Thermal comfort materials and applications at NSRDEC Local Thermal... · Thermal comfort materials...

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Stephen A. Fossey Team Leader, Ballistics & Blast Science Team Warfighter Directorate 18 January 2017 Thermal comfort materials and applications at NSRDEC ARPA-E UNCLASSIFIED/ Public Release [email protected]

Transcript of Thermal comfort materials and applications at NSRDEC Local Thermal... · Thermal comfort materials...

Stephen A. FosseyTeam Leader, Ballistics & Blast

Science TeamWarfighter Directorate

18 January 2017

Thermal comfort materials and applications at NSRDEC

ARPA-E

UNCLASSIFIED/ Public Release

[email protected]

• Overview of Natick Soldier R,D & E Center

• Application of responsive material to cold weather clothing

• Links for further information on NSRDEC and AFFOA

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Outline

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Army Materials Research Enterprise

Army Material Command

ECBCEdgewood Chemical

Biological Center

CERDECCommunications

- Electronics RDEC

ARDECArmaments

RDEC

TARDECTank Automotive

RDEC

NSRDECNatick Soldier

RDEC

AMRDECAviation &

Missile RDEC

RFEC Atlantic

RFEC Pacific

RFEC Americas

ARLArmy Research Laboratory

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INTERNATIONAL ACTIVITIES

Non-Medical

NSRDEC MISSIONProviding the Army with Innovative Science & Technology Solutions to Optimize the Performance of Our Soldiers.

NSRDEC VISIONThe Soldier's RDEC. Ensuring Dominance through Superior Scientific & Engineering Expertise.

NSRDEC - The only people-centric DoD organization

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Human Systems Integration & Performance

Individual Multi-Threat Protection

Force Projection & Sustainment

Airdrop/ Aerial Delivery

Warfighter (Materials, Human Sciences, Mission Equipment, Clothing and Protective

Equipment)

Expeditionary Basing/Collective

Protection

Joint ServiceCombat Feeding

Soldier Systems Engineering Architecture (SSEA)

NSRDEC – Mission Areas

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Food, Clothing, Shelter, Supplies, Soldier Systems

Combat Feeding: What drives research?

• Processing/ packaging methods that enable production of fresh-like quality food.• Biologically tailored, performance optimizing Soldier nutrition•Targeted nutrition to extended physical & cognitive performance• Reduced Soldier load using compact, performance enhancing rations• Rapid detection and identification of food pathogens and toxins• 3-D printing of food products on or near the battlefield• Leverage biometric information to personalize nutrient needs of Soldiers

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Individual Multithreat Protection:What drives research?

• Improved hand, arm, face protection from ballistic, blast, and flame/thermal threats.

• “Smart” fibers to maintain body temperature under a wide range of climatic conditions.

• Lightweight ballistic materials for flexible and hard armor, as well as transparent armor for eye protection.

• Flame resistant fibers and textile treatments with improved performance, domestic availability, and durability.

• Protection against chembio threat agents, disease-carrying insects.

• Capabilities to conceal across the spectrum from visible through thermal.

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Expeditionary Basing and Collective Protection: What drives research?

• Multi-functional tactical habitats in diverse geographical climates and locations.

• Rapidly deployable base camp habitat and organizational equipment systems that enhance expeditionary maneuverability.

• Independence from fuel/water resupply, offering operational flexibility.

• Reduce footprint and maintenance requirements.

• Reduce resource consumption and waste generation. Reduce need for fuel resupply, water resupply, waste backhaul

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Air Drop and Aerial Delivery:What drives research?

• Reduce the signature of airdrop operations: Lower IR/RADAR signatures, dissolvable/camouflage canopies.

• New safety technologies for personnel insertion systems to include an automatic opening device for low altitude static line systems and advanced oxygen systems for military free fall systems.

• Enable on-demand tactical resupply to small unit/squads on the move. Payloads of 100-500lbs on request within 10m, with less than 10lb retrograde.

• Develop a high accuracy, low cost aerial delivery system. 1 ton system accuracy <25m, 35Kft altitude, 25+ mile offset.

• Autonomous service life monitoringUNCLASSIFIED/ Public Release

Human Performance Optimization:What drives research?

• Optimize the Soldier mind, body, and equipment

• Significantly decrease Soldier load• Integrate power, data information systems

on the Soldier to maximize situational awareness without cognitive overload.

