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Aurora Flight Sciences Aurora Flight Sciences
Composite Aircraft: How to Make Airplanes Out of Cloth
Tim Nuhfer
Aerostructures Design
Aurora Flight Sciences 2 10/8/2014
How I got to where I am today
• Grew up in Florida
• B.S. Aerospace Engineering
• Lockheed Martin, Marietta, GA F-22 Raptor, Liaison Engineering
• Gulfstream Aerospace, Savannah, GA Material Review Board and
Composites Shop
• Northrop Grumman, Melbourne, FL Vehicle Structures / Crew and
Equipment
Images from Lockheed Martin, Gulfstream Aerospace, Northrop Grumman
Aurora Flight Sciences 3 10/8/2014
• In-house UAV products Orion
Centaur
Skate
• Aircraft structures Sikorsky, Boeing, Northrop Grumman,
Lockheed Martin, and others
Yes, we compete and team together
• Internship opportunities, even to high schoolers!
• Manassas, VA
• Cambridge MA
• Columbus, MS
• Bridgeport, WV
Aurora Flight Sciences 4 10/8/2014
How do we design an airplane?
• Requirements Customer tells us what they would like an
airplane to do
• Concept Design Small teams from several different
companies comes up with designs that meet those requirements. One or more hopefully gets a contract.
• Preliminary Design A larger team brings a dose of reality to the
concept.
Aerodynamics, propulsion, computers, software, electrical, payload, structure, mechanical systems.
• Detailed Design Create drawings, tooling, manufacturing
planning, lots of coding
• Build, Test, Assemble, Test, Integrate, Test, Fly, Test, Modifications and Upgrades, Test……
Aurora Flight Sciences 5 10/8/2014
What are “Composites”?
• Any structure made of multiple types of materials
laminated to form “composite” structure stronger than the
basic materials
Wood, the original composite
Aluminum sheets laminated with other sheets
Carbon fiber, fiberglass, Kevlar, boron fiber
Aurora Flight Sciences 6 10/8/2014
How does carbon compare to other
materials?
Material Tensile
Strength
Modulus
of
Elasticity
Density Cost
Aluminum 65-75 ksi 10 Msi 0.1 lb/in3 Medium
Steel 180-280 ksi 25-30 Msi 0.3 lb/in3 Low
Carbon
Fiber
75-300 ksi 10-33 Msi 0.05 lb/in3 High
Images from “Composite Airframe Structures”, Michael C.Y. Nui, 1992
Aurora Flight Sciences 7 10/8/2014
Carbon Fiber Basics
• Wet Lay-up Dry fabric is layed into a mold
Epoxy resin is mixed then worked into the fabric either by hand or using pressure or vacuum assisted resin transfer techniques
Typical working time with resin is about 1 to 2 hrs
• Pre-impregnated uni and fabrics (pre-preg) Epoxy is pressed into fabric and tape using
high pressure rollers
Material is sandwiched between layers of carrier film and put onto rolls
Bagged and stored frozen until needed Thawed when ready to work, typical outlife is 7 to 25 days
Images from ministryofwood.com and carbonfiberguru.com
Aurora Flight Sciences 8 10/8/2014
Sandwiches, mmmmm…
• What makes a composite sandwich panel better than a solid panel?
• Think of it like a beam
Load Applied
Replace the middle with core.
Make the outer fibers work to
their full capability
Images from “Composite Airframe Structures”, Michael C.Y. Nui, 1992
Aurora Flight Sciences 9 10/8/2014
Practical uses
• Skin panels
Thin aluminum requires
stiffening to prevent buckling
Composite sandwich panels
can achieve the same or
better buckling strength for
the same or less weight
• Wing spars
• Wing Ribs
Images from “Composite Airframe Structures”, Michael C.Y. Nui, 1992
Aurora Flight Sciences 10 10/8/2014
How to make a part
• Start with a mold or “tool”
“Female” tools will have the part laid up inside of it
“Male” tools will have the part laid up on the outside
• Variety of tool materials
Aluminum, steel, MDF, foam boards…
Must size the tool for thermal growth
• Clean and seal the tool before beginning the lay-up.
Aurora Flight Sciences 11 10/8/2014
Lay-up
• Thaw carbon
• Cut carbon from
the roll
• Perform lay-up
Aurora Flight Sciences 12 10/8/2014
Bagging and cooking
• Perforated release film
• Breather cloth
• Vacuum bag
• Cook in oven Resin will flow throughout the laminate and take a
set
Some systems require an autoclave
Aurora Flight Sciences 13 10/8/2014
Oven vs Autoclave cure cycles
• Oven cure
Entire cure cycle under
vacuum pressure
Max pressure limited to
atmospheric pressure (1 atm)
• Autoclave cure
Autoclave is a large pressure
vessel
Higher pressure allows for
greater compaction
Tooling may be more
expensive to withstand higher
pressure forces
Images from wisoven.com and autoclavesgroup.com
Aurora Flight Sciences 14 10/8/2014
De-mold and trim
• After cure is done
Cut open bag
Pull part from the mold
Trim part to size
Sand and de-burr
Aurora Flight Sciences 15 10/8/2014
Parts are ready, let’s build an airplane
• Parts are held together in assembly jigs and bonded or
bolted together
Image sources: Lockheed Martin and Aurora Flight Sciences
Aurora’s Orion
Wing Assembly
Lockheed Martin’s
Advanced Composites
Cargo Aircraft Fuselage
Assembly
Aurora Flight Sciences 16 10/8/2014
What I use from school
• Math Algebra, Geometry, Trigonometry on a weekly or daily basis
Calculus somewhat more rarely
• Knowing what the calculus means allows me to make simplifications
• English Need to be able to write reports and make presentations
• Chemistry / Materials science Understanding how materials interact with each other is critical
Understanding crystal structure of metals and how it relates to stresses
• Physics F=Ma ∑F=0 ∑M=0
Knowing how to draw a freebody diagram
• Programming Basic understanding of programming logic is critical to being able to
use most engineering software to its fullest
• Art The most brilliant ideas are useless if you can’t present the idea
clearly enough for someone else to make it
• Crafts With composites, being able to use a ruler to draw and cut a straight
line is critical
Aurora Flight Sciences 17 10/8/2014
Questions?