• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    An electrical connection (290) adapted to connect a DC high voltage power source (270) to a user equipment (250), the electrical link comprising an electrical conductor (240) surrounded by an insulating envelope . The electrical connection (290) comprises an electrical protection device (200) comprising: - a conductive sheath (280) arranged around the insulating envelope, - a polarization module (245) configured to bias the conductive sheath (280) in tension. ); - a circuit breaker (210) arranged on the conductor (240) and configured to cut a current flowing through the conductor (240), and - a detection module (220) connected to the conductive sheath (280) configured to sense a current leakage out of the conductor (240) and to control the circuit breaker (210) according to the detection. The invention also relates to a method for the secure supply of electrical energy.
    公开号:FR3066040A1
    申请号:FR1753868
    申请日:2017-05-03
    公开日:2018-11-09
    发明作者:Franck Flourens；Christian DONADILLE；Patrick Oms
    申请人:Airbus Operations SAS；
    IPC主号:
    专利说明:

    ELECTRICAL LINK COMPRISING AN ELECTRICAL PROTECTION DEVICE - VOLTAGE POLARIZATION
    TECHNICAL AREA
    The present invention relates to an electrical connection for the transmission of a high voltage direct current to user equipment, said connection comprising an electrical protection device for supplying electrical energy in a secure manner. The invention also relates to a method for the secure supply of electrical energy to user equipment of a vehicle via the electrical connection.
    STATE OF THE ART
    An electrical installation of an aircraft conventionally comprises an electrical power source connected to a user equipment to be supplied with electrical energy via an electrical connection formed by an electrical conductor covered with an insulating envelope. The electrical connection includes a circuit breaker-type device for monitoring the parameters of the electrical signal passing through the connection between the power source and the user equipment in order to interrupt an overload current or a short-circuit current in the conductor.
    The electric power consumed in aircraft is constantly increasing. This development inevitably leads to an increase in the voltage levels of the power supply systems in aircraft which were conventionally 115 AC (AC for alternative current: alternating current) and 28 Volts DC (DC for direct current: direct current).
    Voltages of the order of +/- 270 Volts DC or 540Volts DC are now considered.
    Such voltage values reveal new problems in aircraft. For example, series or parallel arcs can occur during a current leakage outside the electrical connection. A parallel arc between an electrical conductor supplying equipment and the conductive structure of an aircraft, or between two adjacent electrical conductors, could damage the user equipment.
    The circuit breaker type devices of the prior art are not optimized to secure the transmission of energy via the electrical connections of installations using such voltages. Indeed, at such voltages, with the circuit breakers of the prior art, it is mandatory to respect large safety distances between a strand comprising power cables and the chassis of the aircraft, or between a strand comprising power cables and another strand comprising cables for data transmission, in order to prevent a possible electric arc in the strand comprising power cables from damaging the conductive structure of the aircraft by thermal effect, or the strand with cables for data transmission. These security obligations generate significant space constraints in an aircraft.
    STATEMENT OF THE INVENTION
    There is a need to find an electrical protection device for an electrical connection making it possible to secure the supply of high voltage electrical energy to a user equipment of a vehicle, overcoming all or part of the drawback of the aforementioned prior art. . To this end, the invention relates to an electrical connection suitable for connecting a high voltage direct current energy source to user equipment, the electrical connection comprising an electrical conductor surrounded by an insulating envelope, the electrical connection comprising a device for electrical protection comprising: - a conductive sheath arranged around the insulating envelope, - a polarization module configured to polarize the conductive sheath in voltage; - a circuit breaker arranged on the conductor and configured to cut a current flowing through the conductor, and - a detection module connected to the conductive sheath configured to detect a leak of current outside the conductor and to control the circuit breaker. The invention also relates to a method for the secure supply of electrical energy to user equipment of a vehicle via an electrical link (290) connecting the user equipment to a supply source supplying a DC voltage, the electrical link comprising: - an electrical conductor surrounded by an insulating envelope; - an electrical protection device comprising: o a conductive sheath arranged around the insulating envelope; o a polarization module configured to polarize the conductive sheath in voltage; o a circuit breaker arranged on the conductor and configured to cut a current flowing through the conductor; and a detection module comprising a comparator, a first input of which is connected to the conductive sheath and a second input of which is connected to a DC voltage generator supplying a so-called reference voltage, and a microcontroller connected between an output of the comparator and the circuit breaker, the microcontroller being configured to send a control signal to the circuit breaker according to an output signal received from the comparator.