• Novel approaches to enhance human performance (bioengineering)

• Enhanced biofidelic human modeling/encumbered anthropometry

• Sensory analysis and consumer research to optimize rations, clothing, and other areas

• Monitor and optimize cognitive performance of soldiers/squads in high-stakes environments

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Technology Focus

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• High Strength-to-Weight Fibers• Flame Resistant Fibers• Antimicrobial Fibers• Conductive Fibers• Antistatic Fibers• Photovoltaic Fibers• Smart Fibers - Sense and Respond • Biomimetic Fibers• Biodegradable Fibers• Mono/Bi/Tri Component Fibers• Dye-able High Performance Fibers• UV Stable High Performance Fibers• EMI Shielding Fibers • Super omniphobic fibers• Multifunctional Fibers

• Fibers and Fabrics• Films• Coatings• Printing on fabrics

Challenge for Soldier S&T

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Our Soldiers are more capable than in any time in history, but their capability has come at the expense of over burdening them with systems which often weigh too much, inhibit mobility and contribute to physical and cognitive stress.

Our challenge is to formulate science and technology programs that can contribute to optimizing the performance of individual Soldiers and small squads, by reducing total weight and volume, while enabling increased physical and mental agility, particularly over extended periods.

Keywords for Soldier S&T

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• Reduce weight

• Lower cost

• Rely on US materials/manufacturing

• Rapidly field

Soldier Domain Knowledge Network

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Thermal balance maintained by sweating, some change in body temperature AND actions of wearer.

Heat Balances, A Rough Guide

Solar radiation 0 to 680 wattsHeat loss to night sky

Heat loss by radiation, conduction,and natural convection

Heat loss by wind(still air adds ~1 clo)

Internal heat generation

105 watts at rest300 watts moderate work500 watts maximum sustained~1000 watts peak work rate

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Heat Balances, Rates of Change

• Change of location, hours – daysMount Washington, 6/20/04 Pinkham Notch, 65º F, 15 mph wind, Sunny Summit 23º F, 60 mph wind, Rime Ice

• Solar load – minutes (0 to 680 watts) Adds as much power as hard work Based on AM1.5 solar spectrum

• Wind - minutes (up to 1 Clo) As much as ¼ to ½ of insulation requirement Burton & Edholm “Man in a Cold

Environment”

http://www.cs.dartmouth.edu/whites/pinkham.htmlMt Washington observations: A. Jessiman

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0

1

2

3

4

5

6

7

8

9

10

-50 -40 -30 -20 -10 0 10 20

External Temperature (C)

Ther

mal

Insu

latio

n (c

lo)

1 Met (resting)2 Met (light work)3 Met (moderate work)6 Met (heavy work)

Required Insulation for Thermal Equilibrium

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Edholm & Burton“Man in a Cold Environment

Advantages of AdaptiveInsulation

• Increased temperature range Possible reduction of number of items

• Requires less user intervention Self regulating Continuously variable insulation

• Improved moisture management Reduce sweating and water requirements Reduce moisture build-up in garments

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Adaptive Insulation Concept

• Fibers act like a bi-metal spring coiling when cooled.• Coiled fibers create loft, which provides insulation.

3 components using the same polymer - No curling or change in thickness.

3 different polymers -Fibers curl, batting getsthicker.*

* In the interests of full disclosure - this initial curling probably includes some stress relaxation.

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Batting Thermal Resistance

( )

+=

−= I

xk

TTAq

Ra

oi

tot1

Thermal resistance Batting thickness Radiant heat transfer(not a function of thickness)

Thermal conductivityof air

Stuart, I.M., and Holcombe, B.V., “Heat Transfer Through Fiber Beds by Radiation with Shading and Conduction”,Textile Research Journal, Vol. 54, 1984, pp 149-157.

I and ka both decrease with temperature.

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Fiber Design

• The bending of a bi-metal strip was first calculated by Timoshenko1 in 1925.

• A combination of a crystalline and amorphous polymer will give a large difference in coefficient of thermal expansion.• Unfortunately, this combination is not efficient

at producing bending because of a large difference in stiffness between the two materials.

• By extending Timoshenko’s analysis to geometries other than flat strips, bending for fibers with very different stiffnesses can be maximized2.

1Timoshenko, S. Analysis of Bi-metal Thermostats. J. Opt. Soc. Am. 1925, 11 (3), pp.233-255

2DeCristofano et al. Proceedings MRS Fall 2010 Boston MA.

