• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
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  • 优先权
    • 专利摘要:
    The invention relates to a DC-DC converter adapted to be powered by a primary voltage source and to power a control electronics of a three-phase inverter, said three-phase inverter being configured to control a fan of a ventilation system. an aircraft. The DC-DC converter is characterized in that it comprises a transformer (16), a primary circuit (12) comprising two loops forming a symmetrical arrangement, at least one secondary circuit (14) comprising a secondary winding (Ls), adapted to supply on the one hand to the inverter an output voltage equal to twice the peak voltage across the secondary winding (Ls), and on the other hand to a branch of the circuit adapted to provide the inverter with a output voltage equal to the opposite of the peak voltage across the secondary winding (Ls), and in that the controllable transistors (M1, M2) are adapted to be each switched to zero voltage.
    公开号:FR3037453A1
    申请号:FR1555330
    申请日:2015-06-11
    公开日:2016-12-16
    发明作者:Valery Chau；Philippe Preciat；Pascal Rollin；Sonia Dhokkar
    申请人:Labinal Power Systems SAS；
    IPC主号:
    专利说明:

    [0001] CONTINUOUS CONTINUOUS CONVERTER FOR STEERING AN AIRCRAFT FAN INVERTER, CONTROL METHOD AND FAN THEREFOR 1. TECHNICAL FIELD OF THE INVENTION The invention relates to the optimization of a structure of a continuous electrical converter. continued. In particular, the invention relates to a DC-DC converter for controlling a three-phase inverter, in particular a three-phase inverter driving a fan of a ventilation system of an aircraft. 2. Technological background The ventilation systems for regulating the air circulation within an aircraft comprise at least one ventilator adapted to ensure air circulation in the aircraft, in particular in the cabin of the aircraft . Each fan is controlled by a three-phase inverter. The three-phase inverter comprises three power supply arms, each of these arms comprising two isolated-gate bipolar transistors (IGBTs for Insulated Gate Bipolar Transistors). The driving voltage requirements of the IGBT transistors are conventionally +15 V in positive bias voltage and -7.5 V in negative bias voltage. These voltages are provided by at least one DC-DC converter (DC-DC for Direct Current) and in general one IGBT transistor converter.
    [0002] Nevertheless, new generations of fans have been developed, whose mass and volume have been significantly reduced. Thus, in order to benefit from these reductions in mass and volume, it is necessary to use suitable DC-DC converters. In particular, the DC-DC converters currently used have a large size and weight and a large number of components. Thus, they are no longer suitable for new generations of fans in which the space dedicated to the installation of the DC-DC converter is reduced. In addition, because of the reduction of this space, new thermal stresses appear, which current DC-DC converters are not suitable because their performance is too low and causes unacceptable thermal overheating in this reduced space.
    [0003] 3037453 2 It is therefore necessary to propose a new type of DC-DC converter suitable for the new generations of aircraft ventilation system fans. OBJECTIVES OF THE INVENTION The invention aims at overcoming at least some of the disadvantages of known DC-DC converters. In particular, the invention aims to provide, in at least one embodiment of the invention, a DC-DC converter comprising a reduced number of components.
    [0004] The invention also aims to provide, in at least one embodiment of the invention, a DC-DC converter comprising few complex components. The invention also aims to provide, in at least one embodiment of the invention, a DC-DC converter having a footprint and a reduced weight. The invention also aims to provide, in at least one embodiment of the invention, a DC-DC converter having a high efficiency. The invention also aims to provide, in at least one embodiment of the invention, a DC-DC converter whose heating is reduced. 4. DESCRIPTION OF THE INVENTION To this end, the invention relates to a DC-DC converter adapted to be powered by a primary voltage source and to supply a control electronics of a three-phase inverter, said three-phase inverter being configured to control a fan of a ventilation system of an aircraft, characterized in that it comprises: a transformer, comprising two primary windings and at least one secondary winding, a primary circuit, comprising a suitable supply input to be connected to a first terminal of the primary voltage source, said supply input being connected to two switching loops each comprising one of the primary windings of the transformer 3037453 3 and a controllable transistor comprising a parasitic capacitance and thereby forming a mounting symmetrical, at least one secondary circuit, comprising a secondary winding of the transformer, said e secondary winding comprising two terminals connected on the one hand to a capacitive rectification bridge, adapted to supply the inverter control electronics with a positive output voltage equal to twice the peak voltage across the secondary winding and on the other hand to a branch of the circuit adapted to provide the inverter control electronics with a negative output voltage equal to the opposite of the peak voltage across the secondary winding, and in that that the controllable transistors are adapted to each be controlled by a control signal between an on state and a off state, so that when a controllable transistor is in an on state, the other controllable transistor 15 is in a locked state and that when a controllable transistor is switched from the off state to the off state, the two controllable transistors are held in the off state for a dead time so as to perform a switch ation at zero voltage. In the following description, the control voltage of a transistor designates the voltage between the gate and the source for a field effect