ITEM 416 - CARBON FIBER
416.1 Description
    
This Item covers carbon fibers for use to reinforced concrete structures as
    shown on the Plans or as directed by the Engineer.
416.2 Materials Requirements 
416.2.1 Definition / Raw Material 
A carbon fiber also called carbon fibre, graphite fiber, or carbon graphite
    is a long, thin strand of material about 0.005-0.010 mm in diameter and
    composed mostly of carbon atoms. The carbon atoms are bonded together in
    microscopic crystals that are more or less aligned parallel to the long
    axis of the fiber. The crystal alignment makes the fiber incredibly strong
    for its size. Several thousand carbon fibers twisted together to form a
    yarn, which may be used by itself or woven into a fabric. The yarn or
    fabric is combined with epoxy and wound or molded into shape to form
    various composite materials. Carbon fiber has many different weave patterns
    and can be combined with a plastic resin and wound or molded to form
    composite materials such as carbon fiber reinforced plastic (also reference
    as carbon fiber) to provide a high strength to weight ratio materials. The
    density of carbon fiber's also considerably lower than the density of
    steel, making it ideal for applications requiring low weight.
Raw Material
The raw material used to make carbon fiber is called the precursor. About
    90% of the carbon fibers produced are made from polyacrylonitrile. The
    remaining 10% are made from rayon or petroleum pitch. All of these
    materials are organic polymers, characterized by long strings of molecules
    bound together by carbon atoms.
Commercial forms of Carbon Fibers
Carbon fibers are available as "tows" or bundles of parallel fibers. The
    range of individual filaments in the tow is normally from 1000 to 200,000
    fibers. Carbon fiber is also available as a prepreg, as well as in the form
    of unidirectional tow sheets. Typical properties of commercial carbon
    fibers are shown in Table 416.2.1.
        Table 416.2.1 Typical properties of commercial composite reinforcing
        fibers
    
    [constructed from Mallick (1988b) and Akzo-Nobel (1994)]
Fiber
                 
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Typical diameter (microns)
                 
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Specific gravity
                 
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Tensile modulus GPa
                 
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Tensile strength GPz
                 
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Strain to failure, percent
                 
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Coefficient of thermal expansion 10-6/C
                 
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Poisson’s ration
                 
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| Carbon PAN-Carbon T-300a | 
7 x 10-6 (7)
                 
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1.76
                 
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231
                 
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3.65
                 
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1.4
                 
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-0.1 to -0.5 (longitudinal), 7-12 (radial)
                 
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-0.20
                 
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| PITCH-Carbon P-555a | 
10-7
                 
(10)
                 
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2.0
                 
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380
                 
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1.90
                 
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0.5
                 
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-0.9 (longitudinal)
                 
