We investigate the feasibility of utilizing a Fabry-Perot Fiber Optic Strain Rosette Sensor (FP-FOSRS) for the evaluation of the internal strain state of a material system. We briefly describe the manufacturing process for this sensor and point out some potential problem areas. Results of an embedded FP-FOSRS in an epoxy matrix with external resistance strain gauges applied for comparative purposes are presented. We show that the internal and external strain measurements are in close agreement. This work lays the foundation for embedding this sensor in actual composite laminas

Carman, Gregory P.

Case, Scott W.

Claus, Richard O.

Fogg, Brian

Lesko, John J.

English

NASA Technical Reports Server

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Devclopn3eni of an Embedded Fabry Pcrot Fiber Oplic
(FP-FOSRS)
//J - 7 u. -
IS 511_.3
Strain Rosclle SellS jll
Gregory P. Carman, John J. Lesko, Scott W. Case [I], Brian Fogg, Richard O. Claus [2]
[1] Materials Response Group, Engineering Science & Mechanics [2] Fiber & ElccIm-
Optics Research Center, Electrical Engineering Virginia Polytechnic Institute & Sl;lle
University Blacksburg Va., 24061
ABSTRACT: In this paper we investigate the feasibilily(_futilizinga Fabry-Pciot
Fiber Optic Strain Rosette Sensor (FP-FOSRS) for the evahlation of the internal
strain state of a material systeM. We briefly describe the manufacturing process For
IhJs sensor and point out some potential problem areas. Results of an embedded
FP-FOSRS in an epoxy matrix with external resistance slrain gauges applied for
comparative purposes are presented. We show that the internal and external strain
measurements are in close agreement. This work lays Ihe foundation for embedding
this sensor in actual composite laminas.
I. INTRODUCTION
It has been shown [!] that embedded Fabry-Perot Fiber Optic Strain Sensors
(FP-FOSS) provide accurate and reproducible measures of strains within a m:ltcrial
system containing complex damage states. This unique fium _,f internal strain meas-
urement provides the lechnical community a tool to inlerr(_gale the structure's heallh
and gives researchers an instrument to study the basic physic;_l behavior of material
systems. The prospect of utilizing these sensors in this manner has sparked a high de-
gree (_f intere,_t in the scientific community. One advantage lhnt lhe FP-FOSSs have
over their resislance slrain gauge counterparts is that their nleaStlrenlelllS are tlnafFeclcd
by lhe presence of surface shears. Therefore, accurale measurernents of strain in the
presence of high surface shear, such as between plies in a composite panel, is easily
accomplishable wilh the FP-FOSSs. For this reason, as well as the sensor's ability to
give accurate measurements in the presence of EM fields, one can readily understand
that the FOSS's are an attractive alternative to resistance slrain gauges.
While fiber optic sensors do provide useful data, their applications have been limited by
the inherent nature of the l-dimensional measurements (i.e. only along the axis of the
FOSS). In terms of health monitoring, a full 3-dimensional slale of slrain ix required
Io quantitatively assess the material's damage state. Wepresenl in this investigation the
philosophy of using multiple FP-FOSSs oriented in chosen directions to cxperinlenlally
delermine the full strain lensor at a point within a mnlerial. Past researchers have uti-
lized this approach to investigate surface strains [2]. In particular three sensors oriented
