Composite Material Andrew Nydam Slides from Ken Youssefi Mary P. Shafer Fabric Development, Inc. Quakertown, PA 18951
What is a composite Material? A broad definition of composite is: Two or more chemically distinct materials which when combined have improved properties over the individual materials. Composites could be natural or synthetic. Wood is a good example of a natural composite, combination of cellulose fiber and lignin. The cellulose fiber provides strength and the lignin is the "glue" that bonds and stabilizes the fiber. Bamboo is a very efficient wood composite structure. The components are cellulose and lignin, as in all other wood, however bamboo is hollow. This results in a very light yet stiff structure. Composite fishing poles and golf club shafts copy this natural design. The ancient Egyptians manufactured composites! Adobe bricks are a good example. The combination of mud and straw forms a composite that is stronger than either the mud or the straw by itself. Mechanical Engineering Dept.
Fiber Reinforced Polymer Matrix • Transfer Load to Reinforcement • Temperature Resistance • Chemical Resistance Matrix Reinforcement • Tensile Properties • Stiffness • Impact Resistance
Composites Compositesare combinations of two materials in which one of the material is called the reinforcing phase, is in the form of fibers, sheets, or particles, and is embedded in the other material called the matrix phase. Typically, reinforcing materials are strong with low densities while the matrix is usually a ductile or tough material. If the composite is designed and fabricated correctly, it combines the strength of the reinforcement with the toughness of the matrix to achieve a combination of desirable properties not available in any single conventional material.
Composite Material Two inherently different materials that when combined together produce a material with properties that exceed the constituent materials.
Design Objective Performance: Strength, Temperature, Stiffness Manufacturing Techniques Life Cycle Considerations Cost
Reinforcement: fibers Matrix materials Interface GlassCarbonOrganicBoronCeramicMetallic PolymersMetalsCeramics Bonding surface Composites Composites are combinations of two materials in which one of the material is called the reinforcing phase, is in the form of fibers, sheets, or particles, and is embedded in the other material called the matrix phase. Typically, reinforcing materials are strong with low densities while the matrix is usually a ductile or tough material. If the composite is designed and fabricated correctly, it combines the strength of the reinforcement with the toughness of the matrix to achieve a combination of desirable properties not available in any single conventional material. Components of composite materials Mechanical Engineering Dept.
Weight Considerations Aramid fibers are the lightest 1.3-1.4 g/cc Carbon 1.79 g/c Fiberglass is the heaviest 2.4 g/cc Aluminum (for comparison) 2.7g/cc Steel (for comparison) 7.85g/cc Water @20degrees C 1.00g/cc
Strength Considerations Carbon is the strongest 600-800 ksi 5,650 MPa Fiberglass 400-600 ksi 3,447MPa Aramids 400 ksi 2,757 Mpa Steel 77ksi 530MPa
Strength Considerations Carbon is the strongest 600-800 ksi Fiberglass 400-600 ksi Aramids 400 ksi
Impact Resistance Kevlar is the toughest Fiberglass Carbon
Stiffness Considerations Carbon is the stiffest 30-40 msi Aramids 14 msi Fiberglass 10-13 msi
Cost Considerations Fiberglass is cost effective $5.00-8.00/lb. Aramids $20.00/lb Carbon $30.00-$50.00/lb
Fabric Structures Woven: Series of Interlaced yarns at 90° to each other Knit: Series of Interlooped Yarns Braided: Series of Intertwined, Spiral Yarns Nonwoven: Oriented fibers either mechanically, chemically, or thermally bonded
Physical Properties Construction (ends & picks) Weight Thickness Weave Type
Components of a Woven Fabric Mary P. Shafer
Basic Weave Types Plain Weave Mary P. Shafer
Basic Weave Types Satin 5HS Mary P. Shafer
Basic Weave Types 2 x 2 Twill Mary P. Shafer
Basic Weave Types Non-Crimp Mary P. Shafer
Braiding A braid consists of two sets of yarns, which are helically intertwined. The resulting structure is oriented to the longitudinal axis of the braid. This structure is imparted with a high level of conformability, relative low cost and ease of manufacture. Mary P. Shafer
Braid Structure Mary P. Shafer
Types of Braids Mary P. Shafer
Triaxial Yarns A system of longitudinal yarns can be introduced which are held in place by the braiding yarns These yarns will add dimensional stability, improve tensile properties, stiffness and compressive strength. Yarns can also be added to the core of the braid to form a solid braid. Mary P. Shafer
Conclusions Composite materials offer endless design options. Matrix, Fiber and Preform selections are critical in the design process. Structures can be produced with specific properties to meet end use requirements. Mary P. Shafer
Composites The essence of the concept of composites is that the load is applied over a large surface area of the matrix. Matrix then transfers the load to the reinforcement, which being stiffer, increases the strength of the composite.It is important to note that there are many matrix materials and even more fiber types, which can be combined in countless ways to produce just the desired properties. In the United States, composites manufacturing is a 25 billion dollar a year industry. There are about 6000 composites related manufacturing plants and materials distributors across the U.S. The industry employs more than 235,000 people. An additional 250,000 people are employed in businesses that support the composites industry, including materials suppliers, equipment vendors, and other support personnel. About 90% of all composites produced are comprised of glass fiber and either polyester or vinylester resin. Composites are broadly known as reinforced plastics. Mechanical Engineering Dept.
