2019
DOI: 10.20998/2074-272x.2019.5.06
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A Choice of Critical Sections of Electric Wires and Cables in Power Circuits of Electrical Equipment of Power Industry

Abstract: Implementation of close calculation determination of critical sections of S Ci and critical amplitudes of density of alternating current δ Ci of frequency 50 Hz in wires and cables of power circuits of electrical equipment of power industry, characterized flowing in it at malfunctions of operation current i k (t) of short circuit (SC) with set amplitude-temporal parameters (ATP). Methodology. Scientific and technical bases of power engineering, electrophysics bases of technique of high-voltage and large pulsed… Show more

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Cited by 2 publications
(4 citation statements)
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“…It can be seen that the indicated values of the skin layer thickness Δ i turn out to be comparable with the radii (thicknesses) of the current-carrying cores (shells) of wires and cables, usually used in electrical circuits of the aircrafts under consideration (in particular, in aircraft networks [7]). As in [1,2], we use the condition of the adiabatic nature of the action of the current i k (t) of a single-phase SC in the on-board network of the aircraft, no more than t kC =40f -1 =100 ms in the conductive materials of the cores (shells) of the thermal process in CCP under consideration, in which the influence of heat transfer from the surfaces of their current-carrying parts having current temperature θ iS ≥θ 0 , and the thermal conductivity of the layers of their electrically conductive materials and insulation on the Joule heating of the current-carrying parts of the cores (shells) of the studied wires (cables) can be neglected. It is required by calculation in an approximate form, taking into account the nonlinear nature of the change, due to the Joule heating of the investigated CCP of the specific conductivity γ i of the material of its cores (shells) and the conditions of the thermal resistibility of the CCP to the action of the current i k (t) of a single-phase SC in the onboard network of the aircraft to determine in the range of change of AC frequency f = (50-400) Hz in the power circuits of its electrical equipment the maximum permissible cross-sections S il of current-carrying parts for uninsulated copper (aluminum) wires, as well as for insulated wires and cables with copper (aluminum) cores (shells), PVC, R and PET insulation, through which in emergency operation mode of the aircraft single-wire onboard network (with a common «minus» on its massive metal casing, which serves as a reverse current lead [10]) or two-wire on-board aircraft network [11] current of a single-phase SC i k (t) flows with known duration t kC and with specified amplitude-temporal parameters (ATPs).…”
Section: приведены результаты предложенного инженерного электротехничmentioning
confidence: 99%
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“…It can be seen that the indicated values of the skin layer thickness Δ i turn out to be comparable with the radii (thicknesses) of the current-carrying cores (shells) of wires and cables, usually used in electrical circuits of the aircrafts under consideration (in particular, in aircraft networks [7]). As in [1,2], we use the condition of the adiabatic nature of the action of the current i k (t) of a single-phase SC in the on-board network of the aircraft, no more than t kC =40f -1 =100 ms in the conductive materials of the cores (shells) of the thermal process in CCP under consideration, in which the influence of heat transfer from the surfaces of their current-carrying parts having current temperature θ iS ≥θ 0 , and the thermal conductivity of the layers of their electrically conductive materials and insulation on the Joule heating of the current-carrying parts of the cores (shells) of the studied wires (cables) can be neglected. It is required by calculation in an approximate form, taking into account the nonlinear nature of the change, due to the Joule heating of the investigated CCP of the specific conductivity γ i of the material of its cores (shells) and the conditions of the thermal resistibility of the CCP to the action of the current i k (t) of a single-phase SC in the onboard network of the aircraft to determine in the range of change of AC frequency f = (50-400) Hz in the power circuits of its electrical equipment the maximum permissible cross-sections S il of current-carrying parts for uninsulated copper (aluminum) wires, as well as for insulated wires and cables with copper (aluminum) cores (shells), PVC, R and PET insulation, through which in emergency operation mode of the aircraft single-wire onboard network (with a common «minus» on its massive metal casing, which serves as a reverse current lead [10]) or two-wire on-board aircraft network [11] current of a single-phase SC i k (t) flows with known duration t kC and with specified amplitude-temporal parameters (ATPs).…”
Section: приведены результаты предложенного инженерного электротехничmentioning
confidence: 99%
“…Introduction. In [1,2], as applied to the tasks of industrial electric power industry, the issues of a refined choice of the maximum allowable S il and critical S iC cross-sections of uninsulated electric wires, as well as insulated wires and cables with polyvinyl chloride (PVC), rubber (R) and polyethylene (PET) insulation and copper (aluminum) cores (sheaths) according to conditions of their, respectively, thermal stability and electric explosion (EE) are considered. As is known, the calculation modes for choosing the maximum allowable cross-sections S il of cable-conductor products (CCP) used in power circuits of electrical equipment with alternating current of frequency f=50 Hz are the modes of single or three-phase short circuit (SC) [3,4].…”
Section: приведены результаты предложенного инженерного электротехничmentioning
confidence: 99%
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