transistor, the output voltage across a transistor refers to the voltage between the drain and the source for a field effect transistor and the current flowing through the transistor means the current between the drain and the source for a field effect transistor. The conducting state of the controllable transistors corresponds to a state in which a current flows through the transistor and the blocked state of the controllable transistors corresponds to a state in which the current flowing through the transistor is zero or negligible. The controllable transistors thus behave as controllable switches with parasitic capacitance in parallel, the on state corresponding to a closed switch and the off state corresponding to an open switch. A DC / DC converter according to the invention thus makes it possible to control a control electronics of a three-phase inverter with a reduced number of components. In particular, the primary circuit comprises a symmetrical mounting (also called push-pull assembly) comprising only two transistors instead of four transistors in the frequently used full bridge structures. In addition, the structure of the secondary circuit of the DC-DC converter makes it possible to obtain two voltages at the output of the secondary circuit with a single secondary winding. Apart from the primary and secondary windings, the DC-DC converter does not include magnetic components, which generally have a large footprint. The DC-DC converter according to the invention therefore has a smaller footprint than current solutions. The primary circuit comprises a symmetrical mounting controlled so as to perform a switching of the Zero Volt Switching (ZVS) transistors. Thus, each controllable transistor is alternately in an on or off state, but when a controllable transistor goes from the on state to the off state, the other controllable transistor remains in the off state for a dead time, then passes in the passing state. This dead time is a time interval which makes it possible to minimize the switching losses due, in the prior art, to a voltage-current switching with non-zero values. The dead time during which the two transistors are blocked allows voltage-current switching to very low values, resulting in very low switching losses. Thus, the efficiency of the DC-DC converter is improved and the heating is reduced.
    [0005] Zero-voltage switching is ensured during the dead time and by a particular combination of the primary windings and parasitic capacitances of the controllable transistors. A first controllable transistor is in the off state, the voltage at its terminals is at its maximum level and its parasitic capacitance is charged, a second controllable transistor is in the on state, the voltage at its terminals is at its minimum level. and its stray capacitance is discharged. During dead time, the two transistors are in the off state and the primary windings are no longer supplied with current by the primary voltage source. A magnetizing current of the transformer makes it possible to discharge the parasitic capacitance of the first controllable transistor and to charge the parasitic capacitance of the second controllable transistor. Once this charge and this discharging of the parasitic capacitances are completed, the switching can be done without loss: indeed, the transistor comprises a diode which is spontaneously initiated during the dead time. The primary windings and the controllable transistors are thus chosen so that their characteristics allow the switching to zero voltage. In particular, the parasitic capacitances of the transistors, the magnetizing current and the duration of the dead time are chosen so as to obtain zero voltage switching without adding components. The DC / DC converter according to the invention is therefore, in particular thanks to the combination of a push-pull arrangement, a capacitive rectification bridge and a zero voltage switching, perfectly adapted to the constraints of the new generations of Aircraft ventilation system fan, especially in terms of size, weight and thermal efficiency. In addition, its cost is reduced. Advantageously and according to the invention, the three-phase inverter comprising a plurality of insulated gate bipolar transistor, the DC-DC converter is characterized in that it comprises a plurality of secondary circuit 15 each comprising a secondary winding of the transformer, each secondary circuit being adapted to supply at least one insulated gate bipolar transistor of the control electronics of the three-phase inverter. According to this aspect of the invention, the DC-DC converter supplies a plurality of insulated gate bipolar transistors of the three-phase inverter 20 with a single primary power source. Each insulated gate bipolar transistor of the three-phase inverter requiring a secondary winding to obtain a positive and negative voltage, duplicate the number of secondary windings on the same transformer can drive a complete three-phase inverter, which allows a reduction of the the size, the weight and the price of all the DC-DC converters necessary for controlling a fan. Advantageously and according to the invention, the controllable transistors are field effect transistors. Preferably, the controllable transistors of the DC-DC converter are metal-oxide gate field-effect transistors (also called Metal Oxide Semiconductor Field Effect Transistor MOSFETs). Other components may also be used, provided that they are complemented by a freewheeling diode. Advantageously and according to the invention, each loop comprises a capacitor connected to the controllable transistor in parallel with its parasitic capacitance.
    [0006] According to this aspect of the invention, the capacitance of the controllable transistors can be regulated more precisely by the addition of a capacitor in parallel with the parasitic capacitance, in order to control the drift of the parasitic capacitance value of the Mosfet transistor and therefore to ensure zero voltage switching in all cases.