    The method comprises the following successive steps: - injection, by the polarization module, of a direct voltage in the conductive sheath; - comparison, by the comparator of a voltage on the conductive sheath with the reference voltage; - monitoring, by the microcontroller, of the state of the comparator output signal, said state being either a first state indicative of a current leakage outside the electrical conductor or a second state otherwise - activation of the circuit breaker, by the microcontroller, if the comparator output signal is in the first state.
    Thus, the present invention makes it possible to secure the transmission of energy via the electrical connections of installations using high voltages by reducing the distance constraints between an electrical connection and the chassis of the vehicle or between two electrical connections.
    According to a particular embodiment, the detection module comprises: - a comparator, a first input of which is connected to the conductive sheath and a second input of which is connected to a DC voltage generator supplying a so-called reference voltage; and - a microcontroller connected between an output of the comparator and an input of the circuit breaker, the microcontroller being configured to send a control signal to the circuit breaker as a function of an output signal received from the comparator.
    According to a particular mode, the polarization module comprises a DC voltage source and a bidirectional current limiter.
    According to a particular mode, the link comprises a detection module test module, the test module comprising a central unit associated with a first switch and with a second switch, the central unit being configured to control the switching of the switches: the first switch being connected to the first comparator input and being able to switch to a first air terminal or to a second terminal connected to the electrical conductor or to a third terminal connected to a current return line, • the second switch being connected to the microcontroller output of the detection module and able to switch to a first terminal connected to the central unit so that it is the central unit only which receives the control signal from the microcontroller or to a second terminal connected to the circuit breaker so that only the circuit breaker receives the microcontroller control signal.
    According to a particular mode, the detection module comprises a low-pass filter arranged between the conductive sheath and the first input of the comparator.
    According to a particular embodiment, an insulating envelope surrounds the conductive sheath. According to a particular mode, the polarization module injects a voltage of sign opposite to the sign of the voltage supplied by the power source.
    According to a particular mode, the detection module further comprising a test module, the test module comprising a central unit associated with a first switch and with a second switch, the central unit being configured to control the switching of the switches: the first switch being connected to the first comparator input and being able to switch to a first terminal in the air or to a second terminal connected to the electrical conductor. The second switch being connected to the output of the microcontroller of the detection module and being able to switch to a first terminal connected to the central unit so that it is only the central unit which • receives the control signal from the microcontroller or on a second terminal connected to the circuit breaker so that it is the circuit breaker only which receives the control signal from the microcontroller, characterized in that the method comprises a test step, implemented for a predetermined time, during which the central unit controls the first switch to cause it to switch to its second terminal and controls the second switch to cause it to switch over to its first terminal, and in which the central unit monitors a change in state of the control signal of the microcontroller; when the test step is not implemented, the central unit controls the first switch to cause it to switch to its first terminal and controls the second switch to cause it to switch to its second terminal.
    BRIEF DESCRIPTION OF THE DRAWINGS
    The characteristics of the invention mentioned above, as well as others, will appear more clearly on reading the following description of an exemplary embodiment, said description being made in relation to the accompanying drawings, among which: the FIG. 1 represents an aircraft comprising an electrical installation having a power source connected to a user equipment via an electrical connection and a current return line and an electrical protection device of the electrical connection according to an embodiment of the invention ; - Figure 2 shows a block diagram of the electrical installation shown in Figure 1, and a representation of the electrical protection device of the electrical connection according to an embodiment of the invention; - Figure 3 shows a schematic view of a conductive sheath arranged on an electrical connection and forming a part of the electrical protection device according to the invention; - Figure 4 shows an electrical diagram of the electrical installation shown in Figure 2; - Figures 5a and 5b are diagrams illustrating the evolution of the voltages on the conductive sheath according to Figure 3 when the latter is current biased; - Figure 6 is a view similar to Figure 2 wherein the electrical protection device of the driver further comprises a test module according to an embodiment of the invention; and - Figure 7 shows an electrical diagram of the electrical installation shown in Figure 6.
