Carbon Fiber SMC Technology for Lightweight · PDF fileCarbon Fiber SMC Technology for...

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Carbon Fiber SMC Technology for Lightweight Structures The Composites Group 1 Matt Kaczmarczyk| Senior Design Engineer Quantum Composites - AS9100C:2009 / ISO9001:2008 1310 South Valley Center Drive Bay City, Michigan 48706-9798 USA Phone: 989-922-3863 ext. 116 Fax: 989-922-3915 [email protected] Tim Langschwager| Lead Development Chemist Quantum Composites - AS9100C:2009 / ISO9001:2008 1310 South Valley Center Drive Bay City, Michigan 48706-9798 USA Phone: 989-922-3863 ext. 120 Fax: 989-922-3915 [email protected]

Transcript of Carbon Fiber SMC Technology for Lightweight · PDF fileCarbon Fiber SMC Technology for...

Carbon Fiber SMC Technology for Lightweight Structu res

The Composites Group 1

Matt Kaczmarczyk| Senior Design Engineer

Quantum Composites - AS9100C:2009 / ISO9001:2008

1310 South Valley Center Drive

Bay City, Michigan 48706-9798 USA

Phone: 989-922-3863 ext. 116

Fax: 989-922-3915

[email protected]

Tim Langschwager| Lead Development Chemist

Quantum Composites - AS9100C:2009 / ISO9001:2008

1310 South Valley Center Drive

Bay City, Michigan 48706-9798 USA

Phone: 989-922-3863 ext. 120

Fax: 989-922-3915

[email protected]

Outline of Presentation

• What is Forged Composite?

• Differences Between CF-SMC and Traditional SMC

• High Flow vs. Low Flow Molding

The Composites Group

• Typical Mechanical Properties of CF-SMC

• Important Characteristics of CF-SMC

• CF-SMC Applications

• Processes Comparisons

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What is Forged Composite?

• Forged Composites: Term for compression molded CF-SMC

• Manufactured by Quantum Composites

• Headquartered in Bay City, Michigan

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CF-SMC First Branded as “Forged Composites”– October 2010 Paris Auto Show

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March 2012 Geneva (Aventador J) April 2012 Beijing ( Urus)

Courtesy: Dr. Paolo Feraboli – Automobili Lamborghini Advanced Composites Structures Laboratory

Carbon Fiber Sheet Molding Compound

• Glass fiber SMC has been around since the 1960’s

• In 1987 Quantum developed epoxy 3k carbon fiber molding compound

• CF-SMC have been in use since early 1990’s

• What is unique about CF-SMC?

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– Quasi-Isotropic properties

– Excellent for fastener-intensive and stiffness dominated parts

– Carbon fiber reinforcement

– High fiber content: Vf 40%+ / Wf 50%+

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Carbon Fiber Sheet Molding Compound

Traditional SMC:

Sheet Molding Compounds (SMC) have traditionally been a low-performance process:

• Glass fiber

• Low fiber content: Vf 18%+ / Wf 25%+

• Low mold coverage/ high flow

• Typically polyester resin

• Higher specific gravity

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CF-SMC:

Feedstock material is chopped carbon fiber with resin

They are similar to prepreg in principle, but not in practice

We define Advanced Compression Molding to differentiate it from the traditional Compression Molding if:

• Carbon fiber

• High fiber content: Vf 40%+ / Wf 50%+

• Typically vinyl ester or epoxy resin but also BMI and phenolic

• Lower specific gravity

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Advanced Compression Molding• Ability to use the CF-SMC in a repeatable and predictable way to form

unique applications

• Minimum molded thickness as low as 0.035 in. (1 mm)

• Reduced variability in strength

• Co-mold with selective UD reinforcement

• Understanding the requirements is the key to material selection

� Excellent for fastener-intensive and stiffness-dominated parts

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� Excellent for fastener-intensive and stiffness-dominated parts

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Example Fabricated (Welded) Steel Tubing Compression Molded CF-SMC

21 lbs 8 lbs

Advanced Compression Molding

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Structural features such as ribs and gussets can easily be molded for

acceptable and even matched performance.

Advanced Compression Molding

• Matched-mold process

Figure 1. Mold is closing Figure 2. Mold is opening after cure

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High Flow MoldingSimilar to traditional SMC - fiber “orientation” is not controlled

Cut the material Weigh the charge Prepared Charge

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Cut the material Weigh the charge

Load the Charge

Courtesy: Premix

Prepared Charge

Low Flow MoldingSimilar to traditional lay-up - fiber “orientation” is more controlled

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Material is precisely cut and placed into mold

• Material flow and charge pattern can effect mechanical properties.

• Creating a uniform direction of fibers does not necessarily translate into improved strength.

• Flow fronts and fiber bunching creating weak areas in the coupons/parts.

40000

45000

Tensile Strength

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Tensile Modulus

High Flow vs. Low Flow MoldingHigh Flow vs. Low Flow Molding

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0

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10000

15000

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25000

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High Flow Low Flow

(psi

)

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2

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High Flow Low Flow

(Msi

)

High Flow

High Flow vs. Low Flow Molding

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Low Flow

High flow specimen showing fiber bunching at

fracture area (Edge Effect at end of flow)

High Flow vs. Low Flow Molding

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Low flow specimen showing a more uniform fiber

displacement resulting in elevated strength properties.