    [0007] The invention also relates to an aircraft system fan, characterized in that it is controlled by a three-phase inverter comprising a control electronics adapted to be powered by at least one DC-DC converter according to the invention. Advantageously and according to this last aspect of the invention, the control electronics of the three-phase inverter comprises three supply arms, each arm being powered by a DC-DC converter according to the invention. Advantageously and according to the invention, the control electronics of the three-phase inverter comprises three power supply arms, and in that it comprises an electrical converter according to the invention comprising six secondary circuits adapted to power the three arms of the power supply. 'food. The invention also relates to a method of controlling a DC-DC converter according to the invention, characterized in that it comprises controlling the two controllable transistors, said first controllable transistor and second controllable transistor, according to the following steps a first step of controlling the first transistor controllable in the on state and the second transistor controllable in the off state, a second step of transition of the first transistor controllable in the off state and the maintenance of the second transistor controllable in the state 30 blocked during the dead time, - a third step of controlling the second controllable transistor 3037453 7 in the on state and the first transistor controllable in the off state, a fourth transition step of the second transistor controllable in the blocked state and the maintenance of the first controllable transistor in the off state during the dead time.
    [0008] The method according to the invention therefore allows control of the DC-DC converter comprising two transition stages in which the two transistors are in a blocked state to allow a zero voltage switching.
    [0009] The invention also relates to a DC-DC converter, a fan and a control method characterized in combination by all or some of the features mentioned above or hereinafter. 5. List of Figures Other objects, features and advantages of the invention will appear on reading the following description given solely by way of non-limiting example and which refers to the appended figures in which: FIG. 1 is a diagrammatic view of a DC-DC converter according to a first embodiment of the invention, - Figures 2a, 2b, 2c and 2d are schematic views of a DC-DC converter according to the first embodiment of the invention. During various stages of a method according to one embodiment of the invention, FIG. 3 represents curves a, b, c respectively representing the control voltages of the controllable transistors, the voltages at the terminals of the controllable transistors, and the currents flowing through the controllable transistors of a DC-DC converter according to the first embodiment of the invention; FIG. The following is a diagrammatic view of a supply chain comprising three DC-DC converters according to the second embodiment of the invention. the invention and a fan according to one embodiment of the invention. 6. Detailed Description of an Embodiment of the Invention The following embodiments are examples. Although the description refers to one or more embodiments, this does not necessarily mean that each reference relates to the same embodiment, or that the features apply only to a single embodiment. Simple features of different embodiments may also be combined to provide other embodiments. Figures, scales and proportions are not strictly adhered to for the purpose of illustration and clarity.
    [0010] Figure 1 shows schematically a DC-DC converter 10 according to a first embodiment. The DC-DC converter comprises a primary circuit 12, a secondary circuit 14 and a transformer 16. The transformer 16 makes the connection between the primary circuit 12 and the secondary circuit 14.
    [0011] In particular, the transformer 16 comprises two perfectly coupled primary windings, a first primary winding Lp1 and a second primary winding 42, and a secondary winding L. The primary windings Lpi. and Lp2 are part of the primary circuit 12 and the secondary winding Ls is part of the secondary circuit 14. The primary circuit 12 is powered by a primary voltage source whose terminals are respectively connected to a VIN supply input so as to power the DC-DC converter. The VIN power input is connected to two parallel switching loops, a first loop and a second loop. The first loop comprises the first primary winding Lp1 and a first controllable transistor M1, and the second loop comprises the second primary winding Lp2 and a second controllable transistor M2. The two loops thus form a symmetrical assembly, also called push-pull assembly. The energy delivered by the primary circuit 12 at the two primary windings is transmitted to the secondary circuit 14 via the transformer 16: the secondary winding Ls recovers a ratio of the primary voltage present at the two primary windings. In particular, the secondary winding Ls has a voltage VsEc at its terminals. The terminals of the secondary winding Ls are connected on the one hand to a first branch comprising a capacitive rectification bridge, comprising two capacitors Cs and Cp and two diodes D1 and D3 forming a circuit called a Schenkel doubler and the other. part of a second branch comprising a diode D2 and a capacitor CN. The capacitor Cs plays the role of capacitive doubler.
    [0012] The first branch is adapted to provide a device, here represented by a resistor Roun, a first output voltage VouTp equal to twice the peak voltage across the secondary winding L. Indeed, as shown in Figure 1 , the voltage VouTp is equal to the sum of the voltage VsEc, the voltage across the capacitor Cs and the voltage across the diode D1. However, the voltage across the capacitor Cs is equal to the sum of the voltage VsEc and the voltage across the diode D3. By neglecting the voltages of the diodes D1 and D3, VouTp = 2XVSEC- The second branch is adapted to provide a device, here represented by a resistor RouT2, a second output voltage VouTN equal to the opposite of the peak voltage. at the terminals of the secondary winding L. Indeed, as shown in Figure 1, the output voltage VouTN is equal to the sum of the opposite of the voltage VsEc and the voltage across the diode D2. By neglecting the voltage of the diode D2, we obtain VouTN = -V SEC. SEC- By dimensioning VSEC peak = 7.5 V, we thus obtain VouTp = 15V and VouTN = -7.5 V, corresponding to the polarization voltages generally necessary for transistors of the IGBT type used in three-phase inverters. For different voltage requirements, it is possible to obtain other values by dimensioning the number of turns of the secondary winding accordingly.
