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The University of Kansas

The University of Minnesota
College of Biological Sciences

Revolutionary New Adaptive Material
“SolutionCell © ”
SolutionCell© is a Pressure Adaptive Honeycomb (PAH)
www.SolutionCell.com & www.SolutionCell.net

unclassified

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Adaptive Aerostructures Laboratory

Brought to you by:

Shawn Paul Boike

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

Solution Vehicles Co &
American Industrial Consultants
From: BOEING, Northrop, Lockheed, FORD, GM & NASA
Long Beach, CA. 90803
562.343.5660 / 562.338.9911 (m)
https://www.facebook.com/AmericanIndustrialConsultantsGroup

by

Ron Barrett
The University of Kansas, Lawrence
Aerospace Engineering Department
and

Cassandra Barrett
The University of Minnesota
College of Biological Sciences

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rev. 28 February 2010

1
The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

College of Biological Sciences

Presentation Dates

• So. California (Feb 24-28 2014):
Thu

Fri

2/27

2/28

Northrop
UAV *San
Diego

Boeing Seal
Bch

Boeing LB

Aero/Def

San Diego
Gen
Atomics??

Boeing HB

???

distribution unlimited

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Mon
2/24

Tue
2/25

Wed
2/26

Zodiac Aero

Aero/Def

Eaton/Parker

Unclassified

rev. 28 February 2010

2
The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

College of Biological Sciences

Revolutionary Adaptive Aerostructures, Changing
Flight via Nature's Analogs for Dramatic Fuel Savings
by

Ron Barrett
The University of Kansas, Lawrence
Aerospace Engineering Department
and

Cassandra Barrett
The University of Minnesota
College of Biological Sciences

1st international Conference and Exhibition on Mechanical and
Aerospace Engineering, San Antonio, Texas
30 September – 2 October 2013
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The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

College of Biological Sciences

Outline
1. Introduction & Motivation
2. Fast-Response Actuators in Eukaryotes
3. Biomimetic FAA-Certifiable Artificial Muscles
4. Selected Aerospace Applications
5. Summary

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College of Biological Sciences

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Adaptive Aerostructures Laboratory

The University of Minnesota

Motivation: The same as nature
T/O & Landing: Maximize CLmax, Reject Gust Loading
Cruise: Maximize L/D

Minimize Airframe Weight
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The University of Kansas

College of Biological Sciences

Successful Applications of Biomimicking
Adaptive Materials In the Aerospace Industry:
Weapon Systems

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The University of Minnesota

Piezoelectric, Shape-Memory-Alloys, Electroluminiscent Materials...

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The University of Minnesota

Adaptive Aerostructures Laboratory
College of Biological Sciences
Successful Applications of Biomimicking
Adaptive Materials In the Aerospace Industry:

Disappearing UAVs

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The University of Kansas

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The University of Kansas

The University of Minnesota
College of Biological Sciences

Selected Aerospace Morphing Concepts
Section Morphing

www.nextgenaeronautics.com 2008

Planform Morphing

Gould et al. 1981

MissionAdaptiveWing

Pendelton et al. 1981

1980’s: Mission Adaptive Wing

www.geocities.com 2008

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

University of Florida

1990’s: NASA’s AAW
Lockheed Martin

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The University of Kansas

The University of Minnesota
College of Biological Sciences

Adaptive Materials & Structures
Piezoelectric Materials

Shape Memory Alloys

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

Air Muscles

McMurtry 2004

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9
The University of Kansas

College of Biological Sciences

Conventional Adaptive Materials
Current range of actuator materials available
Can they be used in commercial aircraft as a class?
...or in primary structure?

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Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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College of Biological Sciences

What Would an Aircraft Designer want if s/he could
design an adaptive material???
An "Ideal" Adaptive Aeromaterial/Aerostructure:

•Material capable of "huge" (>50+%?) strains

•Fully proportional, easily controlled
•Stiff & strong enough to handle "real" loads
•Lighter & faster than conventional aircraft actuation systems

•Less costly & lower drag than conventional aircraft actuation systems
•Certifiable under FAR 23/25, 27/29

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The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota
College of Biological Sciences

Solution? ...Biomimetics

"You should pay attention to what
Mother Nature has done because
she's got a 4.2 billion year lead in
research and development.
-Prof. H.W. Smith, PE, Ph.D.