    DETAILED DESCRIPTION OF EMBODIMENTS
    In connection with FIG. 1, an aircraft 10 comprises an electrical installation having a high voltage power supply source 270 connected to user equipment 250 via an electrical link 290 comprising an electrical protection device 200 associated with the electrical link 290.
    The electrical power source 270 is further connected to the user equipment 250 by a current return line 260.
    The high-voltage power supply 270 supplies a continuous HV voltage of about + or - 270 Volts DC, or even 540Volts DC. The aircraft 10 further comprises a conductive structure (not shown) which is formed by any metallic / conductive element of the aircraft which is at the reference potential and forms the mass.
    With reference to FIGS. 2 to 3, and according to the invention, the electrical connection 290 comprises an electrical conductor 240 surrounded by an insulating envelope 320 (for example a plastic sheath) and the electrical protection device 200 comprises a part arranged on the insulating envelope 320 of the conductor 240, and a part composed of electronic devices, for example arranged in a secure box 12.
    The part arranged on the insulating envelope 320 comprises a conductive sheath 280 surrounded by an insulating envelope 310, the conductive sheath 280 surrounding the insulating envelope 320 of the conductor 240.
    The part located in the housing 12 (see FIG. 2) comprises: • a circuit breaker 210 connected to the electric power source 270 and which, when controlled in this direction, makes it possible to interrupt the supply of the signal HV to the user equipment 250 via the electrical conductor 240. In known manner, the circuit breaker 210 functions as a switch which, when activated, opens and thus turns off the electrical conductor 240; • a polarization module 245 for voltage biasing the conductive sheath 280; and • a detection module 220 for detecting a leak of current outside the electrical conductor 240.
    A current leak occurs when the electrical connection 290 is damaged. For example, a current leak occurs during contact of the conductor 240 with the conductive sheath 280 when the insulating envelope 320 is damaged or contact of the conductor 240 with an element external to the electrical connection when the two insulating envelopes 310 and 320 are damaged. A current leak can lead to the creation of electric arcs between the conductor 240 and the conductive structure of the aircraft 10 or with another conductor put at a potential different from the conductor or with the current return line 260 if the latter is at a potential differ from ground.
    The electrical connection 290 advantageously extends from the housing 12 to the user equipment 250 (only a portion of the electrical connection has been shown in FIG. 4).
    With reference to FIG. 4, the polarization module 245 comprises a DC voltage source 245a supplying a voltage V_PSS to ensure the polarization function of the conductive sheath 280 and a protection circuit, such as for example a bidirectional current limiter 245b , which has the function of allowing the voltage to fluctuate on the conductive sheath 280. The voltage source 245a is connected between the current return line 260 and a first termination of the bidirectional current limiter 245a. The second termination of the bidirectional current limiter 245a is connected to the conductive sheath 280.
    The voltage V_PSS delivered by the voltage source 245a is lower in absolute value than the voltage delivered by the electric power source 270, and it is given a value which is not dangerous for people.
    Preferably, the sign of the voltage V_PSS delivered by the voltage source 245a is also inverse to that of the voltage HV delivered by the electric power source 270, in order to facilitate the detection of a passage or a leak of current outside the electrical connection 290. For example, the voltage V_PSS delivered by the voltage source 245a is -30 Volts for a HV voltage of 540 Volts.
    The detection module 220 comprises a comparator 220a as well as a microcontroller 220b connecting the output of the comparator 220a to the input of the circuit breaker 210. The microcontroller 220b receives an output signal VComp from the comparator 220a and the latter provides a signal of control at circuit breaker 210.
