cetex-tc1100[1]

7/28/2019 CETEX-TC1100[1]

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TenCaTe advanCed ComposiTes Usa, inC

Technical DaTa

Product descriPtion

Cetex® tC1100 is a smi-crysallin polyphnyln sulid hrmoplasic composi UD ap.

I ors clln rsisanc o chmicals and solvns, is lam rardan and combins ou-sanding oughnss wih high mpraur prormanc. C tC1100 is ord wih sandard

or inrmdia modulus carbon ibr or S-2 glass ibr. C tC1100 has a vry low void con-

n (<1%). typical carbon uniap widh ord is 12 inchs/304.8 mm.

Product tyPe

Polyphnyln Suld (PPS)thrmoplasic Rsin Sysm

service temPerature

200°F/93°C

Features

• Ambienttemperaturestorage • Flameretardant • Lowmoistureabsorption • Goodimpactresistance • 3-5minutethermoformingcycles • Goodstructuralperformance • Outstandingsolventresistance • Verylowvoidcontent

tyPical aPPlications

• PrimaryAircraftStructure • SecondaryAircraftStructure • AccessPanels,RibStiffeners,

Bracks, Condui, Flooringtg ..............................................200°F/93°C

tm ............................................536°F/280°C

shelF liFe

Indenite at 77°F (25°C)

ceteX®

tc1100 PPsr s

MECHANICAL PROPERTIES - CETEx TC1100 PPS AS-4

DatadeliveredonAS-4,150gsmFAW,resincontentof35%byweight,42%byvolume.Prepregarealweight227gsm.

Prprty cdt Tt Mtd Rut

Tensile Strength (0°) RTD ASTM D 3039 313 ksi (2158 MPa)

Tensile Modulus (0°) RTD ASTM D 3039 13.1 Msi (90 GPa)

Poisson’s Ratio RTD ASTM D 3039 0.33

Tensile Strength (90°) RTD ASTM D 3039 5.7 ksi (38 MPa)

Tensile Modulus (90°) RTD ASTM D 3039 1.42 Msi (9.8 GPa)

Compressive Strength (0°) RTD ASTM D 6641 110 ksi (758 MPa)

Compressive Modulus (0°) RTD ASTM D 6641 16.8 Msi (116 GPa)


Compressive Modulus (0°) RTD ASTM D 6410 17.3 Msi (119 GPa)


In-Plane Shear Strength RTD ASTM D 3518 11.9 ksi (82 MPa)

In-Plane Shear Modulus RTD ASTM D 3518 0.5 Msi (3.5 GPa)

In-Plane Shear Strength V-Notch RTD ASTM D 5379 18.1 ksi (125 MPa)

In-Plane Shear Modulus V-Notch (3) RTD ASTM D 5379 5.4 Msi (37 GPa)

Flexural Strength (0°) RTD ASTM D 790 251 ksi (1730 MPa)

Flexural Modulus (0°) RTD ASTM D 790 19.7 Msi (136 GPa)

Flexural Strength (90°) RTD ASTM D 790 7.6 ksi (52 MPa)

Flexural Modulus (90°) RTD ASTM D 790 0.9 Msi (6.2 GPa)

Interlaminar Shear Strength (SBS) RTD ASTM D 2344 12.0 ksi (82.7 MPa)

Open Hole Compressive Strength RTD ASTM D 6484 38.7 ksi (266 MPa)

Compression Ater Impact Strength RTD ASTM D 7137 31.4 ksi (216 MPa)

Compression Ater Impact Modulus RTD ASTM D 7137 6.9 Msi (47.6 GPa)

(1) Cured ply thickness average is .0056” (0.14 mm). (2) Density is 0.058 lb/in3 (1.6 g/cm3).(3) Measured at 5% oset.

MECHANICAL PROPERTIES - CETEx TC1100 PPS IM-7

DatadeliveredonIM-7,146gsmFAW,resincontentof34%byweight,41%byvolume.Prepregarealweight221gsm.

Prprty cdt Tt Mtd Rut

Tensile Strength (0°) RTD ASTM D 3039 414 ksi (2854 MPa)

Tensile Modulus (0°) RTD ASTM D 3039 22.1 Msi (152 GPa)

Tensile Strength (90°) RTD ASTM D 3039 6.2 ksi (42.7 MPa)

Tensile Modulus (90°) RTD ASTM D 3039 1.4 Msi (9.7 GPa)


In-Plane Shear Tension RTD ASTM D 3518 10.2 ksi (703 MPa) of 4 TC1100_DS_031212

Verylowvoidcontent,500xviewofsingleplyCetexUD prprg, as producd, wihou urhr consolida-tion.Averagevoidlevelof<0.2%withevenberandrsin disribuion.