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The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota
College of Biological Sciences

Fast-Response Actuators
in Eukaryotes
•Animal Muscle Cells and Tissues

• Fast-Acting Plant
Cells and Tissues

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The University of Kansas

College of Biological Sciences

Fast-Response Actuators
in Eukaryotes
Animal Muscle Cell & Tissues

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

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The University of Minnesota

Solution:
Adaptive Aerostructures Laboratory
College of Biological Sciences
Actuators Made from 100% FAA-Certifiable
materials, but arranged like fast-acting plant cells

15

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The University of Kansas

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Video Credit: & © C.M. Barrett
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The University of Kansas

College of Biological Sciences

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

16

Solution:
FAA-Certifiable Actuators based on Plant Cell Structures

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Adaptive Aerostructures Laboratory

The University of Minnesota

Albizia julibrissin

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The University of Kansas

The University of Minnesota
College of Biological Sciences

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

17

Solution:
FAA-Certifiable Actuators based on Plant Cell Structures

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Adaptive Aerostructures Laboratory

Pulvinus

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College of Biological Sciences

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18

Solution:
FAA-Certifiable Actuators based on Plant Cell Structures

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Adaptive Aerostructures Laboratory

The University of Minnesota

Ground Cells

Phloem
Xylem

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The University of Minnesota

Solution:
Adaptive Aerostructures Laboratory
College of Biological Sciences
Actuators Made from 100% FAA-Certifiable
Materials, but arranged like fast-acting plant cells

19

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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The University of Kansas

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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The University of Kansas

College of Biological Sciences

Solution:
FAA-Certifiable Actuators based on Plant Cell Structures
Fundamental Structural Arrangement:

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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The University of Minnesota

Biomimetic Honeycomb
Based on Plant Actuator Cells

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

College of Biological Sciences

• Easily modeled, light, strong

• Made of conventional materials
(aluminum, steel, aramids)
• Already known and accepted by certifying
agencies like the FAA
Unclassified

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21
The University of Kansas

College of Biological Sciences

PAH Theory, Experiment & Correlation

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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The University of Kansas

College of Biological Sciences

PAH Single-Cell Tension-Compression Test

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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The University of Minnesota

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College of Biological Sciences

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Multi-Cell Compression Test

180mm

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The University of Kansas

College of Biological Sciences

PAH Single-Cell Tension-Compression Test

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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The University of Kansas

College of Biological Sciences

Comparison to Other
Adaptive Materials and Actuators
Conventional Hydraulic Actuators

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

High Pressure
Adaptive Honeycomb

Atmospherically Triggered
Adaptive Honeycombs

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The University of Minnesota
A New Approach to Flight Biological Sciences
Adaptive Aerostructures Laboratory
College of Control...
Based on Nature:

27

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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The University of Kansas

PAH employs distributed, rather than concentrated actuation...

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All 4.Aerospace 28 February 2010
rev. 5.Automotive
The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota
College of Biological Sciences

Current Aircraft Actuator Design
Philosophy

Distributed airloads

Control surface loads
concentrated at
finite hard points
Loads transferred
through actuators
& tracks

Loads redistributed
into primary
structure

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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28
The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota
College of Biological Sciences

PAH Actuator Design Philosophy

Control surface loads
stayed distributed
Distributed control
surface loads passed
thru distributed
actuators
Distributed loads
transferred to primary
strucure

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The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota
College of Biological Sciences

Comparison of PAH to Adaptive Materials
and FAA Certified Actuators
High Pressure Adaptive Honeycomb

Conventional
Hydraulics
& Pneumatics

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The University of Minnesota

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Adaptive Aerostructures Laboratory

College of Biological Sciences

and C.M. al. 2007
Copyright © R.M. Murray et Barrett 2013 all rights reserved

unclassified

Pressure Adaptive Wing Section

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The University of Kansas

The University of Minnesota
College of Biological Sciences

Pressure-Adaptive Flap in Wind Tunnel (cont.)

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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0kPa CDP

40kPa CDP

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The University of Kansas

The University of Minnesota

Base Stiffness Cell Differential Pressure Behavior
1.6
NCCDP
(kPa)
40
20

Net Camber CDP = 40kpa

1.4
Lift Coefficient, Cl (~)

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

33

College of Biological Sciences

PAH Wing Section: Controllable Aerocompliance

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1.3
0

1.0

-20

0.8

-40

0.6
0.4
0.2
0
-5

0

5
10
Angle of Attack, a (deg)

15

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The University of Kansas

College of Biological Sciences

Current Aircraft Technology in Gust Fields

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

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The University of Kansas

College of Biological Sciences

PAH Wings: Enhancing Ride Quality, Fatigue
Properties & Flight Safety via Active Aerocompliance

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

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The University of Kansas

The University of Minnesota

Structure of a typical FAR-25 V-n Diagram

Commercial Aircraft
Structural Weights are
set by these points

Gust Limits
Maneuver Limits

Load Factor, n (g's)