    The comparator 220a is connected, on a first input, to the conductive sheath 280, and on a second input, to a DC voltage generator (not shown) supplying a voltage, called reference, Vref.
    The comparator 220a compares the voltage V280 in the conductive sheath 280 with the reference voltage Vref so as to detect a current leakage outside the conductor 240. The output signal VComp of the comparator takes two states, ie a first state (for example 1 in Boolean logic) indicative of a current leak out of the electrical conductor 240, ie a second state (for example 0) otherwise.
    The reference voltage is chosen according to the sign of the voltage HV delivered by the high-voltage power source 270 and according to the sign of the voltage V_PSS.
    In an example where the high voltage power source 270 produces a positive voltage, and the voltage source 245a supplies a voltage V_PSS of negative sign, the negative input of the comparator 220a is connected to the DC voltage generator which supplies the voltage of reference Vref chosen greater than the voltage V_PSS delivered by the voltage source 245a. For example, the voltage Vref is equal to -25Volts for V_PSS to -30Volts. In this example, the comparator output signal VComp goes from the second state to the first state (for example 1 in Boolean logic) when V280 is greater than Vref, and is in the second state (for example 0) when V280 is less than Vref .
    As an option, the comparator 220a includes a low pass filter (active, passive or hybrid) 220c arranged on the electrical connection between the conductive sheath 280 and the input of the comparator 220a so as to eliminate any interference signals present on the sheath conductive 280 and which could distort the results of the comparisons made by the comparator 220a.
    In relation to FIG. 5a, an example of the evolution of the signals Vref, V280, HV (the signal on the conductor 240) and VComp is shown over time, when from a time Tl, the electrical connection 290 has a fault (case of a fault / rupture of the insulating envelope 320 of the conductor 240) and a situation of current leakage outside the conductor 240 appears.
    In this example, the high voltage power source 270 produces a positive HV voltage: HV = 540 Volts (the logic given below would be reversed for negative HV) V_PSS = -30 Volts,
    Vref = -25 Volts, In FIG. 5a, from the time T1 and for a duration T5a, the conductive sheath 280 is in contact with the conductor 240.
    Before the time T1, the signal V280 on the conductive sheath 280 is equal to the DC voltage V_PSS fixed at -30 Volts and therefore greater in absolute value than Vrefl which is fixed at -25Volts. The output signal Vcomp of the comparator 220a is therefore in its second state, for example at 0. The conductive sheath 280 is not in contact with the conductor 240 or no electric arc exists between the conductive sheath 280 and the conductor 240 .
    After Tl, and for the duration noted T5a, the conductive sheath 280 is in contact with the conductor 240 (either directly or by the formation of an electric arc). The signal V280 on the conductive sheath 280 is equal to the voltage HV on the conductor 240 and is therefore greater than Vref. The output signal VComp of the comparator 220a therefore passes from the second state to its first state, for example goes from 0 to 1. The microcontroller 220b sends a signal to the circuit breaker 210 to thereby put the conductor 240 off.
    After the duration T5a, the supply of electrical energy is interrupted and the voltage HV becomes zero.
    The duration T5a is determined so as to be free from any parasitic pulses which could cause false detections.
    Thanks to the present invention, as soon as contact of the conductive sheath 280 with the electrical conductor 240 is detected, the supply of electrical energy is interrupted after a brief reaction time T5a of the electronic circuits. The voltage-polarized conductive sheath 280 thus forms a detector capable of detecting damage to the electrical connection 290. The rapid interruption (a few milliseconds) of the electrical energy prevents the creation / propagation of electric arcs and thus the possible damage by effect that could occur to surrounding materials as well as the injection of current into surrounding materials, as well as the propagation of high voltage HV in other cables / conductors.
