nanofibers and nanocomposites for aerospace applications

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Nanofibers and Nanocomposites for aerospace applications Prof. Yuntian Zhu Dept. of Materials Science and Engineering 20μm

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Page 1: Nanofibers and Nanocomposites for aerospace applications

Nanofibers and Nanocomposites for aerospace applications

Prof. Yuntian Zhu

Dept. of Materials Science and Engineering

20µm

Page 2: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

2

www.ncsu.edu/nano Nano for Safety and Environment

NONWOVENS COOPERATIVERESEARCH CENTER

NCSU

IndustryState of NC

2 um

1 um

20 nm

•  Nanofiber Filtration: Clean Water and Air –  Nanofibers for air, water

filtration devices –  Reduce energy consumption –  “Smart Filters” – Integrated

sensor devices

•  Protection –  Fire, Chemicals –  Particulates, Toxins

500nm

Behnam Pourdeyhimi Nonwovens Institute

Page 3: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano Current Nanofiber Fabrication Technology

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•  Currently, the most commonly-used method for producing nanofibers is electrospinning (90% publications on nanofibers are based on electrospinning)

•  However, the mass production of nanofibers by electrospinning is limited by its low production rate (<100 mg per hour), poor safety, and high cost

•  More importantly, electrospun nanofibers are mechanically weak due to the lack of molecular orientation, and they are not suitable for composite applications

Electrospinning:

Page 4: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano

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Our Approach: Centrifugal Spinning

20µm

•  Our preliminary results demonstrated that the production rate of the centrifugal spinning process is 600 times greater than that of typical single-syringe electrospinning

•  More importantly, the stretching of jets during centrifugal spinning results in a high degree of molecular orientation, thereby leading to excellent mechanical properties that cannot be obtained by other methods

Polyacrylonitrile nanofibers by centrifugal spinning

•  Our approach is to use the centrifugal spinning technique to produce ultra-strong nanofibers for composite applications at high speed, high safety, and low cost

Collector

Liquid  jet

Spinning  head

Polymer  solution  or  melt

Spinning  head

JetNanofiber  sheet

Substrate

(A) (B)

Page 5: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano

  Four key factors for the best properties in CNT composites

1.  Straight, non-waviness: To make all CNTs carry the load simultaneously (unique for CNTs)

2.  Good Alignment: For a CNT to carry load effectively, it has to be aligned in the loading direction

3.  Long individual CNTs: Long nanotubes are more effective in carrying load

4.  High nanotube volume fraction: The composite strength increases with increasing nanotube volume fraction

What are issues of the CNT composites?

Page 6: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano Our New Approach for Fabricating CNT Composites

•  Long CNTs •  High volume fraction •  Good alignment •  Good preliminary properties •  Potentially produce the multifunctional CNT composite with

–  Strength much higher than current carbon fiber composites –  High electrical conductivity –  High thermal conductivity

Page 7: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano Spray Winding CNT Composites

Conducive to low-cost, large scale production

Stretch-Spray-winding Automatic stretch-winding machine

Page 8: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano High strength, stiffness, electrical

conductivity, and thermal conductivity

Page 9: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano Unidirectional Carbon Nanotube - Carbon Composites:

Polyacrylonitrile (PAN) as Precursor

Polymer Infiltration and Pyrolysis: PAN

CNT/PAN composite precursor (dip winding)

Stabilization at 250 °C for 2hrs, 320°C for 25 min

(under tension)

Carbonization at 1300 °C (under compression )

Graphitization at 2150 °C

40-60 walls Diameter: 35-60 nm Length: 900 µm

Resultant CNT-carbon composites: §  Relatively high carbon yield from PAN (50-55%) §  Long, aligned CNT structure with weight fraction of 5~20% §  Providing scaffold for PAN graphitization, enhance thermal stability of composites,

which in turn strengthen the CNTs

1, 2, 5% PAN in DMF were used Good infiltration obtained

Page 10: Nanofibers and Nanocomposites for aerospace applications

NC STATE UNIVERSITYNC STATE UNIVERSITY

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www.ncsu.edu/nano Mechanical and electrical properties

Precursor After Carbonization