Fiber Bending Theory

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Theory – Rectangular Strip

• Assuming no slippage at the interface, the elongation in each must be equal:

1

2

a11

a22

𝛼𝛼1(𝑡𝑡 − 𝑡𝑡0) +𝑃𝑃1

𝐸𝐸1𝐴𝐴1+𝑎𝑎11

2𝜌𝜌= 𝛼𝛼2(𝑡𝑡 − 𝑡𝑡0) −

𝑃𝑃2

𝐸𝐸2𝐴𝐴2−𝑎𝑎22

2𝜌𝜌

thermal strain axial strain bending strain

b

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Timoshenko, S. “Analysis of Bi-metal Thermostats.” J. Opt. Soc. Am. 11, 233-255 (1925).

A Lot of Math Later…

“Curvature”

)())((241 012

nCBnAh

TT++

−−=

ααρ

Where:ρ Is the radius of curvature α is the coefficient of thermal expansion for material 1 or 2T is the temperatureT0 is a reference temperature where the fiber is straightn is the ratio of the Young’s moduli of the two componentsh is the height or diameter of the fiberA, B, and C are a function of the fiber geometry

Small fibershave a stronger response.

This term can be optimized for any given “n”.

Response is linear with CTE difference and temperature change.

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Fiber Cross-Section

A1

A3A2

Concept

Actual fibers

Polymer 1, amorphous(low modulus, high CTE)

Polymer 3, crystalline(high modulus, low CTE)

Compatiblizer layer(plus pigment)

Predicted curvature for bi-componentTriangular cross section fiber

Maximum curvature

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Theory – Graphical Results

• Looking more closely at the results for the triangle configuration:

0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 10

50

100

150

E1/E2 = 0.2E1/E2 = 0.1

fiber 1 is in this region

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Measured Thickness Change

2725 Oct 11 UNCLASSIFIED

0.0 0.2 0.4 0.6 0.8 1.0 1.20.0

0.2

0.4

0.6

0.8

1.0

1.2

1.4

1.6

1.8

Thic

knes

s (in

)

Load (Lbf)

Test 1 27C Test 2 27C Test 1 0C Test 2 0C Test 1 -20C Test 2 -20C

27 C (80 F)

0 C (32 F)

-20 C (-4 F)

0

2

4

6

8

00.0020.0040.0060.008

0.010.0120.0140.0160.018

0.02

0.2 0.25 0.3 0.35 0.4 0.45 0.5 0.55

Curvature per oC (1/m)Th

ickne

ss c

hang

e pe

r o C

Area Fraction C (bottom) (i-PP)

Temperature Response of Battings

Temperature Response

Calculated curvature

Measured batting thickness change

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Small changes in composition result in large changes in performance.

Estimated Performance

0.5

0.7

0.9

1.1

1.3

1.5

1.7

1.9

2.1

2.3

-35 -30 -25 -20 -15 -10 -5 0 5 10 15

Ther

mal

Res

ista

nce

(R)

Ambient Temperature (C)

Response of Clothing Insulation to Temperature

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Required thermal insulation for moderate

activity (3 Met)

Conventional insulation

Adaptive insulation

Thermal insulation that adapts to the environment extends the useful temperature range of a clothing item.

Temperature Adaptive Batting: Heat Transfer Analysis – 2

• 𝑞𝑞𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐 = ℎ 𝑇𝑇𝑠𝑠 − 𝑇𝑇∞ = 𝑇𝑇𝑠𝑠−𝑇𝑇∞𝑅𝑅𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐

and 𝑞𝑞𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐 = 𝑇𝑇0−𝑇𝑇𝑠𝑠𝑅𝑅𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐

• We can’t directly measure 𝑅𝑅𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐 when a sample is in place, but ASTM F1868 provides a method for determining it.

• The resistance used is the resistance calculated from GHP data when no sample is present on the bare plate, 𝑅𝑅𝑏𝑏𝑏𝑏.

• The resistance of the sample is the total resistance calculated from GHP with the sample in place, 𝑅𝑅𝑡𝑡𝑐𝑐𝑡𝑡 , minus the bare plate resistance.