    In relation to FIG. 5b, an example of the evolution of the signals Vref, V280, HV (the signal on the conductor 240) and VComp is shown over time, when from a time Tl, the electrical connection 290 is brought into contact with the current return line 260 and has a fault: case of a fault / rupture of the insulating casing 310 of the conductive sheath 280. This example aims to show that, thanks to the present invention, from that contact of the conductive sheath 280 with the current return line 260 or the conductive structure of the aircraft is detected, the supply of electrical energy is interrupted. 11
    In this example, the high voltage power source 270 produces a positive HV voltage: HV = 540 Volts (the logic given below would be reversed for negative HV), V_PSS = -30 Volts,
    Vref = -25 Volts Ohms. From time T1 and for a period T5b, the conductive sheath 280 is in contact with the current return line 260, the conductor 240 and the conductive sheath being isolated from each other (no current leakage outside of the driver).
    Before the time T1, the signal V280 on the conductive sheath 280 is equal to the DC voltage V_PSS of -30 Volts and therefore greater in absolute value than Vref fixed at -25Volts. The output signal VComp of the comparator 220a is therefore in its second state, for example at 0. The conductive sheath 280 is not in contact with the return line 260 or no electric arc exists between the conductive sheath 280 and the return line 260.
    During the duration T5b, the conductive sheath 280 is in contact with the current return line 260. The voltage V280 on the conductive sheath 280 changes to zero voltage, greater than Vref. The output signal VComp of the comparator 220a therefore passes from the second state to its first state, for example goes from 0 to 1. The microcontroller 220b sends a signal to the circuit breaker 210 to thereby put the conductor 240 off.
    After the duration T5b, the supply of electrical energy is interrupted and the voltage HV becomes zero.
    Thus, according to the invention, when the conductive sheath 280 polarized in voltage is no longer able to perform its function of detector capable of detecting damage to the electrical connection 290, the conductor 240 is insulated to completely secure the installation electric.
    The duration T5b is determined so as to be free from any parasitic pulses which could cause false detections.
    In an alternative embodiment of the invention shown in FIGS. 6 and 7, the electrical protection device 200 also comprises a test module 230 making it possible to verify the correct operation of the detection module 220. The test module 230 is, for example, consisting of a central unit 230a associated with a first switch SW1 and a second switch SW2.
    The switch SW1 is connected to the input of the detection module 220 and can switch to three different terminals: • a first terminal in the air; or • a second terminal connected to the conductor 240; or • a third terminal connected to the current return line 260.
    The switch SW2 is connected to the output of the detection module 220 and can switch on two different terminals: • a first terminal connected to the central unit 230a so that it is only the central unit which receives the control signal microcontroller 220b; or • a second terminal connected to the input of the circuit breaker 210 so that it is the circuit breaker only which receives the control signal from the microcontroller 220b. The central unit 230a is configured to control the switches SW1, SW2 and to implement a first and a second test program at regular intervals.
    When the central unit 230a does not implement the test program, the switch SW 1 switches to its first terminal and the switch SW2 switches to its second terminal.
    On the other hand, when the central unit 230a implements the first test program: the switch SW 1 switches to its second terminal so as to force the input of the detection module 220 with the conductor 240 (to force the passage of the signal of output VComp of comparator 220a to pass from the second state to the first state, case of FIG. 5a for example) and the switch SW2 switches on its first terminal so as not to activate the circuit breaker 210 during the implementation of the test . Only the microcontroller receives a signal from the detection module 220 and can check whether the latter is operational, that is to say has indeed generated an order to activate the circuit breaker 210 during the test. If, after a predetermined test time, the detection module 220 has not generated an order to interrupt the supply of electrical energy, the central unit 230a of the test module 230 emits an alert to destination of an operator who can, according to his choice, maintain the supply of electrical energy until the end of the flight, for example, or cause the interruption of the supply of electrical energy by actuating, for example, a circuit breaker in the cockpit of the aircraft. An operator will have to repair the detection module 220 so that the system for securing the supply of electrical energy becomes operational again.