PRocessing oPTions

Press,Thermoorm,in-situ ATL or Autoclave

7/28/2019 CETEX-TC1100[1]



Technical DaTa

ceteX®

tc1100 PPsr s

Pg G f ceteX PPs*tp cp m

Cetex® PPS hrmoplasic composi marials rom tnCa ar procssd by haing h

marial abov h PPS mling poin and molding i and cooling i undr prssur o h dsird

shap. Bcaus no chmical chang occurs o h PPS mari, procssing is vry rapid. th quick

asy procssing o Cetex marials is also mad possibl bcaus o h rapid crysallizaion

ra o h PPS mari. th ky hrmal procssing paramrs ar:

Ml tmpraur .................................................................................. 560°F(293°C)

typical Procssing tmpraur ............................................................ 625°F(330°C)

tnCa can also produc Cetex owprgs & simpl prols (round rods, ovals,

rcangls, c.). tnCa also has h capabiliy o chop h owprgs & simpl prols ino

discr lngh long br hrmoplasic yp marials or injcion or comprssion molding

yp procsss.

Automated ProcessesBlow ar svral ampls o auomad procsss ha ar uilizd and availabl in h

mark oday. Boh procsss uiliz similar prmiss in ha hy limina h nd or auoclav

consolidaion o hrmoplasic composi pars, hrby dramaically rducing h cos o

producing coninuous br composi srucurs.

1. Fiber Placement with In Situ Consolidation Thisprocessutilizesnarrowwidthtapestypically0.25–1inches(6–25mm)asitscompositematerial

mdium and lays down, has via ho gas, lasr, or ohr haing mhods and consolidas hcomposi marial ono h ool, in siu, wihou h nd or urhr consolidaion procsss.

PhotocourtesyofAutomatedDynamics www.auomaddynamics.com

PhotocourtesyofAFPT www.ap.biz/

2. Rapid Lamination / Forming this procss uss widr UD aps ypically ≥2inches(50mm)widthtorapidlylaydown and consolida h hrmoplasic composi marial ino an nginrd lamina srucurha can hn b ransormd ino pars via a scondary comprssion hrmoorming procss.

Automated tape laying o tailoredblank ollowed by consolidation.

The consolidated fat laminate is thenthermoormed to a 3-D nal shape.

Phoo Coursy o FibrForgwww.brorg.com

Phoo coursy o tnCa

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Technical DaTa

ceteX®

tc1100 PPsr s

Press Lamination:AlaminatecanbepressmoldedfromanyCETEXprepregbystackingtwoor mor plis in h dsird orinaion ino a picur ram mold, ransrring h assmbly o a

heatedplatenpresswhereitisbroughttoapproximately610°F(320°C)atcontactpressureuntil

thematerialreachestemperature.Thepressureshouldthenbeincreasedto100-400psi(7-21bar)

andheldforapproximately15-30minutes.Theassemblyshouldthenbequicklytransferredtoa

chilld plan prss and coold o room mpraur whil prssur is mainaind.

Autoclave Lamination:AutoclaveConsolidationisusedforfabricatinglaminatesfromanyCetex prprg ap. Individual layrs ar sackd in h dsird orinaion and vacuum baggd

(vacuumshouldbemaintainedthroughouttheentireprocess).Ahightemperaturebaggingmaterial,

such as Kapon polyimid should b usd. th assmbly should hn b placd in h auoclav

andbroughttoapproximately610°F(320°C),atwhichtimethepressureisincreasedfromambient

to100-150psi(7-10bar)andmaintainedforaround20-30minutes.Thepartshouldthenbecooledtoroomtemperatureata5-20°Ccooldownrate.

Thermoforming Laminates into Shapes: thrmoorming is usd o convr a fa consolidad

coninuous br rinorcd lamina ino a compl shap wih no chang in saring lamina

thickness.Thelaminateshouldbeheatedtoaround610°F(320°C)inaninfraredorsimilaroven

andthenquicklytransferredtoamatchedcore/cavitymoldwhereitcanbeformedat150-600psi

(10-40 bar). For opimum propris and ormabiliy, haing o h composi lamina should ak

nolongerthan8minutes.Overallpartproductioncycletimesarebetween2-10minutes,depend -

ing on marial hicknss and par gomry. Producion ooling consiss o machind aluminum

halvs, on ha has a complian layr o cas silicon, and an associad lamina nsioning

sysm o prvn wrinkling wihin h par bing hrmoormd.

