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National Institute of Aerospace Structural Boron Nitride Nanotube Composite Development February 21, 2014 Catharine Fay NASA Langley Research Center Advanced Materials and Processing Branch Strategic Partner:

Structural Boron Nitride Nanotube Composite … Institute of! Aerospace! Structural Boron Nitride Nanotube Composite Development February 21, 2014 Catharine Fay NASA Langley Research

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National!Institute of!Aerospace!

Structural Boron Nitride Nanotube Composite Development

February 21, 2014

Catharine Fay

NASA Langley Research Center Advanced Materials and Processing Branch

Strategic Partner:

•  Vehicle weight is a primary driver for most NASA missions. Reducing vehicle weight can: –  Expand mission capability –  Reduce launch costs –  Reduce fuel consumption –  Systems analysis shows that

reducing materials mass by 20% leads to a 30% reduction in launch vehicle gross weight

–  Same study indicates a 50% reduction in materials mass reduces launch vehicle gross weight by >60%, enables potential single stage to orbit designs

–  Additional multifunctionality: thermal, radiation protection, sensing capabilities, no corrosion

2

Effect of Materials Mass Reduction on Launch Vehicle Gross Weight

Project Goal

Strategic Overview

Potential Impact: Produce advanced BNNT composites with higher thermal stability, lightweight, no corrosion, tough, and radiation shielding effectiveness

BNNT

0

200

400

600

800

1000

0 20 40 60 80 100 120 140 160 180

Spec

ific

Mod

ulus

, GPa

/(g/c

m3 )

Specific Strength, GPA/(g/cm3)

IM7

M46J

M46J CFRP Al 2219

SiC/Be

TiFoamSand BeAl

Al2O3/Al TiAl IM7 CFRP AlFoam

Nt/P

Nt/Al

0

50

100

150

200

250

300

0 0.5 1 1.5 2 2.5 3 3.5 Spec

ific

Mod

ulus

, GPa

/(g/

cm3 )

Specific Strength, GPA/(g/cm3)

Baseline Materials 5-10 years (TRL = 4-6) 10-20 years + (TRL = 1-3)

Charlie E. Harris, M. J. Shuart, H. Gray, NASA/TM-2002-211664

The structural material properties

for nanotubes significantly

exceed those of current SOA

materials.

Properties of Materials for Vehicle Structure

@ RT SWCNT

BNNT

0

200

400

600

800

1000

0 20 40 60 80 100 120 140 160 180

Spec

ific

Mod

ulus

, GPa

/(g/c

m3 )

Specific Strength, GPA/(g/cm3)

Baseline Materials 5-10 years (TRL = 4-6) 10-20 years + (TRL = 1-3)

Charlie E. Harris, M. J. Shuart, H. Gray, NASA/TM-2002-211664

SiC/Be

TiAl

0

50

100

150

200

250

300

0   0.5   1   1.5   2   2.5   3   3.5  Spec

ific

Mod

ulus

, GPa

/(g/

cm3 )

Specific Strength, GPA/(g/cm3)

@ 700⁰C

Properties of Materials for Vehicle Structure

Technology Areas TA 6 7, 10 and 12

High Temperature Components

Micrometeoroid Protection

Structure: Stronger/Tougher/Lighter

Components

Ultralightweight Wire Insulation

Life Support Membranes

(e.g. water, CO2)

Lightweight Tethers

Radiation Shielding/ Protection

5

Thermal Protection Systems

6 National Institute of Aerospace

4 Aerothermodynamics Branch, LaRC Research Directorate

2 Advanced Sensing and Optical Measurements Branch, LaRC Research Directorate

Radia&on  Sheila  Thibeault1  

Team

1 Advanced Materials and Processing Branch, LaRC Research Directorate

Modeling  Peter  Gnoffo4  

Diagnos&cs  Paul  Danehy2  

Characteriza&on  &  Processing  Cheol  Park6  

Systems  Analysis  Kevin  Earle5  

5 Space Mission and Analysis Branch, LaRC Systems Analysis & Concept Directorate

Synthesis  &  Produc&on  Joseph  Lee2  

BNNT  Team  

Technical  Group  Lead  Catharine  Fay1  

Hoa  Luong3   Godfrey  SauJ6  

Jennifer  Inman2  Stephen  Jones2    

Derek  Liechty4  Vesselin  Yamakov6    

Glen  King1  Sharon  Lowther1  Sang-­‐Hyon  Chu6  Luke  Gibbons6  Jin  Ho  Kang6  Amanda  Tiano6  Samantha  Applin6  Wanda  Gresham3  