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-
                 
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416.2.2 Sampling and Testing
The product shall be subject to sampling and testing. The product shall
    meet ACI Guidelines and ASTM D 3039.
416.3 Construction Requirements
416.3.1 The Manufacturing Process
The process for making carbon fibers is part chemical and part mechanical.
    The precursor is drawn into long strands or fibers and then heated to a
    very high temperature without allowing it to come in contact with oxygen.
    Without oxygen, the fiber cannot burn. Instead, the high temperature causes
    the atoms in the fiber to vibrate violently until most of the non-carbon
    atoms are expelled. This process is called carbonization and leaves a fiber
    composed of long, tightly inter-locked chains of carbon atoms with only a
    few non-carbon atoms remaining.
The fibers are coated to protect them from damage during winding or
    weaving. The coated fibers are wound unto cylinders called bobbins
416.3.1.1 Spinning
• Acrylonitrile plastic powder is mixed with another plastic, Iike methyl
    acrylate or methyl methacrylate, and is reacted with a catalyst in a
    conventional suspension or solution polymerization process to form a
    polyacrylonitrile plastic.
• The plastic is then spun into fibers using one of several different
    methods. In some methods, the plastic is mixed with certain chemicals and
    pumped through tiny jets into a chemical bath or quench chamber where the
    plastic coagulates and solidifies into fibers. This is similar to the
    process used to form polyacrylic textile fibers. In other methods, the
    plastic mixture is heated and pumped through tiny jets into a chamber where
    the solvents evaporate, leaving a solid fiber. The spinning step is
    important because the internal atomic structure of the fiber is formed
    during this process.
• The fibers are then washed and stretched to the desired fiber diameter.
    The stretching helps align the molecules within the fiber and provide the
    basis for the formation of the tightly bonded carbon crystals after
    carbonization.
416.3.1.2 Stabilizing
Before the fibers are carbonized, they need to be chemicaly altered to
    convert their linear atomic bonding to a more thermally stable ladder
    bonding. This is accomplished by heating the fibers in air to about
    200-300° C for 30-120 minutes. This causes the fibers to pick up oxygen
    molecules from the air and rearrange their atomic bonding pattern. The
    stabilizing chemical reactions are complex and involve several steps, some
    of which occur simultaneously. They also generate their own heat, which
    must be controlled to avoid overheating the fibers. Commercially, the
    stabilization process uses a variety of equipment and techniques. In some
    processes, the fibers are drawn through a series of heated chambers. In
    others, the fibers pass over hot rollers and through beds of loose
    materials held in suspension by a flow of hot air. Some processes use
    heated air mixed with certain gases that chemically accelerate the
    stabilization.
416.3.1.3 Carbonizing
· Once the fibers are stabilized, they are heated to a temperature of about
    1,000-3,000°C for several minutes in a furnace filled with a gas mixture
    that does not contain oxygen. The lack of oxygen prevents the fibers from
    burning in the very high temperatures. The gas pressure inside the furnace
    is kept higher than the outside air pressure and the points where the
    fibers enter and exit the furnace are sealed to keep oxygen from entering.
    As the fibers are heated, they begin to lose their noncarbon atoms, plus a
    few carbon atoms, in the form of various gases including water vapor,
    ammonia, carbon monoxide, carbon dioxide, hydrogen, nitrogen, and others.
    As the noncarbon atoms are expelled, the remaining carbon atoms form
    tightly bonded carbon crystals that are aligned more or less parallel to
    the long axis of the fiber. In some processes, two furnaces operating at
    two different temperatures are used to better control the rate of heating
    during carbonization.
416.3.1.4 Treating the surface
· After carbonizing, the fibers have a surface that does not bond well with
    the epoxies and other materials used in composite materials. To give the
    fibers better bonding properties, their surface is slightly oxidized. The
    addition of oxygen atoms to the surface provides better chemical bonding
    properties and also etches and roughens the surface for better mechanical
    bonding properties. Oxidation can be achieved by immersing the fibers in
    various gases such as air, carbon dioxide, or ozone; or in various liquids
    such as sodium hypochlorite or nitric acid. The fibers can also be coated
    electrolytically by making the fibers the positive terminal in a bath
    filled with various electrically conductive materials. The surface
    treatment process must be carefully controlled to avoid forming tiny
    surface defects, such as pits, which could cause fiber failure.
416.3.1.5 Sizing
· After the surface treatment, the fibers are coated to protect them from
    damage during winding or weaving. This process is called sizing. Coating
    materials are chosen to be compatible with the adhesive used to form
    composite materials. Typical coating materials include epoxy, polyester,
    nylon, urethane, and others.
· The coated fibers are wound onto cylinders called bobbins. The bobbins
    are loaded into a spinning machine and the fibers are twisted into yarns of
    various sizes.
416.3.2 Quality Control 
The very small size of carbon fibers does not allow visual inspection as a
    quality control method. Instead, producing consistent precursor fibers and
    closely controlling the manufacturing process used to turn them into carbon
    fibers controls the quality. Process variables such as time, temperature,
    gas flow, and chemical composition are closely monitored during each stage
    of the production.
416.3.3 Applications 
Carbon Fiber Reinforced Polymer (CFRP) becomes an increasingly notable
    material use in strengthening concrete, masonry, steel cast iron and timber
    structures. It's use in industry can be either for retrofitting to
    strengthen existing structures or an alternative reinforcement (or
    prestressing material) instead of steel from outset of the project.
Retrofitting has become the increasingly dominant use of Carbon Fiber
    Reinforced Polymer (CFRP) and applications include increasing the load
    capacity of old structures (such as bridges) that were designed to tolerate
    far lower service loads than they are experiencing today, seismic
    retrofitting, and repair of damaged structures. Retrofitting is popular in
    many instances as the cost of replacing the deficient structure can greatly
    exceed its strengthening using Carbon Fi Reinforced Polymer (CFRP).
Applied to reinforced concrete structures for flexure, carbon fiber
    typically has a large impact on strength (doubling or more the strength of
    the section is not uncommon), but only a moderate increase in stiffness
    (perhaps a 10% increase). This is because the material used in this
    application is typically very strong (e.g., 3000 MPa ultimate tensile
    strength, more than 10 times mild steel) but not particularly stiff (150 to
    250 GPa, a little less than steel, is typical). As a consequence, only
    small cross-sectional areas of the material" are used. Small areas of very
    high strength but moderate stiffness material will significantly increase
    strength, but not stiffness.
Carbon Fiber Reinforced Polymer (CFRP) can also be applied to enhance shear
    strength of reinforced concrete by wrapping fabrics or fibers around the
    section to be strengthened. Wrapping around sections (such as bridge or
    building columns) can also enhance the ductility of the section, greatly
    increasing the resistance to collapse under earthquake loading. Such
    'seismic retrofit' is the major application in earthquake-prone areas,
    since it is much more economical than alternative methods.
If a column is circular (or nearly so) an increase in axial capacity is
    also achieved by wrapping. In this application, the confinement of the
    carbon fiber wrap enhances the compressive strength of the concrete.
    However, although large increases are achieved in the ultimate collapse
    load, the concrete will crack at only slightly enhanced load, meaning that
    this application is only occasionally used.
Special ultra-high modulus carbon fiber (with tensile modulus of 420 GPa or
    more) is one of the few practical methods of strengthening cast-iron beams.
    In typical use, it is bonded to the tensile flange of the section, both
    increasing the stiffness of the section and lowering the neutral axis, thus
    greatly reducing the maximum tensile stress in the cast iron. Carbon Fiber
    Reinforced Polymer (CFRP) could be used as prestressing materials due to
    high strength. The advantages of Carbon Fiber Reinforced Polymer (CFRP)
    over steel as a prestressing material cause it’s lightweight and corrosion
    resistance should enable the material to be used for applications such as
    in offshore environments.
416.4 Method of Measurement
The carbon fiber shall be measured by the number of square meter placed and
    accepted as shown on the Plans.
416.5 Basis of Payment
The quantity to be paid for, as provided in Section 416.4 Method of
    Measurement shall be paid for at the contract unit price for Carbon Fiber,
    which price and payment shall be full compensation for furnishing and
    placing all materials, including all labor, equipment, accessories, tools
    and incidentals necessary to complete the Item.
Payment will be made under:
Pay Item Number
                 
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Description
                 
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Unit of Measurement
                 
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416
                 
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Carbon (Thickness in mm)
                 
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Square Meter
                 
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