Cutting and Machining: thrmoplasic composi laminas and hrmoormd pars canb machind wih d ras and ip spds similar o hos usd whn machining brass.

th ollowing ar som gnral guidlins:

CircularSaw: Diamond-grit-edgebladeof220grit.Bladespeed:6000fpm

(1830 mpm) wih war or soap soluion as coolan.

Fd ras dpnd on hicknss.

TurningOperations: CuttingSpeed:350-400fpm(105-120mpm)forhighspeedtools,

1500-2500fpm(180-455mpm)forStelliteorcarbidetools,and

2000-4000fpm(600-1200mpm)fordiamondtools

MillingOperations: Tipspeed:250-450fpm(75-135mpm)forcarbideanddiamondtools

Plungefeedrate:0.5-1fpm(0.15-0.30mpm)

3. Continuous Compression Molding In his muli-sp procss, mulipl plis o hrmoplasic uniap is had in a mold andprssd ino a lamina. this lamina is hn prssd ino a mold and hrmoormd o h

desiredprole.Analstepthenmoldswithheatandgentlepressureintothecurvedprole hrough a procss calld coninuous comprssion molding. Ims such as clips, rails, bamsand prol ar manuacurd in his yp o procss.

PhotoCourtesyofACM/XperionAerospace www.acm-n.d

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ISO 9001AS 9100

Registered

www.tt.m

e-m: [email protected]

2450 Cordelia Road

Fairfeld, CA 94534 USA

Tel 707 359 3400

Fax 707 359 3459

TENCATE AdvANCEd COMPOSITES USA, INC.

18410 Butterfeld Blvd.

Morgan Hill, CA 95037

Tel 408 776 0700

Fax 408 776 0107


Technical DaTa

ceteX®

tc1100 PPsr s

DrillingOperations: FeedRate:0.008-0.016in/rev(0.2-0.4mm/rev)

Drillspeed:150-300fpm(45-90mpm)

Drillpointangles:60°forthinparts,90°forthickparts Clearanceangle:15°

Tapping: Toolrakeof0°to5°negative

Shearing: Thicknessesupto0.125inch(3.2mm)

Joining: thrmoplasic composis can b joind via mchanical asnrs, adhsiv bonding, or

usion wlding.

Srong adhsiv bonds ar possibl wih poy adhsivs whn PPS suracs ar cland wih a

suiabl dgrasing solvn (i.. MeK), abrasiv ramn (i.., abrasion whls, sand papr, or

gritblastedwith#100or#200AluminumOxide).Thesurfaceenergymayalsobeenhancedbyfam/corona ramn, chromic acid ching, lasr ramn, or plasma chniqus. epoy

lmsorpasteswithcuretemperaturesupto350°F(177°C),anaerobics,siliconesealers,andcyanoacrylas ar civ adhsivs dpnding on spcic rquirmns.

Cetex® PPS basd composis may also b bondd using convnional hrmoplasic wlding

chniqus. PPS basd marials hav vry high ml mpraurs and considrabl amouns o

nrgy mus b pu ino h inrac o achiv a good bond. Saisacory rsuls hav also bn

obaind using inducion or rsisanc wlding.

Painting: Cetex® PPS composi suracs can b paind wih a variy o producs. I is

rcommndd ha a painabl (non-silicon) mold rlas b usd, i possibl, during h molding

o all suracs o b paind. I a silicon or tfon mold rlas is usd during molding, lamina

and par suracs may rquir abrasion prior o paining. In all cass, suracs mus b wipd wiha suiabl solvn (.g. MeK, DuPon 3919S) o rmov oils, rlas agns, or ohr impuriis.

Health & Safety: Halh and say inormaion on handling and procssing tnCa

composi marials is dscribd in a Marial Say Daa Sh availabl rom tnCa

AdvancedCompositesUSA,Inc.ToobtainthisoranyotherinformationaboutTenCatePPS

thermoplasticcompositematerials,contact:TenCateAdvancedCompositesUSA,Inc.attheaddrsss and lphon numbrs blow.

of 4 TC1100_DS_031212

Revised 03/2012

All data given is based on representative samples

of the materials in question. Since the method and

circumstances under which these materials are processed and tested are key to their performance,

and TenCate Advanced Composites USA, Inc.

has no assurance of how its customers will use

the material, the corporation cannot guarantee

these properties.

cetex-tc1100[1]

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