This invention relates to composite transmission and distribution components, and more particularly, to protecting fiberglass components from damage due to handling and environmental issues.
The first composite component designs were developed during the 1960's. From the beginning the advantages of utilizing composite materials in components were clear. The composite components offered:
These advantages have provided a strong impetus for the further development of this technology. However, not all manufacturers were equally successful in producing well performing composite components. While some units have performed exceptionally well, other designs have failed miserably, making it difficult for users to predict whether or not a new design will perform well. The reason for this is the fact that the organic materials used to construct composite components are prone to ageing, which may severely deteriorate the components electrical and mechanical performance over time.
Today, fiberglass components are utilized in numerous applications in transmission and distribution systems. Examples include poles, cross-arms, guy strain insulators, hotsticks, arrestors, bushings and composite insulators. In some of these applications the fiberglass is bare to the environment, or it may be coated with epoxy paint or a rubber weathershed system.
Degradation occurs on fiberglass components that are directly subjected to the environment due to UV, moisture, contamination, and rough handling. In the cases where epoxy coatings are used these coatings have been shown to be fragile and the fiberglass easily exposed and consequently degraded. In the case of composite insulators, the rubber housings have been shown to be tough, but if compromised, moisture can come in contact with the fiberglass insulator which in-turn may result in failure.
Accordingly, this invention aims to impart new surface functionality to GRP (Glass-Reinforced Pultruded)/GFR (Glass Fiber-Reinforced) components, such as rods, not offered by existing technologies—epoxy coating, a veil, or a rubber housing. The coating technology disclosed here provides damage-resistance during handling and installation, while enhancing environmental resistance.
These and other shortcomings of the prior art are addressed by the present invention, which provides a two layer coating adapted to protect fiberglass components used in transmission and distribution systems.
According to one aspect of the invention, a composite component adapted for use in the power transmission industry includes a fiberglass inner core, a pliable first coating layer applied to the fiberglass core, and a hard second coating layer applied to the first coating layer.
According to another aspect of the invention, a composite component adapted for use in the power transmission industry includes a fiberglass inner core, a pliable first coating layer applied to the fiberglass core, and a hard second coating layer applied to the first coating layer. The first coating layer is enriched with ultraviolet absorbers to block ultraviolet light from penetrating into and degrading the fiberglass core. The second coating layer provides mechanical resistance to scratching, abrasion, and impact to prevent the fiberglass core from being exposed to the environment.
The subject matter that is regarded as the invention may be best understood by reference to the following description taken in conjunction with the accompanying drawing figures in which:
Referring to the drawings, an exemplary composite component having a two layer protective coating according to an embodiment of the invention is illustrated in
One of the advantages of the two layer coating is that it bonds well to fiberglass, eliminating the need to sandblast or grind the surface of fiberglass rods to ensure a good bond, thereby reducing manufacturing costs and adding functionality. In addition, rubber can bond well to the coating utilizing standard vulcanizing manufacturing procedures. This enables the utilization of the coating in composite insulator applications where a redundant barrier 16 to moisture penetration or handling damage may be desirable. See
The hard second coating layer 13 provides mechanical resistance to handling (scratch, abrasion and impact) which could result in delamination (See FIG. 6—Delamination causes darkening within the composite), is dense, and acts as a moisture barrier (water causes stress corrosion cracking). The pliable first coating layer 12 is engineered to be UV resistant to block UV rays from penetrating into the fiberglass rod, to prevent cracking of the second coating layer 13, and to provide additional mechanical strength when a metal end fitting is swaged onto the composite component.
Metal end fittings are usually swaged (crimped) on to composite components to allow mechanical attachment to structures, conductors, and other hardware. The mechanical strength of the components is often limited by this swaged interface. Common failures include the metal end fittings slipping off of the composite components.
Generally, hard coatings are not pliable and crack when applied to hard surfaces, especially when metallic end-fittings are crimped on to the ends of a composite component because of the lack of ductility. As shown in
For testing purposes, three coating formulations were used—Formulation A, Formulation B, and Formulation C. The testing results for all three formulations can be seen in the various Figures, but only Formulation B and Formulation C are discussed below in detail.
Coating Formulation B consisted of an organic-inorganic hybrid compound which was synthesized in an aqueous medium. A dip coating process was used to apply the coating formulation in a uniform manner on composite insulator rods and flats, followed by thermal curing.