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

36

College of Biological Sciences

The Real Savings... from Class I Design Forward

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+1
0

-1

VS1

VA

Flight Speed, Vflt (kts)

VC

VD

Gust Limits

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The University of Minnesota

37

College of Biological Sciences

Weight Saving Paradigm Shift:
Compression of Gust Lines to within Maneuver
...just like birds do, via dynamic aerocompliance

Load Factor, n (g's)

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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+1
0

-1

VS1

VA

Flight Speed, Vflt (kts)

VC

VD

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The University of Kansas

The University of Minnesota

38

College of Biological Sciences

Weight Saving Paradigm Shift:
Compression of Gust Lines to within Maneuver
...just like birds do, via dynamic aerocompliance

saving... 7 – 23% total aircraft structural weight!

Load Factor, n (g's)

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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+1
0

-1

VS1

VA

Flight Speed, Vflt (kts)

VC

VD

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The University of Kansas

College of Biological Sciences

Reference: Boeing 787
$32B investment in new product RDT&E:
• Just over half of the RDT&E was devoted to new materials & manufacturing
to achieve a ~20% weight reduction WRT conventional materials

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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The University of Minnesota

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The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

College of Biological Sciences

PAH Implications for Commercial Aircraft
Implications for commercial jets:
• Reduction in Structural Weight
• Increase in mission integrated L/Dmax
• Reduction in DOC at constant range
• Increase in range at constant TOW
• Airfoil section gust load rejection:
• Net airframe gust load rejection
• Safe Airframe Life Extension

9 - 22%
6 - 9%
7 - 11%
12 - 18%
up to 380%
up to 87%
11 - 14%

US Pat. 8,366,057 Issued 13 February 2013

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Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Acknowledgements

Prof. Roelof Vos

NASA Ames Research Center

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41
The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

College of Biological Sciences

PAH Flap and Winglet System Implications
Implications for commercial jet fleets:

Korean Air:

KRW11.807 trillion 2011 in operating expenses
Retrofit Impacts: ~ +KRW200B
(Net loss in 2011: KRW98B)

New Equipment Impacts:
+KRW850B DOC savings +
+KRW220B Airframe Life Extension +
+KRW660B increased cargo carriage revenue ~ KRW1.7 trillion

European Patent EP 2459442 A2
US Patent 8,366,057 B2 February 2013
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The University of Minnesota

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College of Biological Sciences

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Questions?

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43
The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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44

What if...

Something about the flight environment itself
could deploy the surfaces...

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45

Pressure Adaptive Honeycomb (PAH)
Flap Systems
Example for LSA wing

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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Adaptive Aerostructures Laboratory

The University of Minnesota

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All 4.Aerospace 28 February 2010
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The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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The University of Minnesota
College of Biological Sciences

46

Potential Application: Pressure Adaptive
Honeycomb (PAH) Flap
Implications for LSA* based on a 20% increase of clean CLmax:**
• 17% reduction in wing wetted area
• 20% increase in aspect ratio
• 10% increase in L/D
• 8% reduction fuel burn and DOC at constant range
• 1.5% decrement in TOW and purchase price at constant range
• 37% gust rejection loads

*45kts flaps-up stall requirement
**Based on: Roskam “Airplane Design,” part I, II, V, and VIII, and Cessna 162 Skykatcher Data

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Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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The University of Minnesota
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47

PAH Gurney Flap (cont.)
Implications for jets based on a 6% increase of CLmax:
5.8% decrease in wetted area
6% increase in aspect ratio
3% increase in L/Dmax
3.2% reduction in DOC at constant range
3% increase in range at constant TOW
380% section gust load rejection
87% net airframe gust load rejection

*Based on: Roskam “Airplane Design,” part I, II, and V,

and Cessna Citation Sovereign

Data
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The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

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The University of Minnesota

48

College of Biological Sciences

PAH Implications for Commercial Aircraft
Implications for commercial jets:

• Increase in CLmaxL/TO
• Reduction in Structural Weight
• Increase in mission integrated L/Dmax:
• Reduction in DOC at constant range
• Increase in range at constant TOW
• Section gust load rejection:
• Net airframe gust load rejection

Retrofit
STC
3%
0%
2.4%
2.5%
2.2%
43%
21%

Class I
Design
6%
9 - 22%
6 - 9%
7 - 11%
12 - 18%
380%
87%

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College of Biological Sciences

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PAH Cell Modeling

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49
The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

College of Biological Sciences

PAH Linear-Elastic Modeling Background
Cellular Material Theory (CMT) after Gibson et al. 1988
Considerations:
l
• Only valid for small thickness-to-length ratio
t
qi
• Only valid for +/- 20% of strain
• Linear stress-strain relationship