• Then, ℎ 𝑇𝑇𝑠𝑠 − 𝑇𝑇∞ = 𝑇𝑇𝑠𝑠−𝑇𝑇∞𝑅𝑅𝑏𝑏𝑏𝑏

combined with 𝑞𝑞𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐 = 𝑇𝑇0−𝑇𝑇𝑠𝑠𝑅𝑅𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐

yields,

𝑇𝑇𝑠𝑠−𝑇𝑇∞𝑅𝑅𝑏𝑏𝑏𝑏

= 𝑇𝑇0−𝑇𝑇𝑠𝑠𝑅𝑅𝑠𝑠

(where, 𝑅𝑅𝑐𝑐𝑐𝑐𝑐𝑐𝑐𝑐 has been replaced with 𝑅𝑅𝑠𝑠 , the sample resistance.)

Ts, Fabric Surface Temperature

T0, Hot Plate Temperature (35 oC)

hot plate

sample condqconvqT∞, Ambient Temperature

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Temperature Adaptive Batting: Heat Transfer Analysis – 4

• From the GHP data,

(temperatures units are oC and resistance units are clo)

• For a change in sample temperature of 10.3 oC, an increase in clo of 0.211 was measured (over a 25 oC ambient temperature range).

1.56 % / oC

𝑇𝑇∞ 𝑇𝑇0 𝑅𝑅𝑡𝑡𝑐𝑐𝑡𝑡 𝑅𝑅𝑏𝑏𝑏𝑏 𝑅𝑅𝑠𝑠 𝑇𝑇𝑠𝑠 𝑇𝑇𝑠𝑠𝑠𝑠𝑠𝑠𝑏𝑏𝑠𝑠𝑠𝑠

20 35 1.666 0.355 1.311 23.2 29.12 35 1.702 0.355 1.347 8.9 21.9-5 35 1.877 0.355 1.522 2.6 18.8

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Thermal Insulation as a Function of Air Temperature in Guarded Hot Plate Test

Notes: Specific insulation [Intrinsic Clo/(oz/yd2)] at various air temperatures with plate at 35 C.“Bare plate clo” = 0.355The thermal conductivity of air is a function of temperature and the net radiant heat transfer through the batting varies approximately as the cube of the mean temperature (absolute) which leads to a slight increase in clo with decreasing temperature for the control.

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0.000

0.100

0.200

0.300

0.400

0.500

0.600

0.700

-10 -5 0 5 10 15 20 25

Insu

latio

n [in

trins

ic C

lo/(o

z/yd

2 )]

Air Temperature (C)

Climashield TemperatureResponsive Batting

Control - Climashield Apex(laundered 3x)

Thermal Insulation as a Function of Air Temperature in Guarded Hot Plate Test

0.800

1.000

1.200

1.400

1.600

1.800

2.000

Temp @ 20oC Temp @ 2oC Temp @ -5oC

Clo

Air Temperature (oC)

Climashield

Control Climashield Apex Laundered 3times

Total Clo at various air temperatures with plate at 35 CNote: The thermal conductivity of air is a function of temperature and the net radiant heat transfer through the batting varies approximately as the cube of the mean temperature (absolute) which leads to a slight increase in clo with decreasing temperature for the control.

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Thermal Insulation as a Function of Air Temperature in Guarded Hot Plate Test

Total Clo/(oz/yd2) at various air temperatures with plate at 35 CNote: The thermal conductivity of air is a function of temperature and the net radiant heat transfer through the batting varies approximately as the cube of the mean temperature (absolute) which leads to a slight increase in clo with decreasing temperature for the control.

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0.000

0.100

0.200

0.300

0.400

0.500

0.600

0.700

0.800

0.900

Temp @ 20oC Temp @ 2oC Temp @ -5oC

Spec

ific

Insu

latio

n cl

o/(o

z/yd

2 )Specific Insulation as a Function of Air Temperature

Climashield Control Climashield Apex Laundered 3 times

• “AFFOA is an advanced manufacturing institute created to bring demonstrated technologies to pilot scale production. Technologies in the DELTA program fit also into AFFOA's mission. I would be delighted to attend this event to define synergies between the outcome of this program and AFFOA's mission to scale and commercialize.”

• Aimee Rose - Chief Technology Officer for Advanced Functional Fabrics of America (AFFOA)

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AFFOA

• Partnering with NSRDEC– http://nsrdec.natick.army.mil/business/partneri

ng.htm• Manufacturing USA & AFFOA

– https://www.manufacturingusa.com/institutes– http://join.affoa.org/membership/

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Links

The Science Behind

the SoldierYesterday, Today and Tomorrow

US Army Natick Soldier Research, Development &

Engineering Center

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