within a plane at 0, 45, and 9()"(see Figure I) are embedded in an epoxy coupon far
Icsting. The F;ll_ly-Per(ll IVil-,er Optic Strain Roselte .Rcn_nr I'rI'-FOSRS h:ls a gauge
(NASA-CR-190490) DEVELOPMENT OF AN EMBEOOED
FABRY PgRNT FIBER OPTIC STRAIN ROSETTE
SENSOR (FP-FOSRS) (Virginia Po1#technic
Inst. and State Univ.) 6 p
G3114
N92-29088
Unclas
0105113
https://ntrs.nasa.gov/search.jsp?R=19920019845 2020-03-17T10:50:19+00:00Z
lenglh of nppn_×im;llely 4ran1 and thu_ conslitules poinl me:rqrrenlenls of slrain wilh
Fc'_pect to Ihe size oF Ih¢ Cmllmn. The malerial is subjecled Io variety of loading o,ndi-
lions Io investigale the ability of the internal sensor to m_milor different slalc_ of
inlernal strain. The data obtained from the embedded FOSRS are compared to cla'_,_ical
experiment techniques to demonstrate lhe accuracy of the device. This measurenleilt
nletlmdology gives resenrchers a important tool to undersland lhe nature oF inlelnal
,strain redistribution near dainnged region R_r bolh homogenemL_ ,and in-homngeneou._
systems.
2. MANUFACTUP, ING ..
qhe Fabry-Pcn_t fiber optic strain rosette is cornpriscd of three Sel_aratc Fabry Peror
fiber optic sen,_ol._. E.ach of these scnsols iS 111alltlfflCtUled wilh a gnuge Icngth of 2-Thin1.
"fhe reader is l:eferlcd l(1 {21 for details on the nlanufacturlng process ,and {111the strain
Ineasuromerl( (oc]lnique of tire FP-FOSS. The three FP-FO.qS which comprise lhc
rosette are inilially posilioncd in an nlignment fixture Io orient the sens;ols _il nnlllilln[
:ingles of ()_ , 45 _ , ;111(1Q()_. elite positioned, the XCllSl)lS nre :ldlleled Iogelher wilh a
slnndard epoxy applied at their interseclion defined by point "A" as shown in I"igurc I.
The epoxy prevents inovenlent of the sensol._ iclalive !o one another oilco the rosetle i._
assom bled.
The initial design and nlatlul'acture of the rosctlcs involved phlcing ihc hollow core
I_ortion of the FP-FOSS (the portion which essentially defines the gauge length) a.s clause
as possible to the intersection "A" of the three XellSOl._. The htdlmv cores were pl:lced at
this position in an attempt lo produce a seilsor capable of IlleaStlFillg point strains as
compared to a sensor which would monitor slrains over a finite region. For heallh
monildrh3g purposes point strains are a more tiscful quantily, l lowever, duc to lho for-
malion of all air bubble produced by oulgassillg ,of lhe epoxy (discus.sod in resulls sec-
lion), the hollmv core has been rcposilioned outside of this inlerseclinn' in subsequenlly
mallul'actured sonsois. Picselltly the single triode [_ollion._ _f Ihe sensor intersect al this
h_calion, and lhc lhree htllh)w cores qi'e npproxinlalely 5111131PlOlll Ihis point. Purlher-
lllOle, ill llrl allompt ttl eliminate the pleSence of the air I_ul_blc, Ihc epoxy has been re-
placed in the lll('lle IeCelll SCllSOlX wilh with an AE-10 cpoxy. ".. ..
3. TEST SEFUP
The validation oFslrain nlea._urem0nt.s obtained [rom embedded FP-FOSRS can be lie
:lccomplished by several different methodical :lpl_roaches. l l_,wever, we believe Ihe most
elTicieni, and revealing approach is to investigate the respc>nse ,,f the FP-FOSI?,S in a
homogeneous matrix material. This technique eliminates any extraneous parameter_
which might influence the results, such as strain gradients caused by local distuibances.
By ulilizirig a transparent epoxy as a test matrix, we have lhe ability to visually inspect
