OPTIMIZED DEVICE FOR THE PROTECTION OF AN ELECTRICAL LINE, ELECTRICAL SYSTEM AND AIRCRAFT.

Abstract

The invention relates to an optimized protection device (1) configured to open a low-voltage power line (10) in the event of an HVDC disturbance, while also directing the potential occurrence of a secondary electric arc. Advantageously, this makes it possible to increase system safety by isolating a power line as effectively as possible in the event of HVDC disturbances exceeding a predetermined intensity. Fig. 1

Description

Title of the invention: OPTIMIZED DEVICE FOR THE PROTECTION OF AN ELECTRICAL LINE, ELECTRICAL SYSTEM AND AIRCRAFT. technical field

[0001] The present invention relates to a device for protecting a low-voltage power line, and in particular to protecting interface signals of onboard aeronautical equipment subjected to induced phenomena from high-voltage circuits. The invention also relates to an electrical system comprising one or more protection devices, as well as an aircraft comprising such an electrical system. PREVIOUS STATE OF THE ART

[0002] The aeronautical industry is making profound changes in aircraft design, with the aim of significantly reducing carbon dioxide and nitrogen oxide emissions, due to ecological and sustainable development constraints.

[0003] The increased use of electrical power in aircraft systems, and in particular propulsion systems, implies the use of numerous interconnected devices that may utilize high-voltage electrical networks (including HVDC networks, an acronym for "High-Voltage Direct Current"). These high-voltage devices, known as "HVDC devices," are also interconnected with the many systems already used in aircraft, such as computers and supervisory systems, for example. Interface circuits called low-voltage interfaces are used to interconnect high-voltage devices with low-voltage devices or with low-voltage power sources. These new architectures introduce a new risk, namely the propagation of HVDC waves or, more broadly, disturbances in low-voltage circuits.Protective measures such as fuses, programmed fuses, isolation barriers, and voltage limiters are available, but the lack of an integrated solution increases the volume and mass of the circuits used, which contradicts the mass reduction typically sought in aeronautics. Some protection systems also utilize predetermined and calibrated weak points in equipment printed circuit boards to allow the opening of power lines in the event of a fault and to limit or prevent the propagation of high-voltage waves or disturbances if a fault occurs. However, such systems are sometimes not completely effective due to... the appearance of secondary electrical arcs. There is therefore a need to limit the effects of secondary arcs by minimizing the mass and volume characteristics of the systems.

[0004] The situation can be improved. Description of the invention

[0005] An object of the present invention is to limit the propagation of high voltage waves or disturbances in electrical circuits by isolating the affected circuits and by controlling and directing possible secondary electrical arcs.

[0006] To this end, a device for opening an electrical line of an electrical circuit is proposed, the opening device comprising a central part of the electrical line, having a first section of a predetermined dimension, and two distal parts of the electrical line, each having a second section of a dimension greater than the dimension of said first section, and respectively connected to said central part, the opening device being such that:

[0007] - each of the distal parts is connected to the central part via a part intermediate electrical line having a third section whose dimension is between the dimension of the first section and the dimension of one of the second sections to which it is adjacent,

[0008] - the portions of the power line, internal to said opening device, and where variations in the dimensions of the cross-section of the power line exist between said central part and said intermediate parts on the one hand, and between each of said intermediate parts and said adjacent distal part on the other hand, and present right or substantially right angles, and

[0009] - a terminal surface of a second power line is arranged opposite one of the said intermediate parts and has right or substantially right angles, so as to create an area of ​​electric arc initiation when a fusion rupture of said central part occurs.

[0010] Thus, in the event of disturbances of the type of HVDC waves on an electrical line, it is possible to direct a secondary arc which originates after the opening of this electrical line by melting the central part of such an electrical line opening device implemented on this electrical line, thanks to a starting zone created by the aforementioned arrangement.

[0011] According to one embodiment, the device is made in the form of a printed circuit board.

[0012] The invention also relates to an electrical system or circuit comprising at least one electrical line opening device as previously described and at least one voltage limiting device.

[0013] Another object of the invention is an aircraft comprising at least one electrical line opening device as previously described or an electrical circuit as mentioned above. Brief description of the drawings

[0014] [Fig-1] illustrates a protection device by opening an electrical line, implemented on an electrical line, according to an embodiment;

[0015] [Fig.2] is a symbolic representation of the protection device already shown on the [Fig.l];

[0016] [Fig.3] illustrates specific dimensions and areas of the protection device already represented on [Fig.1];

[0017] [Fig.4] symbolically illustrates an interface circuit of equipment comprising a protective device such as already shown in [Fig.1], combined with a voltage limiting device;

[0018] [Fig. 5] symbolically illustrates an interface circuit of equipment comprising two protective devices as already shown in [Fig. 1], combined with a voltage limiting device; and,

[0019] [Fig.6] is a side view of an aircraft comprising at least one device of protection advantageously configured to operate an opening of an electrical line in case of HVDC disturbances, according to an embodiment.