Unclassified

distribution unlimited

© R. Barrett

All Rights Reserved

rev. 28 February 2010

50
The University of Kansas

The University of Minnesota
College of Biological Sciences

PAH Linear-Elastic Modeling Background

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

Unclassified

distribution unlimited

© R. Barrett

All Rights Reserved

rev. 28 February 2010

51
The University of Kansas

The University of Minnesota

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

College of Biological Sciences

PAH Theoretical Characterization
Global stress-strain relations:
@ constant pressure:

@ constant mass:

with

Unclassified

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All Rights Reserved

rev. 28 February 2010

52
The University of Kansas

College of Biological Sciences

53

PAH Geo-Kinematic Properties

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

The University of Minnesota

CDP = Cell Differential Pressure

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
© R. Barrett
All 4.Aerospace 28 February 2010
rev. 5.Automotive
The University of Kansas

The University of Minnesota
College of Biological Sciences

Non-linear Mechanics of PAH Structures

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

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Adaptive Aerostructures Laboratory

Unclassified

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rev. 28 February 2010

54
The University of Kansas

The University of Minnesota
College of Biological Sciences

Effects of Different PAH Boundary Conditions

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

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Adaptive Aerostructures Laboratory

Unclassified

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© R. Barrett

All Rights Reserved

rev. 28 February 2010

55
The University of Kansas

The University of Minnesota
College of Biological Sciences

PAH Longitudinal Stress-Strain Correlation

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

p = 55kPa
Unclassified

distribution unlimited

p = 60kPa
© R. Barrett

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rev. 28 February 2010

56
The University of Kansas

The University of Minnesota
College of Biological Sciences

Experimental PAH Stress-Strain Relations

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

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Adaptive Aerostructures Laboratory

Unclassified

distribution unlimited

© R. Barrett

All Rights Reserved

rev. 28 February 2010

57
The University of Kansas

The University of Minnesota
College of Biological Sciences

PAH Four-Cell Tensile Test of Steel PAH

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

Unclassified

distribution unlimited

© R. Barrett

All Rights Reserved

rev. 28 February 2010

58
The University of Kansas

College of Biological Sciences

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

59

PAH Bender Experimental Characterization
Validation
Experiment:
Three-point
bend test

unclassified

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Adaptive Aerostructures Laboratory

The University of Minnesota

FEM Modeling:

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
© R. Barrett
All 4.Aerospace 28 February 2010
rev. 5.Automotive
The University of Kansas

The University of Minnesota

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

College of Biological Sciences

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

PAH Cell Modeling

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rev. 28 February 2010

60
The University of Kansas

College of Biological Sciences

PAH Multi-Cell Compression Test

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

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Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
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All 4.Aerospace 28 February 2010
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61
The University of Kansas

College of Biological Sciences

62

PAH Gurney Flaps & Winglets

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

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Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
© R. Barrett
All 4.Aerospace 28 February 2010
rev. 5.Automotive
The University of Kansas

College of Biological Sciences

Fast-Response Actuators in Eukaryotes
Molecuar Mechanism of Muscle Contraction
Stimulus

Myosin head binds to actin

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

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Adaptive Aerostructures Laboratory

The University of Minnesota

6.7nm
contraction

Myosin head turns as P1 is released

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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All 4.Aerospace 28 February 2010
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63
The University of Kansas

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

The University of Minnesota
College of Biological Sciences

Fast-Response Actuators
in Eukaryotes
Mechanical Analogs of Animal Muscle Tissues:
-Shape-Memory-Alloys
-Pneumatic Tubes
-Piezoelectric Polymers
-Adaptive Gels
-Electrostatic Actuators

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
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64
The University of Minnesota

Adaptive Aerostructures Laboratory
College of Biological Sciences
Successful Applications of Biomimicking
Adaptive Materials In the Aerospace Industry:

UAVs & Hovering Missiles

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

The University of Kansas

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
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All 4.Aerospace 5. Summary
rev. 28 February 2010

65
The University of Kansas

The University of Minnesota
College of Biological Sciences

Biomimetic Plant-Cell Based
Honeycomb Actuator

After: Olympio et al. 2007

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

Standard

Auxetic

Hybrid

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
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All 4.Aerospace 28 February 2010
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66
The University of Kansas

College of Biological Sciences

67

Aerocompliance: Key to Birds Wings and PAH

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

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Adaptive Aerostructures Laboratory

The University of Minnesota

Gust load relieving smoothes flight

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
© R. Barrett
All 4.Aerospace 28 February 2010
rev. 5.Automotive
The University of Kansas