    When the central unit 230a implements the second test program: the switch SW1 switches to its third terminal so as to force the input of the arc and / or contact detection module 220 with the current return line 260 (to force the passage of the output signal VComp of the comparator 220a to pass from the second state to the first state, case of FIG. 5b for example) and the switch SW2 switches on its first terminal so as not to activate the circuit breaker 210 during the implementation of the test. Only the central unit 230a receives a signal from the detection module 220 and can check whether the latter is operational, that is to say has indeed generated an order to activate the circuit breaker 210. If, at the end a predetermined test time, the detection module 220 has not generated an order to interrupt the supply of electric energy, the central unit 230a of the test module 230 issues an alert to an operator who may, according to its choice, maintain the supply of electrical energy until the end of the flight for example, or cause the interruption of the supply of electrical energy by actuating for example a circuit breaker in the cockpit of the aircraft. An operator will have to repair the detection module 220 so that the system for securing the supply of electrical energy becomes operational again.
    In the above description, by current return line 260 is meant either a return conductor or a current return network. If the current return line 266 is a conductor placed at a voltage different from that of the conductive structure of the aircraft, then an electrical protection device as described above must be associated with the current return line 266 to secure the current return. The invention has been described to protect the transmission of electrical energy via an electrical connection of an electrical installation of an aircraft 10. However, the invention finds application to any other type of vehicle, for example a ship or an automobile . The invention has been described, in particular via the examples illustrated in FIGS. 5a and 5b, for a positive HV voltage and a negative V_PSS voltage. The modification of the invention to take into account other parameters (positive or negative HV voltage, positive or negative V_PSS voltage) is within the reach of the skilled person.
    权利要求:
    Claims (9)
    [1" id="c-fr-0001]
    CLAIMS 1) Electrical connection (290) adapted to connect a high voltage direct current energy source (270) to user equipment (250), the electrical connection comprising an electrical conductor (240) surrounded by an insulating envelope (320 ), characterized in that the electrical connection (290) comprises an electrical protection device (200) comprising: - a conductive sheath (280) arranged around the insulating envelope (320), - a polarization module (245) configured for voltage biasing the conductive sheath (280); - a circuit breaker (210) arranged on the conductor (240) and configured to cut a current passing through the conductor (240), and - a detection module (220) connected to the conductive sheath (280) configured to detect a current leakage out of the conductor (240) and to control the circuit breaker (210).
    [0002]
    2) Connection (290) according to claim 1, characterized in that the detection module (220) comprises: a comparator (220a) of which a first input is connected to the conductive sheath (280) and of which a second input is connected to a DC voltage generator providing a so-called reference voltage (Vref); and a microcontroller (220b) connected between an output of the comparator (220) and an input of the circuit breaker (210), the microcontroller being configured to send a control signal to the circuit breaker according to an output signal received from the comparator (220a).
    [0003]
    3) Connection (290) according to any one of claims 1 to 2, characterized in that the polarization module (245) comprises a DC voltage source (245a) and a bidirectional current limiter (245b).
    [0004]
    4) Connection (290) according to claim 2, characterized in that it comprises a test module (230) of the detection module (220), the test module comprising a central unit (230a) associated with a first switch ( SW1) and a second switch (SW2), the central unit being configured to control the switching of the switches: • the first switch (SW1) being connected to the first comparator input (220a) and being able to switch to a first terminal in air or on a second terminal connected to the electrical conductor (240) or to a third terminal connected to a current return line (260), • the second switch (SW2) being connected to the output of the microcontroller (220b) of the detection module (220) and able to switch to a first terminal connected to the central unit (230a) so that it is only the central unit which receives the control signal from the microcontroller (220b) or to a second terminal connected at circuit breaker (220) so that it is the circuit breaker only which receives the control signal from the microcontroller (220b).
    [0005]
    5) Connection (290) according to any one of claims 2 to 4, characterized in that the detection module (220) comprises a low-pass filter (220c) arranged between the conductive sheath (280) and the first input of the comparator (220a).
    [0006]
    6) Connection (290) according to any one of claims 1 to 5, characterized in that an insulating envelope (310) surrounds the conductive sheath (280).
