

an

ND

E R

aman

spec

trosc

opy

is b

eing

exp

lore

d as

an

ND

E te

chni

que

to p

redi

ct th

e on

set o

f stre

ss ru

ptur

e in

te

chni

que

to p

redi

ct th

e on

set o

f stre

ss ru

ptur

e in

K

evla

r com

posi

te m

ater

ials

Kev

lar c

ompo

site

mat

eria

ls••

Test

age

d K

evla

r stra

nds t

o di

scov

er tr

ends

in th

e Te

st a

ged

Kev

lar s

trand

s to

disc

over

tren

ds in

the

Ram

an re

spon

seR

aman

resp

onse

••St

reng

th re

duct

ion

in K

evla

r pol

ymer

will

St

reng

th re

duct

ion

in K

evla

r pol

ymer

will

m

anife

st it

self

on th

e R

aman

spec

tra

man

ifest

itse

lf on

the

Ram

an sp

ectra

Page 46: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Con

clus

ions

Con

clus

ions

Ram

an sp

ectro

scop

y ha

s sho

wn

Ram

an sp

ectro

scop

y ha

s sho

wn

––R

elat

ive

chan

ges i

n th

e in

tens

ity a

nd F

WH

M o

f the

~16

13

Rel

ativ

e ch

ange

s in

the

inte

nsity

and

FW

HM

of t

he ~

1613

cmcm

-- 11pe

akpe

ak••

Red

uctio

n in

rela

tive

inte

nsity

for c

reep

, fle

et le

ader

, and

SIM

Red

uctio

n in

rela

tive

inte

nsity

for c

reep

, fle

et le

ader

, and

SIM

spec

imen

s com

pare

d to

the

virg

in st

rand

s sp

ecim

ens c

ompa

red

to th

e vi

rgin

stra

nds

••In

crea

se in

FW

HM

has

bee

n ob

serv

ed fo

r the

cre

ep a

nd fl

eet

Incr

ease

in F

WH

M h

as b

een

obse

rved

for t

he c

reep

and

flee

t le

ader

spec

imen

s com

pare

d to

the

virg

in st

rand

s le

ader

spec

imen

s com

pare

d to

the

virg

in st

rand

s ••

Cha

nges

in th

e R

aman

spec

tra m

ay re

sult

from

redi

strib

utin

g C

hang

es in

the

Ram

an sp

ectra

may

resu

lt fr

om re

dist

ribut

ing

load

s with

in th

e m

ater

ial d

ue to

the

disr

uptio

n of

hyd

roge

n lo

ads w

ithin

the

mat

eria

l due

to th

e di

srup

tion

of h

ydro

gen

bond

ing

betw

een

crys

talli

tes o

r def

ects

in th

e cr

ysta

llite

s fro

mbo

ndin

g be

twee

n cr

ysta

llite

s or d

efec

ts in

the

crys

talli

tes f

rom

agin

g th

e K

evla

r stra

nds

agin

g th

e K

evla

r stra

nds

––Pe

ak sh

iftin

g ha

s not

bee

n ob

serv

ed to

dat

e. A

naly

sis i

s Pe

ak sh

iftin

g ha

s not

bee

n ob

serv

ed to

dat

e. A

naly

sis i

s on

goin

gon

goin

g ……

……

––St

ress

mea

sure

men

ts m

ay p

rovi

de a

tool

in th

e sh

ort t

erm

Stre

ss m

easu

rem

ents

may

pro

vide

a to

ol in

the

shor

t ter

m

Page 47: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Que

stio

ns?

Page 48: Condition Assessment of Kevlar Composite Materials Using ...Condition Assessment of Kevlar Composite Materials Using Raman Spectroscopy ... Fiber Failure •In fiber composite material,

Than

k Y

ouTh

ank

You