Hyunjung  Kim6  

     

3 Materials Experiments Branch, LaRC Research Directorate

NASA BNNT Product Strategy Steps

BN Nanotubes Production Synthesis

7

• Two trained operators. •  Runs on average 3 days a week 4 hours per day. (not including startup and shutdown/harvesting) •  To date has produced approximately 9 grams of material. •  Production rate between 15 and 20 mg per hour. •  Enables purification and dispersion studies. •  Enables fabrication of yarns mats and other structural components. •  Enables Material Transfer Agreements to NIA and Universities.

BNNT Purification Progress

Acid Treatment Purification

Using nitric acid, remove boron

nanoparticles (an impurity) from sample.

•  Boron nanoparticles removed

•  Noticeable damage to the nanotubes resulting in poor quality of the acid-treated sample

•  Acid-treated structural mats have no integrity

Thermal Purification

Use heat to remove boron nanoparticles

and potentially remove boron oxides (i.e.

water soluble impurities).

•  Boron nanoparticle removal alternative

•  Assumption: the darker the BNNT, the higher the boron content/impurity content; visible color change from a darker to a lighter-colored material

•  Further analysis and investigation in progress

Surfactant Purification

Using surfactants, remove all impurities, which includes boron

nanoparticles and amorphous and crystalline BN.

•  Least harmful method to purifying the nanotubes

•  Potential removal of crystalline BN (which cannot be removed via other listed purification methods)

•  Further analysis and investigation in progress; will include sonication and centrifugation as well*

Dispersion studies

•  By surveying a variety of solvents/co-solvents, surfactants, and polymers (A), a solubility region for BNNTs was established (B) using Hansen solubility theory.

•  Extending this knowledge, we generated BNNT structural composites (C) with a plethora of interesting properties (D).

DMF DMF/ Toluene

Toluene Acetone

CTAB Triton X-100

PVP SDBS

Frozen dispersion fabrication method

12% BNNT PU 30% BNNT PU 30% BNNT PU (drop)

50% BNNT PVA

50% BNNT PVA +

sonication

50% BNNT CP2

Before hot-press

20% BNNT PMMA

75% BNNT PVA

1 inch

After hot-press

67% BNNT-PU Pressed 67% BNNT-PU

1 inch New fabrication method simplifies processing for high

weight nanocomposites

This approach can be used to fabricate BNNT + polymers/epoxies and lock in the dispersion conditions

The “frozen dispersion” step is intermediate - the sample is

consolidated during hot-pressing

10% BNNT PVA

67 % BNNT PAN

PU - Polyurethane PMMA - Poly(methyl methacrylate) PVA - Polyvinyl alcohol PAN - Polyacrylonitrile CP2 – LaRC CP2 Polyimide

BNNT Purification, Dispersion, & Spinning

11

TEM images

BNNTs

Non-nanotube BN

BNNT in Chlorosulfonic (CSF) Acid (Superacid): Spontaneous dispersion and debundling

Continuous fiber spinning technology for armchair quantum wire

Matteo Pasquali Departments of Chemical & Biomolecular Engineering and Chemistry,

The Smalley Institute for Nanoscale Science & Technology The Ken Kennedy Institute for Information Technology

Rice University, Houston, TX; [email protected]

AFOSR Low Density Material Program Review Wright Brothers Institute, Dayton (OH), 4 June 2012

FIBER SPINNING

Collaboration with Teijin, manufacturers of Twaron (PPTA) and Toho Tenax (C fibers)

CNT superacid spinning CNT spun fibers

CNT spinning •  BNNT Superacid Spinning in collaboration with Rice University

Rice University (Prof Matteo Pasquali) Stretched 35% aligned MWNT Stretched 25% aligned MWNT