Composites Fibers Matrix materials Mechanical Engineering Dept.
Composites – Polymer Matrix Polymer matrix composites (PMC) and fiber reinforced plastics (FRP) are referred to as Reinforced Plastics.Common fibers used are glass (GFRP), graphite (CFRP), boron, and aramids (Kevlar). These fibers have high specific strength (strength-to-weight ratio) and specific stiffness (stiffness-to-weight ratio) Matrix materials are usually thermoplastics or thermosets; polyester, epoxy (80% of reinforced plastics), fluorocarbon, silicon, phenolic. Mechanical Engineering Dept.
Graphite (99% carbon) or Carbon (80-95% carbon) – more expensive than glass fibers, but lower density and higher stiffness with high strength. The composite is called carbon-fiber reinforced plastic (CFRP). Boron – boron fibers consist of boron deposited on tungsten fibers, high strength and stiffness in tension and compression, resistance to high temperature, but they are heavy and expensive. Aramids (Kevlar) – highest specific strength, toughest fiber, undergoes plastic deformation before fracture, but absorbs moisture, and is expensive. Composites – Polymer Matrix Reinforcing fibers Glass – most common and the least expensive, high strength, low stiffness and high density. GFRP consists 30-60% glass fibers by volume. The average diameter of fibers used is usually less than .0004 inch (.01 mm). The tensile strength of a glass fiber could be as high as 650 ksi (bulk glass Su = 5-150 ksi) Mechanical Engineering Dept.
Properties of Reinforced Plastics The mechanical properties of reinforced plastics vary with the kind, shape, relative volume, and orientation of the reinforcing material, and the length of the fibers. Effect of type, length, % volume, and orientation of fibers in a fiber reinforced plastic (nylon) Mechanical Engineering Dept.
Consumer Composites Typically, although not always, consumer composites involve products that require a cosmetic finish, such as boats, recreational vehicles, bathwear, and sporting goods. In many cases, the cosmetic finish is an in-mold coating known as gel coat. Industrial Composites A wide variety of composites products are used in industrial applications, where corrosion resistance and performance in adverse environments is critical. Generally, premium resins such as isophthalic and vinyl ester formulations are required to meet corrosion resistance specifications, and fiberglass is almost always used as the reinforcing fiber. Industrial composite products include underground storage tanks, scrubbers, piping, fume hoods, water treatment components, pressure vessels, and a host of other products. Applications of Reinforced Plastics Phenolic as a matrix with asbestos fibers was the first reinforced plastic developed. It was used to build an acid-resistant tank. In 1920s it was Formica, commonly used as counter top., in 1940s boats were made of fiberglass. More advanced developments started in 1970s. Mechanical Engineering Dept.
Applications of Reinforced Plastics Advanced Composites This sector of the composites industry is characterized by the use of expensive, high-performance resin systems and high strength, high stiffness fiber reinforcement. The aerospace industry, including military and commercial aircraft of all types, is the major customer for advanced composites. These materials have also been adopted for use in sporting goods, where high-performance equipment such as golf clubs, tennis rackets, fishing poles, and archery equipment, benefits from the light weight – high strength offered by advanced materials. There are a number of exotic resins and fibers used in advanced composites, however, epoxy resin and reinforcement fiber of aramid, carbon, or graphite dominates this segment of the market. Mechanical Engineering Dept.