the embedded FP-FOSS to determine if any anomalies are present which might inFlu-
ence the l'e.;tllts. This would not be possible in ,'in nctual c_lnposite. Nonetheless, by
using an epoxy xyslcm similar to thai of a gr:_phitelepoxy cnmpnsile, we expect adllexion
characlelislies present in the honmgeneous test specimens ;ind the actual composite
system to also be sinlilar.
In our illVeslig;lli_ln, the FP-FOSRS nre on, bed<led in :l honl_lgcnelitis PI..M-9 elmxY
inaleiial all([ cured lle;ll InOill lelllperalure (i.e. 37_("). llv curing Ihe lesl spocilllen ,it
hollow core
A single mode fiber
0
45
i
aug'e Length
Figuro I' llluslr:ltion of" a Pabry-Pcrot Str_lin R()scllc +_ensor.
Figure 2: Picture oF the <qir bubble <qround the inlCl_ccliol_ oF the h_fllow core
fi I)CI1'_•
a rclalivcly low I.elllpOlature, we have decreased the a111_Killl itf hind Irallsfor due to
Ihermal stresses. If', nf`ler 1osting, we discover that the load liansFer is lnsurficienl, Ihe
nlalelialcall bcctlrod nt a tligllcr tenlperalure. Tile size of th¢10st coupon is sufficienlly
large enough Io prevent boundary conditiolls stich as grip of`Peels fl-onl influoncing the
stiain field prcscnl in lhc region around the the FP-FOSRS.
Once the test cnupnn i_ cured, three resistance strain gauges nie carefully attached tt_ Ihe
sui+f'aco of the lest coupon. Each gauge is positioned on Ihe specimen directly over ,Gild
aligned with a FP-FOSS. The data obtained from the le,vi<_l;Ince sll-aln gauges are com-
pared to tile dat;i f`lom Ihc FP-FOSP, S to valitlale lho inlcrnal nlcastircnlcnls. The lest
spccinlen is mounted in a serve-hydraulic lcsl frame wilh lcnsile and coinprc_sivc Ioa(t_
;ipplied along lhe a×i_ ()f the specimen. This loading lllIl(ldtlCCS a stale of plnnc stress
in n homogoncotls; Illalerln] system at dJ_tallces suPf`JcJcnlly far rronl Ihe gllp_. \¥ilhln
the g,tlago section, the slrains are constant. This stalenlelll, i}[" course, asstinlcs lhc
FP-KOSR.S is unoblru,_lvo. ThereFore, the strain nleasurmonl_ obtained ri(ml lho em-
bedded rrP-FOSP, S gauge should he identical Io i11ca_illglllClllS {H_tnined f'1o111Ihc Sill-
Face nmuntcd resistance slraJil gauges.
We wish to point ()tit thnt the current test methodology al<_o provides a worst cage sce-
nario for the cml-md(lcd frP-FOSRS sensor (not considering damage). For our test
setup, the nlodulus of" the FOSP, S is signif`icantly lalger lhan Ihc lllodulus el" the illalrlx
(i.e. 20 times larger). As; a result, we would expecl tile FOSS SCilSOrS Io slightly ef'f'cccl
lilo sliains being measured. On lhe other lland, ill an nclual colnposile the modulus ot"
Iho SCllSOr arid host hnvc similar magnitudes. As a resull, Ihc FP-FOSP, S embedded in
an epoxy resin is a lllOle obtrusive IllOaSLIIClIIOlI[ than a composite stltlCltlro. So, if' lhc
FP-IvOSRS provides nccuratc data in the holnogeneous sy<qem we would also expect it
Io provide ncci'u<qlo rcsulls in <'lepoxy/graphite conlposile.
4. RESULTS
The inilial FP-FOSRS gauge was mantlfacltlrcd with the h.llmv core tub0 attached ;it
Ihe intersection "k" as stated in the manuracturhlg seclinn. We perflunled uninxia[
colnpressiorl and iellsJ('lll lesl,'_ oil this coupoll. In both loading sequences the [-P-FOSRS
provided erratic data. The strain to load wa_ rOtllld Io be different For each loading cy-
cle. rrurthcrlnorc, Ihe (F gauge provided stralll data COlllparnlively Inrger than Iho cx-
lernal strain gauge. Thc 45 ° and 90" gauges exhibiled little In im slialn, n coniradicition
