Más contenido relacionado Similar a Solution wings for Aerospace Applications. (20) Más de Shawn Paul Boike (17) 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
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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
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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
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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All Rights Reserved
Mon
2/24
Tue
2/25
Wed
2/26
Zodiac Aero
Aero/Def
Eaton/Parker
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rev. 28 February 2010
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3. 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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4. 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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5. The University of Kansas
College of Biological Sciences
Copyright © R.M. and C.M. Barrett 2013 all rights reserved
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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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6. 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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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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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
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Adaptive Aerostructures Laboratory
University of Florida
1990’s: NASA’s AAW
Lockheed Martin
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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
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Adaptive Aerostructures Laboratory
Air Muscles
McMurtry 2004
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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?
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Adaptive Aerostructures Laboratory
The University of Minnesota
1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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11. The University of Kansas
The University of Minnesota
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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
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12. 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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13. 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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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
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Adaptive Aerostructures Laboratory
The University of Minnesota
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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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1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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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 Minnesota
College of Biological Sciences
Copyright © R.M. and C.M. Barrett 2013 all rights reserved
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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
Copyright © R.M. and C.M. Barrett 2013 all rights reserved
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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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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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
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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
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22. 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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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
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Adaptive Aerostructures Laboratory
The University of Minnesota
1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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24. The University of Kansas
The University of Minnesota
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Adaptive Aerostructures Laboratory
College of Biological Sciences
Copyright © R.M. and C.M. Barrett 2013 all rights reserved
unclassified
Multi-Cell Compression Test
180mm
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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
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Adaptive Aerostructures Laboratory
The University of Minnesota
1.Introduction 2.Nat. Actuators 3.Art.MusclesRights Reserved
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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
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Adaptive Aerostructures Laboratory
The University of Minnesota
High Pressure
Adaptive Honeycomb
Atmospherically Triggered
Adaptive Honeycombs
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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
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The University of Kansas
PAH employs distributed, rather than concentrated actuation...
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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
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
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29. 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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30. 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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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 Minnesota
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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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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
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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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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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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
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Adaptive Aerostructures Laboratory
The University of Minnesota
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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
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+1
0
-1
VS1
VA
Flight Speed, Vflt (kts)
VC
VD
Gust Limits
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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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Adaptive Aerostructures Laboratory
+1
0
-1
VS1
VA
Flight Speed, Vflt (kts)
VC
VD
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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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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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Adaptive Aerostructures Laboratory
The University of Minnesota
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40. 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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College of Biological Sciences
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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42. 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
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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Adaptive Aerostructures Laboratory
College of Biological Sciences
Copyright © R.M. and C.M. Barrett 2013 all rights reserved
unclassified
Questions?
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44. 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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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
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The University of Minnesota
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46. 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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College of Biological Sciences
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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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48. 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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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