College of Biological Sciences

PAH Four-Cell Tensile Test of Steel
Honeycombs

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
© R. Barrett
All 4.Aerospace 28 February 2010
rev. 5.Summary

68
The University of Minnesota

69

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

The University of Kansas

Solution:
Adaptive Aerostructures Laboratory
College of Biological Sciences
FAA-Certifiable Actuators based on Plant Cell Structures

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
© R. Barrett
All 4.Aerospace 28 February 2010
rev. 5.Automotive
The University of Kansas

College of Biological Sciences

Pressure Adaptive Honeycomb (PAH)
Breakdown for Modeling

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
Unclassified
distribution unlimited
© R. Barrett
All 4.Aerospace 28 February 2010
rev. 5.Summary

70
The University of Kansas

College of Biological Sciences

PAH Nonlinear Mechanics

Copyright © R.M. and C.M. Barrett 2013 all rights reserved

unclassified

ITAR /EAR unrestricted

Adaptive Aerostructures Laboratory

The University of Minnesota

1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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All 4.Aerospace 28 February 2010
rev. 5.Summary

71

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Solution wings for Aerospace Applications.

  • 1. The University of Kansas The University of Minnesota College of Biological Sciences Revolutionary New Adaptive Material “SolutionCell © ” SolutionCell© is a Pressure Adaptive Honeycomb (PAH) www.SolutionCell.com & www.SolutionCell.net unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Brought to you by: Shawn Paul Boike Copyright © R.M. and C.M. Barrett 2013 all rights reserved Solution Vehicles Co & American Industrial Consultants From: BOEING, Northrop, Lockheed, FORD, GM & NASA Long Beach, CA. 90803 562.343.5660 / 562.338.9911 (m) https://www.facebook.com/AmericanIndustrialConsultantsGroup by Ron Barrett The University of Kansas, Lawrence Aerospace Engineering Department and Cassandra Barrett The University of Minnesota College of Biological Sciences Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 1
  • 2. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Presentation Dates • So. California (Feb 24-28 2014): Thu Fri 2/27 2/28 Northrop UAV *San Diego Boeing Seal Bch Boeing LB Aero/Def San Diego Gen Atomics?? Boeing HB ??? distribution unlimited © R. Barrett All Rights Reserved Mon 2/24 Tue 2/25 Wed 2/26 Zodiac Aero Aero/Def Eaton/Parker Unclassified rev. 28 February 2010 2
  • 3. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Revolutionary Adaptive Aerostructures, Changing Flight via Nature's Analogs for Dramatic Fuel Savings by Ron Barrett The University of Kansas, Lawrence Aerospace Engineering Department and Cassandra Barrett The University of Minnesota College of Biological Sciences 1st international Conference and Exhibition on Mechanical and Aerospace Engineering, San Antonio, Texas 30 September – 2 October 2013 Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 3
  • 4. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Outline 1. Introduction & Motivation 2. Fast-Response Actuators in Eukaryotes 3. Biomimetic FAA-Certifiable Artificial Muscles 4. Selected Aerospace Applications 5. Summary 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5. Summary 4
  • 5. The University of Kansas College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota Motivation: The same as nature T/O & Landing: Maximize CLmax, Reject Gust Loading Cruise: Maximize L/D Minimize Airframe Weight 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive 5
  • 6. The University of Kansas College of Biological Sciences Successful Applications of Biomimicking Adaptive Materials In the Aerospace Industry: Weapon Systems Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota Piezoelectric, Shape-Memory-Alloys, Electroluminiscent Materials... 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5. Summary 6
  • 7. The University of Minnesota Adaptive Aerostructures Laboratory College of Biological Sciences Successful Applications of Biomimicking Adaptive Materials In the Aerospace Industry: Disappearing UAVs Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted The University of Kansas 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5. Summary 7
  • 8. The University of Kansas The University of Minnesota College of Biological Sciences Selected Aerospace Morphing Concepts Section Morphing www.nextgenaeronautics.com 2008 Planform Morphing Gould et al. 1981 MissionAdaptiveWing Pendelton et al. 1981 1980’s: Mission Adaptive Wing www.geocities.com 2008 Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory University of Florida 1990’s: NASA’s AAW Lockheed Martin 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5. Summary 8
  • 9. The University of Kansas The University of Minnesota College of Biological Sciences Adaptive Materials & Structures Piezoelectric Materials Shape Memory Alloys Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Air Muscles McMurtry 2004 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 285. Summary rev. February 2010 9
  • 10. The University of Kansas College of Biological Sciences Conventional Adaptive Materials Current range of actuator materials available Can they be used in commercial aircraft as a class? ...or in primary structure? Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5. Summary 10
  • 11. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences What Would an Aircraft Designer want if s/he could design an adaptive material??? An "Ideal" Adaptive Aeromaterial/Aerostructure: •Material capable of "huge" (>50+%?) strains •Fully proportional, easily controlled •Stiff & strong enough to handle "real" loads •Lighter & faster than conventional aircraft actuation systems •Less costly & lower drag than conventional aircraft actuation systems •Certifiable under FAR 23/25, 27/29 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 5. Summary rev. 28 February 2010 11