of the data obalined f`lOill lhe resistance slralll gauges, lnilally, ihi._ dcscrepnncy wns
Ih(+ughl to be dtic Io inndCqtlnle ;idhesJnn bclwCell lilt F()SR lind lhe nl;itli:,_. The c'(ltl-
pen was stibsequenlly cured at all clevnled lentperature (91)'(') Io indtlcc higher residual
thermal stresses, l-lowevei, this did not alter the oulpul oblaincd fl-onl the KP-IvOSRS.
Upon closer inspcciion of the composite (see Figure 2) nn air bubble, larger than the
hollow core's diameter was deteclcd at the hllersection "A". The fOlnlalioil of Ibis nir
I)ubble was believed to be due to the type of" epoxy utilized in lhe 1113ntlf'aCltlrJllg prot'c,g_;
of lhe F'P-FOSRS. This air bubble would thcorelically nller lhe guage lenglh (since it
encnmpasses the hollowcnre) and Ihe load transfer oflhe IrP-FOSS. For this reason,
I.he nlanuf'acturing prncess was altered slightly for stibsequenl sensors. "The ncxl scls of
[:P-FOSRS were nlnnul'nclured with n different epoxy le_in svslclll and Ihe ]_calion (if
lhe hollow core fil_eis wns changed. The hnllmv core ril_crs WelC pl;icc npproxinlalcly
5n1ill otllsJdc of` Ihe inlersec[ion point "A" (<;co Pigtlre 3).
Figure 3: Picture or lhe modified Fabry-Pcrot Sti:_in Rosette soIiSOI'.
A
0 deg. foil sensor
- 45 deg. FP-FOSS
- 0 deg. FP-FOSS
Strain
Fiu;urc 4: COmlx_rison between strain data obi;tinctl from lhc cxlcrl]:ll resistance
slrain _nura,es :lntl Ihc intcrn;ll FP-FOSRS.
rWhile mounling the modified FP-FOSRS in the mold, Ihe single mode portion of the
90 ° sensor was inadvertantly broken, llowever, thedccisim_ was made tostill atlcmpt
to use the sensor. In an effort to reduce the number ofexlraneous parameters in the
measurernent process, the test specimen was cured at 90+'C Io ensure sufficient load
transfer. Resulls of the tension testsperfi+rmed on this specimen nre presented in Figure
4. The maxinlum lensioll applie d to the specirnen was 1000 Ibs. Strail] data obtaine_l
fiom the FP-FOSRS was recorded at various load levels and are presented in this figure
as symbols. Am can rc'adily be seen, the two different sensing melhods are in excellent
ngreemenl. These resull,_ validate the ability of the i:inbeddcd sensor to monil<+r inlcrnnl
sliaills accti ralel.y.
5. CONCLUSIONS
The mancifacturing process utilized in the development of the VP-FOSRS was described.
Potential problem atens such as out-gassing rieai the intersection region of the hollmv
core ill)ors were identified. "lhese prol)lem appeared to be easily solvable by either the
removal of the hollow core fi-om the intersection region or utilizing a different adhcsive
in the irttersection region. Wc demonstratcd that good agreement between the embed-
ded sensors nnd the exlernal strain gauge were obtained once the problem aiens were
i-cmedicd. Tests in the near future will involve enlbcdding the FP-FOSRS between plies
tip an actual graphite/epoxy composite.
6. REFERENCES
I , R.M. Measures, D. l togg, R.D. Turner, T. Vails, & M..l.Gilil)erto "Struclur:llly
Integrated Fiber Optic Strain Rosette", Fiber Optic Smart Structure.s & ,S'l<ins,
Proceedings SPIE 986, pp. 32-42 1988.
, J..l.l.csko, G.P. Carman, B.R. Fogg, W.V. Miller II1, K.L. Reifsnider, R.O.
Claus, "Enlbedded Fabry-Perot Fiber Optic SIr;lin Sensors in lhe Mncromodel
Composites," Oplical Engineering, V. 31 Ntl111. !, pp. 13-23 (1992).


Development of an embedded Fabry Perot Fiber Optic Strain Rosette Sensor (FP-FOSRS)

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