[0020] DETAILED STATEMENT OF IMPROVEMENTS

[0021] Figure 1 schematically represents a protection device 1 for an electrical line, also referred to herein as the electrical line opening device 1. According to the example described, the opening device 1 is configured to open the electrical line 10 if it is subjected to an HVDC disturbance likely to compromise its integrity. To this end, the opening device 1 is implemented on the electrical line 10. In other words, the opening device 1 is integrated into the electrical line 10 that it protects. Naturally, elements of the opening device 1 are calibrated so that the opening device 1 opens the electrical line 10 under predetermined conditions.

[0022] The calibration of the opening device 1 according to the described example depends on the intensity of the disturbance to be treated and is carried out by a person skilled in the art from information obtained via simulations or tests and / or laboratory studies.

[0023] To this end, the opening device 1 comprises a central portion 10m and distal portions 10a and 10b serving respectively as connection interfaces to the portions of the power line 10 not included in the opening device 1. Thus, the term "distal" here means that portions 10a and 10b are the portions furthest from the central portion 10m. These portions are useful for the connection of the opening device 1 with the external elements of the power line 10. Advantageously, the central portion 10m has a cross-section substantially smaller than the cross-sections of the distal portions 10a and 10b, so that, in the presence of an HVDC disturbance, the central portion 10m behaves conditionally as a fuse when the energy passing through it exceeds a predetermined threshold value. Thus, if the energy dissipated in the central portion 10m is greater than the predetermined threshold value, the local temperature of the central portion 10m is high enough to cause programmed deterioration (i.e., melting) of the central portion 10m, thereby limiting the propagation of an HVDC disturbance to a predetermined minimum amplitude.Cleverly and advantageously, intermediate connecting zones 10c and lOd, arranged between the central portion 10m and the distal portions 10a and 10b, each have a cross-section with dimensions intermediate between the dimensions of the central portion 10m and the cross-section of the distal portion directly connected to it (immediately adjacent to it). These intermediate connecting zones are also referred to here as intermediate portions. Cleverly further, the intermediate portions 10c and lOd each have sharp angles, preferably right or nearly right angles, so as to create corner effects (increased current density) in the presence of an HVDC disturbance. The term "nearly right angles" here describes angles between 70 and 110 degrees, preferably between 80 and 100 degrees.Finally, a second electrical line 11, connected to a reference equipotential, for example a ground, is implemented near one of the distal parts of the opening device 1 and extends to a predetermined distance from an edge of an intermediate part, presenting a terminal part 11c arranged with sharp angles. Such an arrangement advantageously allows the creation of a secondary arc initiation zone in the event that such a secondary arc should form after the appearance and eventual extinction of a primary arc between the residual intermediate parts, following a melting of the central part 10m resulting from an HVDC disturbance exceeding the threshold calibrated by the different dimensions of the elements composing the opening device 1. Consequently, if a secondary arc were to originate in the event of an HVDC disturbance, it would be channeled by the initiation zone thus created.

[0024] Advantageously, sections Se2 and Se3 (referenced in [Fig. 3]) of the distal parts of the opening device 1 are dimensioned to withstand the maximum currents likely to occur both under normal operating conditions of the power line 10 and under abnormal conditions (i.e., in the presence of an HVDC disturbance). Furthermore, section Se6 (referenced in the [Fig.3]) of the second power line 11, and of its terminal part 1, must be greater than the Sel section of the central part 10m of the opening device 1.

[0025] Obviously, the sizing characteristics of the sections described, and more broadly the sizing characteristics of all the elements of the opening device 1 cannot be defined intrinsically and are predetermined according to the target level of disturbance for which an opening of the opening device 1 must take place, therefore according to the place in an electrical circuit where the opening device 1 is used (or a device of similar architecture), and the nature of the equipment to be protected.

[0026] A person skilled in the art of protection against high voltage electrical disturbances will be able to calibrate the different sections of the opening device 1 described, respecting the relative sizing conditions stated, from charts, preliminary tests, simulations with specialized and dedicated tools, or studies carried out during research and development work.

[0027] Fig. 2 is a symbolic representation of the opening device 1 operating as a normally closed switch (whose opening is, however, irreversible) on the power line 10 prior to an HVDC disturbance likely to cause its opening.