  • 12. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences Solution? ...Biomimetics "You should pay attention to what Mother Nature has done because she's got a 4.2 billion year lead in research and development. -Prof. H.W. Smith, PE, Ph.D. 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 12
  • 13. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences Fast-Response Actuators in Eukaryotes •Animal Muscle Cells and Tissues • Fast-Acting Plant Cells and Tissues 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 13
  • 14. The University of Kansas College of Biological Sciences Fast-Response Actuators in Eukaryotes Animal Muscle Cell & Tissues Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 14
  • 15. The University of Minnesota Solution: Adaptive Aerostructures Laboratory College of Biological Sciences Actuators Made from 100% FAA-Certifiable materials, but arranged like fast-acting plant cells 15 Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted The University of Kansas 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Video Credit: & © C.M. Barrett Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 16. The University of Kansas College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved 16 Solution: FAA-Certifiable Actuators based on Plant Cell Structures unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota Albizia julibrissin 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary
  • 17. The University of Kansas The University of Minnesota College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved 17 Solution: FAA-Certifiable Actuators based on Plant Cell Structures unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Pulvinus 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary
  • 18. The University of Kansas College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved 18 Solution: FAA-Certifiable Actuators based on Plant Cell Structures unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota Ground Cells Phloem Xylem 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary
  • 19. The University of Minnesota Solution: Adaptive Aerostructures Laboratory College of Biological Sciences Actuators Made from 100% FAA-Certifiable Materials, but arranged like fast-acting plant cells 19 Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted The University of Kansas 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Video Credit: & © C.M. Barrett Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 20. The University of Kansas College of Biological Sciences Solution: FAA-Certifiable Actuators based on Plant Cell Structures Fundamental Structural Arrangement: Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 20
  • 21. The University of Kansas The University of Minnesota Biomimetic Honeycomb Based on Plant Actuator Cells Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences • Easily modeled, light, strong • Made of conventional materials (aluminum, steel, aramids) • Already known and accepted by certifying agencies like the FAA Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 21
  • 22. The University of Kansas College of Biological Sciences PAH Theory, Experiment & Correlation Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 22
  • 23. The University of Kansas College of Biological Sciences PAH Single-Cell Tension-Compression Test Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 23
  • 24. The University of Kansas The University of Minnesota ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified Multi-Cell Compression Test 180mm Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 24
  • 25. The University of Kansas College of Biological Sciences PAH Single-Cell Tension-Compression Test Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 25
  • 26. The University of Kansas College of Biological Sciences Comparison to Other Adaptive Materials and Actuators Conventional Hydraulic Actuators Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota High Pressure Adaptive Honeycomb Atmospherically Triggered Adaptive Honeycombs 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 26
  • 27. The University of Minnesota A New Approach to Flight Biological Sciences Adaptive Aerostructures Laboratory College of Control... Based on Nature: 27 Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted The University of Kansas PAH employs distributed, rather than concentrated actuation... 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 28. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences Current Aircraft Actuator Design Philosophy Distributed airloads Control surface loads concentrated at finite hard points Loads transferred through actuators & tracks Loads redistributed into primary structure 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 28
  • 29. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences PAH Actuator Design Philosophy Control surface loads stayed distributed Distributed control surface loads passed thru distributed actuators Distributed loads transferred to primary strucure 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 29
  • 30. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences Comparison of PAH to Adaptive Materials and FAA Certified Actuators High Pressure Adaptive Honeycomb Conventional Hydraulics & Pneumatics 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 30
  • 31. The University of Kansas The University of Minnesota ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences and C.M. al. 2007 Copyright © R.M. Murray et Barrett 2013 all rights reserved unclassified Pressure Adaptive Wing Section Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 31
  • 32. The University of Kansas The University of Minnesota College of Biological Sciences Pressure-Adaptive Flap in Wind Tunnel (cont.) Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory 0kPa CDP 40kPa CDP Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 32
