This invention relates to dielectric isolation for fluid conveyance systems. More particularly an invention that will serve to control and prevent lightning high voltage surges being transmitted along fuel and or hydraulic systems with ability to detect life performance. This application can be applied to both industrial and aerospace conveyance where low to high voltage surge of 30,000 Volts is a concern.
Aircraft design of the past were fabricated with the use of lightweight aluminum alloys, which provided excellent conductance and shedding of Lightning strike energy through the outer skin of the aircraft to a lower potential ground. With the advent of new aircraft designs, carbon composite have replaced aluminum resulting in a very highly resistive outer skin. The function of dielectric isolators within hydraulic and fuel systems is therefore to make these highly conductive conveyance systems more resistive then the outer composite skin and ground circuit, therefore minimizing the probability of lightning energy puncturing the composite skin to reach these systems and undermine aircraft safety. These dielectric isolators find applications in dry bay areas of the wing but also can be installed in wet bay areas where they lay immersed and surrounded by fuel for most of their operating life. Current art technologies have been found to have limitations due to the nature of their design and fabrication. There are two distinct types of isolators on the market, the first is doped polymer type designs where a conductive fill in a low percentage is mixed into a dielectric polymer. The fillers used vary from carbon powder to chopped fiber to noble metals. These types of isolators have issue in manufacturing as the filler content and where it gathers within the injection molding process is a highly random event. This means each unit shot in the molding process will vary in its electrical performance dramatically within any given lot sample. This technology is also prone to internal arcing within its matrix. When a high differential voltage is applied one conductive fiber or particle will arc internally over to the next. This arc trace then produces a highly conductive path within the matrix until several paths are produced and is why these devices begin to lose their resistivity with each successive high voltage strike. As they lose their resistivity they begin to drop below the specification thresholds. The higher the voltage differential, the bigger the drop in resistance. The second type of isolator uses conductive coatings applied through spray or dip coating. These are more reliable then the former but their integrity is highly reliant on a very chemically resistive base resin and paint chemical formulation. The paint has to withstand in excess of twenty years of fuel immersion including all of the additive chemicals mixed with the fuel to prevent anti-icing, biocides, corrosion inhibitors, and anti static additives. The kerosene fuel and all of its associated additive chemicals slowly over time will be absorbed into the coating and begin to degrade it. The mechanism observed is a slow rise in resistance to the point where it can exceed the upper resistance thresholds. This is safer then the later polymer doped technologies which become less resistive leading to secondary indirect lightning energy to travel and arc down the fuel system. But both change their properties as a function of time and exposure to their environment. Both technologies are highly prone to huge variation in resistance on a lot basis as the process can never be controlled and the size of the tube and the relative surface area and volume it presents also changes the resistance from a small 0.50 inch size tube all the way up to a 4.00 inch size. Prior art performance changes as a function of time but also lot to lot and size to size. Lightning direct and indirect effects is a pure electrical phenomena as such the application described herein solves the issues of prior art as a pure electrical solution. The application submitted takes state of the art high precision electrical resistive elements and embodies them into an integrated system that yields a high precision dielectric isolator with repeatable and reliable performance under all environments. Integrating the end fitting as part of the one piece housing has several benefits of solving the leak path through prior art bonded end fittings, and allows for greater burst pressure while eliminating secondary arcing around the end ferrule. In summary, the application is a highly repeatable fluid conveying dielectric isolator with high precision electrical resistive elements with known failure rates that meet aircraft life expectancy. The precision of the dielectric isolator's resistance allows in service checks and health monitoring of the conveyance system.
U.S. Cl.
174/2; 174/58; 174/137 R; 174/154; 218/102; 218/138; 218/139; 244/1 A; 244/135 R; 361/18; 361/30; 361/215; 361/58; 361/117; 361/126
Field Search
137/554; 137/798; 174/2; 174/58; 174/137 R; 174/154; 218/1; 218/102; 218/138; 218/139; 244/1 A; 244/135 R; 361/18; 361/30; 361/58; 361/117; 361/126; 252/500
U.S. Patent Documents
In accordance with the present invention which can be applied to both Aerospace and Industrial applications, a system is provided for dielectric isolation for all fluid type conveyance systems. The dielectric isolator consists of three precision electrical resistive elements connected in parallel. An integrated housing made from a high dielectric material such as Peek or any high dielectric material suitable for its surrounding environment and fluid medium. The integrated one-piece housing contains pockets within which the electrical resistive elements are recessed and housed. Contact between all three resistive elements is achieved by their leads wires which are recessed such to make contact with the end collars. Each end collar is bonded to the integrated housing with a conductive bonding adhesive. A high dielectric potting compound is used to cover and pot the resistive elements into the housing. All elements of the invention are considered located and embedded and covered as to provide optimum dielectric high voltage withstanding capability. The one-piece integrated housing provides a leak proof conduit to convey fluid and provides the required end connections to mate with both upstream and downstream system components. Said system is designed to withstand up to 30,000 V which far exceeds current Aerospace standards with static dissipation conducted via the resistive elements embedded within the housing. In another embodiment, a bulkhead type configuration dielectric isolator where a center flange employed allows said invention to be applied as a transition dielectric isolator between storage or holding tanks wet bay to dry bay areas. In another embodiment, a high pressure hydraulic dielectric isolator where the current invention as described is wrapped with reinforcing high dielectric filament winding of glass or Kevlar or other type of non conductive fiber element. Said embodiment and over wrap is added to meet higher system pressure requirements. Said embodiment will incorporate end fittings instead of end ferrules of the type flare-less or flared or female boss suitable for Hydraulic interface. In another embodiment can incorporate any resistance range as required to meet system requirement. In another embodiment can be configured to have one single resistive element or multiple.
In the drawings, like reference numerals are used to designate similar or like parts throughout the drawings. It will be appreciated that the illustrations represent only one of the many boundaries of the invention.
The present application is directed to a dielectric isolator for use in aircraft fuel systems but principle of design can be applied to hydraulic and other Industrial fluid conveyance systems where lightning strike protection is required. With reference to