    [0007]
    7) Method for the secure supply of electrical energy to user equipment (250) of a vehicle (10) via an electrical link (290) connecting the user equipment (250) to a power source (270) providing a direct voltage (HV), the electrical connection (290) comprising: - an electrical conductor (240) surrounded by an insulating envelope (320); - an electrical protection device (200) comprising: o a conductive sheath (280) arranged around the insulating envelope (320); o a polarization module (245) configured to voltage bias the conductive sheath (280); o a circuit breaker (210) arranged on the conductor and configured to cut a current passing through the conductor (240); and a detection module (200) comprising a comparator (220a), a first input of which is connected to the conductive sheath (280) and a second input of which is connected to a DC voltage generator supplying a so-called reference voltage (Vref) , and a microcontroller (220b) connected between an output of the comparator (220a) and the circuit breaker (210), the microcontroller being configured to send a command signal to the circuit breaker according to an output signal received from the comparator (220a), o characterized in that the method comprises the following successive stages of: - injection, by the polarization module (245), of a direct voltage (V_PSS) in the conductive sheath (280); - comparison, by the comparator (220a), of a voltage (V280) on the conductive sheath (280) with the reference voltage (Vref); - Monitoring, by the microcontroller (220b), of the state of the comparator output signal (220a), said state being either a first state indicative of a current leakage out of the electrical conductor (240) or a second state otherwise , - activation of the circuit breaker (210), by the microcontroller (220b), if the comparator output signal is in the first state.
    [0008]
    8) Method according to claim 7, characterized in that the polarization module (245) injects a voltage (V_PSS) of opposite sign to the sign of the voltage (HV) supplied by the power source (270).
    [0009]
    9) The method of claim 7, the detection module (220) further comprising a test module (230), the test module comprising a central unit (230a) associated with a first switch (SW1) and a second switch (SW2), the central unit being configured to control the switching of the switches: • the first switch (SW1) being connected to the first comparator input (220a) and being able to switch to a first terminal in the air or to a second terminal connected to the electrical conductor (240). • the second switch (SW2) being connected to the output of the microcontroller (220b) of the detection module (220) and being able to switch to a first terminal connected to the central unit (230a) so that it is the unit central unit only which receives the control signal from the microcontroller (220b) or on a second terminal connected to the circuit breaker (220) so that it is the circuit breaker only which receives the control signal from the microcontroller (220b), characterized in that the method comprises a test step, implemented for a predetermined time, during which the central unit (230a) controls the first switch (SW1) to make it switch to its second terminal and controls the second switch ( SW2) to make it switch to its first terminal, and in which the central unit (230a) monitors a change in state of the control signal of the microcontroller (220b); when the test step is not implemented, the central unit (230a) controls the first switch (SW1) to make it switch to its first terminal and controls the second switch (SW2) to make it switch to its second terminal.
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    同族专利:
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    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US6218647B1|1998-01-19|2001-04-17|Msx, Inc.|Method and apparatus for using direct current to detect ground faults in a shielded heater wire|
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    CN109799410B|2019-03-19|2021-03-26|西北工业大学|Flight profile control device, and airplane power system comprehensive test system and method|
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    2018-11-09| PLSC| Publication of the preliminary search report|Effective date: 20181109 |
    2019-05-23| PLFP| Fee payment|Year of fee payment: 3 |
    2020-05-22| PLFP| Fee payment|Year of fee payment: 4 |
    2021-05-20| PLFP| Fee payment|Year of fee payment: 5 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1753868|2017-05-03|
    FR1753868A|FR3066040B1|2017-05-03|2017-05-03|ELECTRICAL LINK INCLUDING AN ELECTRICAL PROTECTION DEVICE - VOLTAGE POLARIZATION|FR1753868A| FR3066040B1|2017-05-03|2017-05-03|ELECTRICAL LINK INCLUDING AN ELECTRICAL PROTECTION DEVICE - VOLTAGE POLARIZATION|
    US15/969,268| US10951019B2|2017-05-03|2018-05-02|Electrical link comprising an electrical protection device—voltage bias|
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