  • 33. The University of Kansas The University of Minnesota Base Stiffness Cell Differential Pressure Behavior 1.6 NCCDP (kPa) 40 20 Net Camber CDP = 40kpa 1.4 Lift Coefficient, Cl (~) Copyright © R.M. and C.M. Barrett 2013 all rights reserved 33 College of Biological Sciences PAH Wing Section: Controllable Aerocompliance unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory 1.3 0 1.0 -20 0.8 -40 0.6 0.4 0.2 0 -5 0 5 10 Angle of Attack, a (deg) 15 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary
  • 34. The University of Kansas College of Biological Sciences Current Aircraft Technology in Gust Fields Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 34
  • 35. The University of Kansas College of Biological Sciences PAH Wings: Enhancing Ride Quality, Fatigue Properties & Flight Safety via Active Aerocompliance Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 35
  • 36. The University of Kansas The University of Minnesota Structure of a typical FAR-25 V-n Diagram Commercial Aircraft Structural Weights are set by these points Gust Limits Maneuver Limits Load Factor, n (g's) Copyright © R.M. and C.M. Barrett 2013 all rights reserved 36 College of Biological Sciences The Real Savings... from Class I Design Forward unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory +1 0 -1 VS1 VA Flight Speed, Vflt (kts) VC VD Gust Limits 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary
  • 37. The University of Kansas The University of Minnesota 37 College of Biological Sciences Weight Saving Paradigm Shift: Compression of Gust Lines to within Maneuver ...just like birds do, via dynamic aerocompliance Load Factor, n (g's) Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory +1 0 -1 VS1 VA Flight Speed, Vflt (kts) VC VD 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary
  • 38. The University of Kansas The University of Minnesota 38 College of Biological Sciences Weight Saving Paradigm Shift: Compression of Gust Lines to within Maneuver ...just like birds do, via dynamic aerocompliance saving... 7 – 23% total aircraft structural weight! Load Factor, n (g's) Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory +1 0 -1 VS1 VA Flight Speed, Vflt (kts) VC VD 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary
  • 39. The University of Kansas College of Biological Sciences Reference: Boeing 787 $32B investment in new product RDT&E: • Just over half of the RDT&E was devoted to new materials & manufacturing to achieve a ~20% weight reduction WRT conventional materials Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 39
  • 40. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences PAH Implications for Commercial Aircraft Implications for commercial jets: • Reduction in Structural Weight • Increase in mission integrated L/Dmax • Reduction in DOC at constant range • Increase in range at constant TOW • Airfoil section gust load rejection: • Net airframe gust load rejection • Safe Airframe Life Extension 9 - 22% 6 - 9% 7 - 11% 12 - 18% up to 380% up to 87% 11 - 14% US Pat. 8,366,057 Issued 13 February 2013 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 40
  • 41. The University of Kansas The University of Minnesota ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified Acknowledgements Prof. Roelof Vos NASA Ames Research Center Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 41
  • 42. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences PAH Flap and Winglet System Implications Implications for commercial jet fleets: Korean Air: KRW11.807 trillion 2011 in operating expenses Retrofit Impacts: ~ +KRW200B (Net loss in 2011: KRW98B) New Equipment Impacts: +KRW850B DOC savings + +KRW220B Airframe Life Extension + +KRW660B increased cargo carriage revenue ~ KRW1.7 trillion European Patent EP 2459442 A2 US Patent 8,366,057 B2 February 2013 Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 42
  • 43. The University of Kansas The University of Minnesota ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified Questions? Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 43
  • 44. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences 44 What if... Something about the flight environment itself could deploy the surfaces... 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 45. The University of Kansas College of Biological Sciences 45 Pressure Adaptive Honeycomb (PAH) Flap Systems Example for LSA wing Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 46. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences 46 Potential Application: Pressure Adaptive Honeycomb (PAH) Flap Implications for LSA* based on a 20% increase of clean CLmax:** • 17% reduction in wing wetted area • 20% increase in aspect ratio • 10% increase in L/D • 8% reduction fuel burn and DOC at constant range • 1.5% decrement in TOW and purchase price at constant range • 37% gust rejection loads *45kts flaps-up stall requirement **Based on: Roskam “Airplane Design,” part I, II, V, and VIII, and Cessna 162 Skykatcher Data 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 47. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences 47 PAH Gurney Flap (cont.) Implications for jets based on a 6% increase of CLmax: 5.8% decrease in wetted area 6% increase in aspect ratio 3% increase in L/Dmax 3.2% reduction in DOC at constant range 3% increase in range at constant TOW 380% section gust load rejection 87% net airframe gust load rejection *Based on: Roskam “Airplane Design,” part I, II, and V, and Cessna Citation Sovereign Data 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 48. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 48 College of Biological Sciences PAH Implications for Commercial Aircraft Implications for commercial jets: • Increase in CLmaxL/TO • Reduction in Structural Weight • Increase in mission integrated L/Dmax: • Reduction in DOC at constant range • Increase in range at constant TOW • Section gust load rejection: • Net airframe gust load rejection Retrofit STC 3% 0% 2.4% 2.5% 2.2% 43% 21% Class I Design 6% 9 - 22% 6 - 9% 7 - 11% 12 - 18% 380% 87% 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 49. The University of Kansas The University of Minnesota ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified PAH Cell Modeling Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 49