Comparison of Material Performance

40.00

50.00

60.00

70.00

80.00

90.00

100.00

Te

nsi

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th (

ksi

)Tensile Strength vs. Tensile Modulus

Quasi-Iso

Tape

(15.2,174.0)

Ti-6-4

AL6061-T6

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0.00

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20.00

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40.00

0 2 4 6 8 10 12 14 16 18 20

Te

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ksi

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Tensile Modulus (Msi)

Discontinous Carbon Fiber Molding CompoundReference Materials

Glass SMC

Fiber Aspect Ratio

3K – 3,000 filaments per tow (roving)

12K – 12,000 filaments per tow

3k=100 tows

12k=25 tows

• Higher Fiber Aspect Ratio =

– Higher performance

– Lower COV strength values

– Higher notch sensitivity

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12K – 12,000 filaments per tow

50K – 50,000 filaments per tow

50k=6 tows

Comparison of Carbon Fiber Tow (CF -SMC)

30,000

40,000

50,000

60,000

70,000

Te

nsi

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Tensile Strength comparison of ASTM Method

3K SMC

12K SMC

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*ASTM D-638 in the graph above uses “as molded” net shape test specimen.

ASTM D3039, D5766, and D6742 use specimen machined from molded plaques.

0

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20,000

ASTM D-638 ASTM D 3039 MD ASTM D 3039 CMD ASTM D 5766 MD ASTM D 6742 MD

Te

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Test Method

12K SMC

50K SMC

Comparative Properties of CF -SMC

• Moduli as high as prepreg quasi baseline• Unnotched strengths lower than prepreg quasi baseline• Compression higher than tension• Open-hole strengths more appealing• Higher CoV in strength and modulus

� Excellent for fastener-intensive and stiffness-dominated parts

The Composites Group

� Excellent for fastener-intensive and stiffness-dominated parts

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UNT[ksi]

CoVT mod [Msi]

CoVOHT [ksi]

UNC [ksi]

C mod [Msi]

OHC [ksi]

Aluminum 30 2% 10.0 0% 30 30 10.0 30Quasi-isotropic fabric

T700/977-6108 4% 6.0 5% 60 70 4.9 45

3k CF-SMC 47 10% 5.0 10% 37 52 5.4 37

12k CF-SMC 29 18% 5.5 27% 29 42 6.0 33

50k CF-SMC 22 20% 5.5 20%

Comparative Fatigue Curves

25,000

30,000

35,000

40,000

45,000

50,000

UT

S (

psi

)

S-N curve

3K CF-SMC

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Tension – Tension 3Hz

0

5,000

10,000

15,000

20,000

0 200000 400000 600000 800000 1000000

Life (Cycles)

12K CF-SMC

AL6061-T6

Notched Behavior • Specimens containing open holes fail both in the net and gross section

• Typical fastener hole size ¼-inch diameter hole

98.6% failed at hole

1.4% failed away from hole3k

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73.6% failed away from hole

26.4% failed at hole12k

Effects of Defects

• Difficult for Non Destructive Inspection: signal is noisy

• Ultrasonic scans reveal areas of weak reflection or “Hot

Spots” – not necessarily defects

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DE-LAMINATION FLAW

Modulus Variability

• Modulus measurements either

via strain gage or extensometer

• High variability encountered

(approx 19%) much higher than

strength variability (approx 10 %)

• Experiments using gage lengths

of 0.125, 0.25, 0.5, 1.0 and 2.0

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of 0.125, 0.25, 0.5, 1.0 and 2.0

in.

• Also 1.0 in. extensometer

• Longer gages do not yield better

measurements

• Measurements vary along length

and across width of specimens

Modulus Variability

• Digital image correlation (DIC)

• Black speckles are applied to a white background on one side of a specimen

• Images are taken during testing by a pair of digital cameras

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by a pair of digital cameras

• Post processing allows to measure full field strain

• Measurement shows local variations

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Fiber Orientation• High degree of influence on mechanical properties, stiffness

• Changes with high flow vs. low flow molding process and part geometry

• Molded specimens will give high mechanical values due to favorable fiber orientation.

• With cut specimens, the fibers are cut in the gage length reducing the strengths by about 25-30% from molded specimens.

Fibers tend to orient in the direction of flow

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Fibers tend to orient in the direction of flow and along the cavities edge.

ASTM D 3039 CUT FROM PANEL

Fibers are random, but cut at the parts edge

ASTM D 638 MOLDED SPECIMEN

Outline of Presentation

• What is Forged Composite?

• Differences Between CF-SMC and Traditional SMC

• High Flow vs. Low Flow Molding

• Typical Mechanical Properties of CF-SMC

The Composites Group

• Important Characteristics of CF-SMC

• CF-SMC Applications

• Processes Comparisons

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Carbon-Fiber Sheet-Molded Composite Underbody Diffuser for Nissan GTR

Challenge Lower cost, parts consolidation

Solution• Lower part cost vs. prepreg parts

• Corrosion resistance

CF-SMC Applications

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• Corrosion resistance

• High stiffness

• Good impact strength

• Dimensional stability

• Ability to mold in ribs, bosses, changes in thickness (e.g., for attachment points)

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Carbon-Fiber Sheet-Molded Composite Monocoque Tube and Suspension Arm for

Lamborghini Siesto Elemento

Challenge Lower cost, cycle time

Solution• Much lower part cost vs. prepreg parts• Lightweight• High stiffness / strength

CF-SMC Applications

The Composites Group

• High stiffness / strength• Faster cycle time than RTM• Higher volume compression molded• Hybrid structures (e.g., Continuous + Discontinuous

Fibers)

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CF-SMC Applications

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Additional CF -SMC Applications

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Carbon fiber hood inner structure

http://www.sae.org/mags/sve/12288/

Carbon fiber fender support

Injection Molding

RTM

Compression Molding

(CF-SMC)

Transfer

Molding

Composite Fabrication Processes (thermoset)

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Spray-up

Autoclave / Vacuum

Bag

Hand

Lay-up

Production Volume

Too

lin

g C

ost

Thank you!

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