Composites – Metal Matrix The metal matrix composites offer higher modulus of elasticity, ductility, and resistance to elevated temperature than polymer matrix composites. But, they are heavier and more difficult to process. Mechanical Engineering Dept.
Composites – Ceramic Matrix Ceramic matrix composites (CMC) are used in applications where resistance to high temperature and corrosive environment is desired. CMCs are strong and stiff but they lack toughness (ductility) Matrix materials are usually silicon carbide, silicon nitride and aluminum oxide, and mullite (compound of aluminum, silicon and oxygen). They retain their strength up to 3000 oF. Fiber materials used commonly are carbon and aluminum oxide. Applications are in jet and automobile engines, deep-see mining, cutting tools, dies and pressure vessels. Mechanical Engineering Dept.
Application of Composites Lance Armstrong’s 2-lb. Trek bike, 2004 Tour de France Pedestrian bridge in Denmark, 130 feet long (1997) Swedish Navy, Stealth (2005) Mechanical Engineering Dept.
The lowest properties for each material are associated with simple manufacturing processes and material forms (e.g. spray lay-up glass fibre), and the higher properties are associated with higher technology manufacture (e.g. autoclave moulding of unidirectional glass fibre), the aerospace industry. Higher Specific Strength (strength-to-weight ratio) Advantages of Composites Composites have a higher specific strength than many other materials. A distinct advantage of composites over other materials is the ability to use many combinations of resins and reinforcements, and therefore custom tailor the mechanical and physical properties of a structure. Mechanical Engineering Dept.
Design flexibility Composites have an advantage over other materials because they can be molded into complex shapes at relatively low cost. This gives designers the freedom to create any shape or configuration. Boats are a good example of the success of composites. Corrosion Resistance Composites products provide long-term resistance to severe chemical and temperature environments. Composites are the material of choice for outdoor exposure, chemical handling applications, and severe environment service. Advantages of Composites Mechanical Engineering Dept.
Durability Composite products and structures have an exceedingly long life span. Coupled with low maintenance requirements, the longevity of composites is a benefit in critical applications. In a half-century of composites development, well-designed composite structures have yet to wear out. Advantages of Composites Low Relative Investment One reason the composites industry has been successful is because of the low relative investment in setting-up a composites manufacturing facility. This has resulted in many creative and innovative companies in the field. In 1947 the U.S. Coast Guard built a series of forty-foot patrol boats, using polyester resin and glass fiber. These boats were used until the early 1970s when they were taken out of service because the design was outdated. Extensive testing was done on the laminates after decommissioning, and it was found that only 2-3% of the original strength was lost after twenty-five years of hard service. Mechanical Engineering Dept.
Application of Composites in Aircraft Industry 20% more fuel efficiency and 35,000 lbs. lighter Mechanical Engineering Dept.
Disadvantages of Composites Composites are heterogeneous properties in composites vary from point to point in the material. Most engineering structural materials are homogeneous. Composites are highly anisotropic The strength in composites vary as the direction along which we measure changes (most engineering structural materials are isotropic). As a result, all other properties such as, stiffness, thermal expansion, thermal and electrical conductivity and creep resistance are also anisotropic. The relationship between stress and strain (force and deformation) is much more complicated than in isotropic materials. The experience and intuition gained over the years about the behavior of metallic materials does not apply to composite materials. Mechanical Engineering Dept.
Disadvantages of Composites Composites materials are difficult to inspect with conventional ultrasonic, eddy current and visual NDI methods such as radiography. American Airlines Flight 587, broke apart over New York on Nov. 12, 2001 (265 people died). Airbus A300’s 27-foot-high tail fin tore off. Much of the tail fin, including the so-called tongues that fit in grooves on the fuselage and connect the tail to the jet, were made of a graphite composite. The plane crashed because of damage at the base of the tail that had gone undetected despite routine nondestructive testing and visual inspections. Mechanical Engineering Dept.
Introductory Composite Labs for schools Cloth towel and ice Hockey puck ice and reinforcement fibers Hockey puck concrete and reinforcements Foam beam Foam beam and fiber reinforcement Foam beam and tape