  • 50. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences PAH Linear-Elastic Modeling Background Cellular Material Theory (CMT) after Gibson et al. 1988 Considerations: l • Only valid for small thickness-to-length ratio t qi • Only valid for +/- 20% of strain • Linear stress-strain relationship Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 50
  • 51. The University of Kansas The University of Minnesota College of Biological Sciences PAH Linear-Elastic Modeling Background Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 51
  • 52. The University of Kansas The University of Minnesota Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences PAH Theoretical Characterization Global stress-strain relations: @ constant pressure: @ constant mass: with Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 52
  • 53. The University of Kansas College of Biological Sciences 53 PAH Geo-Kinematic Properties Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota CDP = Cell Differential Pressure 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 54. The University of Kansas The University of Minnesota College of Biological Sciences Non-linear Mechanics of PAH Structures Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 54
  • 55. The University of Kansas The University of Minnesota College of Biological Sciences Effects of Different PAH Boundary Conditions Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 55
  • 56. The University of Kansas The University of Minnesota College of Biological Sciences PAH Longitudinal Stress-Strain Correlation Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory p = 55kPa Unclassified distribution unlimited p = 60kPa © R. Barrett All Rights Reserved rev. 28 February 2010 56
  • 57. The University of Kansas The University of Minnesota College of Biological Sciences Experimental PAH Stress-Strain Relations Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 57
  • 58. The University of Kansas The University of Minnesota College of Biological Sciences PAH Four-Cell Tensile Test of Steel PAH Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 58
  • 59. The University of Kansas College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved 59 PAH Bender Experimental Characterization Validation Experiment: Three-point bend test unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota FEM Modeling: 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 60. The University of Kansas The University of Minnesota ITAR /EAR unrestricted Adaptive Aerostructures Laboratory College of Biological Sciences Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified PAH Cell Modeling Unclassified distribution unlimited © R. Barrett All Rights Reserved rev. 28 February 2010 60
  • 61. The University of Kansas College of Biological Sciences PAH Multi-Cell Compression Test Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 61
  • 62. The University of Kansas College of Biological Sciences 62 PAH Gurney Flaps & Winglets Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 63. The University of Kansas College of Biological Sciences Fast-Response Actuators in Eukaryotes Molecuar Mechanism of Muscle Contraction Stimulus Myosin head binds to actin Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 6.7nm contraction Myosin head turns as P1 is released 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 63
  • 64. The University of Kansas Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota College of Biological Sciences Fast-Response Actuators in Eukaryotes Mechanical Analogs of Animal Muscle Tissues: -Shape-Memory-Alloys -Pneumatic Tubes -Piezoelectric Polymers -Adaptive Gels -Electrostatic Actuators 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 64
  • 65. The University of Minnesota Adaptive Aerostructures Laboratory College of Biological Sciences Successful Applications of Biomimicking Adaptive Materials In the Aerospace Industry: UAVs & Hovering Missiles Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted The University of Kansas 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 5. Summary rev. 28 February 2010 65
  • 66. The University of Kansas The University of Minnesota College of Biological Sciences Biomimetic Plant-Cell Based Honeycomb Actuator After: Olympio et al. 2007 Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory Standard Auxetic Hybrid 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 66
  • 67. The University of Kansas College of Biological Sciences 67 Aerocompliance: Key to Birds Wings and PAH Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota Gust load relieving smoothes flight 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 68. The University of Kansas College of Biological Sciences PAH Four-Cell Tensile Test of Steel Honeycombs Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 68
  • 69. The University of Minnesota 69 Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted The University of Kansas Solution: Adaptive Aerostructures Laboratory College of Biological Sciences FAA-Certifiable Actuators based on Plant Cell Structures 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Automotive
  • 70. The University of Kansas College of Biological Sciences Pressure Adaptive Honeycomb (PAH) Breakdown for Modeling Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 70
  • 71. The University of Kansas College of Biological Sciences PAH Nonlinear Mechanics Copyright © R.M. and C.M. Barrett 2013 all rights reserved unclassified ITAR /EAR unrestricted Adaptive Aerostructures Laboratory The University of Minnesota 1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved Unclassified distribution unlimited © R. Barrett All 4.Aerospace 28 February 2010 rev. 5.Summary 71