SEM images of Stretched Aligned MWNT Sheets

SEM images of Stretched Aligned MWNT Sheets

Stretched 53% aligned MWNT

•  BNNT Mat/Sheet Formation (filtering) Stretching BNNT Sheet à Composite Tape à Mechanical Tests

Stretching

CNT Sheet Aligned Sheet

Florida State University (Wang/Liang) FSU FSU

Liquid crystalline state

Need purified BNNT for spinning

Three Goals for BNNT Modeling •  Define the environment in which tubes now grow.

–  “Laser Vaporization and Plume Chemistry in a Boron Nitride Nanotube Production Rig”, JTHT, Vol. 27, No. 3, 2013

–  Simulate domain for irradiated droplet suspended in space to better model convection currents – key to understanding nucleation site environment

•  Define the optimum environment for growing BNNTs. –  Observations suggest significant formation of tubes at nucleation sites rising

from heated surface, even before condensation wire is encountered –  If tip growth mechanism: need to simulate nucleation of supersaturated BN

from rising plume on nucleation site(s) –  If root growth mechanism: need to simulate micro-droplets of liquid Boron

ejected from heated surface •  Melts at ~ 2600 K, Boils at ~ 5000 K at 200 psi •  Simulate evolution of absorbed N2, N, and BN in micro-droplet as it rises in plume and

cools –  Plan to explore molecular dynamics approach of Violi et al. (A multi-scale

computational approach for nanoparticle growth in combustion environments) •  Explore modifications to rig by simulation to promote optimum

environment. –  Directed jets may be used to speed or slow the plume dynamics, possibly

inducing recirculation through the hot zone rich in BN, to promote BNNT growth.

T, K

480046004400420040003800360034003200300028002600

Temperature ExceedingBoron Melting Point

Temperature Contours Around 1 mm Radius Boron Droplet

Can jets be used to: (1)  Promote recirculation of micro-droplets through hot

(red) zone rich in N and BN? (2)  Extend the length (or time of residence) in green

zone to extend life of molten micro-droplet before solidification

Optical Diagnostic Techniques for BNNT

•  Need a detailed understand of chemistry and flow physics of nanotube generation and how the process changes under different operating conditions –  Improve and validate simulation/modeling –  Optimize material properties, production rate

•  Specific Goals: –  Determine gas and melt-ball temperatures –  Determine amount of B2, B, BN, N and N2

•  In-situ, on-surface measurement: –  optical pyrometry for surface temperature

•  Off-surface, gas phase measurement: –  High-speed, high-resolution imaging

•  Shadowgraph and visible emission –  Species sensitive imaging (BN PLIF) –  Temperature measurements (CARS)

Partnerships & Collaborations

•  NASA LaRC Center (5 branches) –  Glenn Research Center –  Goddard Space Flight Center –  Johnson Space Center –  Ames Research Center

•  Other Government –  Air Force Office of Scientific

Research –  NIST

•  Commercial –  BNNT, LLC –  Momentive

•  Universities –  UC-Berkeley –  Rice University –  SUNY-Binghamton –  VA Commonwealth University –  University of North Texas –  University of New Hampshire –  NC State –  Hampton University

•  International –  ONERA (France) –  Institutode Nanociencia de

Aragon (Universidad de Zaragoza, Spain)

15

National!Institute of!Aerospace!

Strategic Partner

16

Hydrogen Storage BNNT

Hydrogenated BNNT

The fabrication processes of BN-BN composite precursor and different BN-BN composite structures (fiber, plate composite).

BNNT enables…………………

Multi-Functional All BN-BN Composite

B

CN

C fiber resource

Fig 3. TEM, EELS, and Raman spectra of BCNNT.

BCN Nanotubes

Fig 2. TEM image of

C60-BNNT (endo-doped) UC Berkeley

BxCyNz Nanotube (BCNNT) Development

Radiation Shielding Materials Containing Hydrogen, Boron, and Nitrogen: Systematic Computational and Experimental Study

BNNT BNNT