[0028] Figure 3 incorporates elements from Figure 1, to which are added dimensioning references for the various elements that together make up the opening device 1. It can be observed that the central part 10m has a cross-sectional area Sel smaller than the respective cross-sectional areas Se2 and Se3 of the distal parts 10a and 10b. Furthermore, the intermediate parts 10c and 10d each have a cross-sectional area intermediate between the cross-sectional area Sel of the central part 10m and the cross-sectional area of ​​the distal part to which they are directly adjacent. Thus, the intermediate part 10c has a cross-sectional area Se4 larger than the cross-sectional area Sel of the central part 10m and smaller than the cross-sectional area Se2 of the distal part 1a. Similarly, the intermediate part 10d has a cross-sectional area Se5 larger than the cross-sectional area Sel of the central part 10m and smaller than the cross-sectional area Se3 of the distal part 10b.The described arrangement allows for the implementation of a structure (or architecture) with sharp angles between the aforementioned adjacent parts, generating corner effects, namely physical phenomena of increased current and energy density at the corners with sharp angles. Cleverly, the creation of these current densities allows for the definition of arc initiation zones, namely zone ZI (outlined with a dashed line) for the main arc resulting from the fusion of the central 10m part, and zone Z2 (also outlined with a dashed line), cleverly obtained through the aforementioned implementation. variations in sections and to that of sharp angles, preferably in the form of right angles.

[0029] Figure 4 symbolically illustrates the opening device 1 used in combination with a voltage limiting device 101 to protect the power line 10 connected on one side to an electrical or electronic device 10e and on the other side to a connection interface lOi. This arrangement makes it possible to protect the device 10e from HVDC disturbances transmitted via the connection interface lOi, when the device 10e does not itself contain an HVDC circuit (the case of an HVDC disturbance from a source external to the device 10e). The voltage limiting device 101 makes it possible to transiently limit the voltage on the power line 10 to be protected, which ensures that the residual voltage present in the event of an HVDC disturbance remains within acceptable limits for the electrical and / or electronic components connected to the power line 10 downstream of the opening device 1 from the point of origin of a possible HVDC disturbance.Furthermore, the voltage limiting device 101 is configured to absorb a large amount of current, which allows sufficient energy to be dissipated locally by Joule heating to open the opening device 1 by melting its central part 10m. In one embodiment, the voltage limiting device 101 is a gas discharge tube. In another variant, the voltage limiting device 101 is a transient suppression diode. These examples are not limiting, and the voltage limiting device 101 can be chosen from any device capable of limiting the detrimental effects on the components arranged and connected downstream on the power line and of allowing the absorption of a quantity of current sufficient to cause the central part of the opening device 1 to melt.

[0030] In a particular embodiment, when the equipment 10e itself comprises at least one HVDC circuit and there is a risk of disturbance originating internally within the equipment 10e to be protected, a protection circuit such as symbolically illustrated in [Fig. 5] can be used, in which the opening device 1 is used in combination with an opening device 1' which has a structure identical to that of the opening device 1. This makes it possible to limit the risk of propagation of an HVDC disturbance from the equipment 10e to the connection interface 10i (in the case of an HVDC disturbance originating internally within the equipment 10e), according to the same principle as previously stated in relation to [Fig. 4]. The voltage limiting device 101 is then connected to the power line 10 between the opening device 1 and the opening device 1'.

[0031] Fig. 6 illustrates an aircraft 100 comprising one or more opening devices similar to opening device 1, which advantageously allows limiting the propagation of HVDC disturbances, if necessary, within equipment and controlling the sequences of events following such an HVDC disturbance.

Claims

Demands

1. Opening device (1) for an electrical line (10) of an electrical circuit, said opening device (1) comprising a central portion (10m) of said electrical line (10), having a predetermined first cross-section (Sel), and two distal portions (10a, 10b) of said electrical line (10), each having a second cross-section (Se2, Se3) greater than said first cross-section (Sel) and respectively connected to said central portion, the opening device being characterized in that: - each of said distal portions is connected to said central portion via an intermediate portion (10c, 10d) of electrical line having a third cross-section (Se4, Se5) included between the first cross-section (Sel) and one of the second cross-sections (Se2, Se3) of which it is adjacent, - the portions of said electrical line, internal to said opening device, and where there are variations in the cross-section of the electrical line,between said central part and said intermediate parts on the one hand, and between each of said intermediate parts and said adjacent distal part on the other hand, present right or substantially right angles, - a terminal surface (11c) of a second electrical line (11) is arranged opposite one of said intermediate parts and presents right or substantially right angles, so as to create an arc initiation zone during a melting rupture of said central part.

2. Device for opening an electrical line according to claim 1, the device being made in the form of a printed circuit board.

3. Electrical circuit comprising at least one opening device (1) of an electrical line according to one of claims 1 and 2 and a voltage limiting device (101).

4. Aircraft comprising at least one opening device (1) for an electrical line according to one of claims 1 and 2 or an electrical circuit according to claim 3.

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