Coated, flat specimens were used to quantify the adhesion and abrasion resistance with standardized testing. Taber abrasion was evaluated with the weight loss method per ASTM D4060. A Taber Industries 5130 abraser with a Calibrase CS-17 wheel set was used to apply 1500 cycles under a 1 kg load. Samples were weighed before and after the test to determine the mass of material removed as a result of abrasion. Results are shown in
Coating adhesion was evaluated with the tape test method per ASTM D3359. An 11 toothed cutter with 1 mm spacing was used to create a crosshatch of 100 squares on a flat sample. A similar crosshatch was made with a razor on a rod sample. The amount of coating removal after application of a pressure-sensitive tape was evaluated by microscope, as shown in
The Formulation C coating structure consists of two layers. The bottom layer is formed from a sol-gel coating solution having ultraviolet absorbers (UVAs), and the top layer is formed from another sol-gel coating solution. The coatings were deposited as per the following protocol. A dip coating process is used to apply the coating formulation in a uniform manner on composite insulator rods and flats, followed by thermal curing. The bottom layer is first deposited and cured, followed by deposition and curing of the top layer. The dip rate and solids loading of the coating formulation is controlled to obtain the desired film thickness.
Coated, flat specimens were used to quantify the abrasion, adhesion, impact and electrical tracking resistance with standardized tests. Taber abrasion was evaluated with the weight loss method per ASTM D4060. A Taber Industries 5130 abraser with a Calibrase CS-17 wheel set was used to apply 1500 cycles under a 1 kg load. Samples were weighed before and after the test to determine the mass of material removed as a result of abrasion. Results are shown in
Coating adhesion was evaluated with the tape test method per ASTM D3359. An 11 toothed cutter with 1 mm spacing was used to create a crosshatch of 100 squares on a flat sample. The amount of coating removal after application of a pressure-sensitive tape was evaluated by microscope, as shown in
Impact resistance was evaluated under the guidelines of ASTM D5420. Assessments were made by visual inspection and area measurements of the delamination zone. Fiber composite will whiten in the region of deformation, indicating delamination of the fiber and matrix. It is this area that can be compared to observe the effect of the coating on impact resistance. See
Standard insulator rods with the same composite structure as the flats, prepared with and without coatings, were tested for weatherability, moisture penetration and crimping performance. Accelerated weathering tests were conducted under the guidelines of ASTM G53, Fluorescent UV-Condensation. This testing utilizes a UVCON test chamber fitted with fluorescent UV lamps, forced condensation and heating. Samples were subjected to a cyclic exposure of UV at 60° C. and humidity at 50° C. Accelerated weathering by Xenon UV exposure was performed in parallel with UVCON under the guidelines of ASTM G26, xenon-arc type with water. This testing utilizes a Xenon test chamber fitted with a rotating sample rack and humidity controlled to ˜95%. This test was first run continuously for 1500 hours before being interrupted for sample assessment. The control rods showed obvious signs of fiber bloom when viewed on edge under a microscope, while the nanocomposite-coated rods showed very few signs of deterioration. Typical micrographs are shown in
A second, larger set of samples were then tested for statistical significance. Macro photographs were taken to compare the visual appearance of the rods before and after 2200 total hours of testing by each exposure method. The reflectivity of the rod surface can be used to gauge the degree of surface damage from weathering, as shown in
Moisture penetration testing has been conducted on coated and uncoated rod samples by stressing the samples with exposure to a dense water fog, generated by an ultrasonic transducer, for 100 hours at room temperature. Electrical properties of the samples were measured before and after the stress test.
Flat samples, with and without a nanocomposite coating, were subjected to a tracking test by applying a 1 kV potential across the sample while simultaneously flowing a standard contaminant solution across its surface. The samples were photographed periodically throughout the test and a typical result is shown in
Dip-coated rods, 14 inches in length, were sent to the manufacturer to be fitted with standard crimped steel end fittings. The crimped rods were then cross sectioned and examined for signs of coating damage as a result of the crimping process. After cross sectioning, the samples were mounted and polished to reveal microstructural detail at the interface.
The manufacturer-crimped rods were then submitted for a standard pull test. In this test, the rod is placed under tension and the load is gradually increased until failure results. Both fracture and slippage of the rod from the end fitting are considered failure points. The data is graphed in
The foregoing has described a composite component having a two layer protective coating. While specific embodiments of the present invention have been described, it will be apparent to those skilled in the art that various modifications thereto can be made without departing from the spirit and scope of the invention. Accordingly, the foregoing description of the preferred embodiment of the invention and the best mode for practicing the invention are provided for the purpose of illustration only and not for the purpose of limitation.
Number | Date | Country | |
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61725758 | Nov 2012 | US |