    [0013] Figures 2a, 2b, 2c, 2d show a DC-DC converter according to the first embodiment of the invention during different steps of a method according to an embodiment of the invention. These figures make it possible to see in more detail the operation of the DC-DC converter according to different stages related to the states of the two controllable transistors M1, M2. In these figures, the 30 controllable transistors M1, M2 are each represented, for simplification and for the sake of clarity, by a closed switch (representing a transistor that can be controlled in the on state) or open (representing a transistor that can be controlled in the "blocked state"), at the terminals of which is connected in parallel parasitic capacitance of each controllable transistor, respectively a first parasitic capacitance CDsi of the first controllable transistor M1 and a second parasitic capacitance CD2 of the second controllable transistor M2.
    [0014] The method comprises the following steps: a first step of controlling the first controllable transistor M1 in the on state and the second controllable transistor M2 in the off state, a second transition step of the first controllable transistor M1 in the state blocked and maintaining the second controllable transistor M2 in the off state during a dead time, a third step of controlling the second controllable transistor M2 in the on state and the first controllable transistor M1 in the off state, a fourth step transition of the second controllable transistor M2 in the off state and the maintenance of the first controllable transistor M1 in the off state during a dead time. FIGS. 2a and 2c show the DC-DC converter during the first and the third stages respectively, in which a controllable transistor 20 is in the on state and the other controllable transistor is in the off state. The push-pull circuit of the primary circuit alternately feeds the first primary winding Lp1 or the second primary winding 42. Thus, the current flowing in the secondary winding Ls changes direction according to the primary winding supplied. The first primary winding Lp1 is supplied by the push-pull assembly 25 when the first controllable transistor M1 is in the on state and the second controllable transistor M2 is in the off state, as shown with reference to FIG. 2a. The second primary winding Lp2 is energized when the first controllable transistor M1 is in the off state and the second controllable transistor M2 is in the on state, as shown with reference to FIG. 2c.
    [0015] A first load current flowing through the resistor Roun and a second load current through the resistor Rou-r2 are provided differently in the direction of the current flowing through the secondary winding L. When the second primary winding Lp2 is energized, as shown With reference to FIG. 2c, the capacitor Cs charges V up to - SEC peaks the capacitor Cp provides the first charging current, the capacitor CN is charged V up to - peak SEC and the secondary winding Ls provides the second charging current. When the first primary winding Lp1 is energized, as shown with reference to Figure 2a, the capacitor Cs discharges into the capacitor Cp and provides the first charging current, the capacitor CN provides the second charging current. Figures 2b and 2d show the DC / DC converter 10 respectively during the second and fourth stages, in which the two controllable transistors are in the off state. These steps are transition steps, making it possible to obtain a zero-voltage switching by keeping the two controllable transistors in the off state during a dead time.
    [0016] The second step follows the first step in which the first controllable transistor M1 was on. Thus, at the beginning of the second step, the first CDi parasitic capacitance of the first controllable transistor M1 is discharged and the output voltage across the first controllable transistor M1 is at its minimum level, that is to say close to zero. Since the second controllable transistor M2 is blocked in the first and second stages, the second parasitic capacitance CD2 of the second controllable transistor M2 is charged and the output voltage across the second controllable transistor M2 is at its maximum level. The two primary windings are no longer powered by the primary voltage source and a magnetizing current propagates in the direction indicated by the arrows on the two loops in Figure 2b. This magnetizing current causes the charge of the first parasitic capacitance CD1 and the discharge of the second parasitic capacitance CD2. Thus, the output voltage across the first controllable transistor M1 grows gradually and the output voltage across the second controllable transistor M2 decreases gradually. To adjust the rate of growth or decay of the voltages, the parasitic capacitance is either only that of the controllable transistor, or an additional capacitor is added in parallel with the parasitic capacitance, the total capacitance then being the combination of the stray capacitance of the 3037453 12 controllable transistor and the capacity of the capacitor in parallel. In a symmetrical manner, in the fourth step shown with reference to FIG. 2d, the first parasitic capacitance CD1 discharges, the output voltage across the first controllable transistor M1 decreases progressively, the second parasitic capacitance CD2 is charged and the voltage output at the terminals of the second transistor controllable M2 grows gradually. The second step and the fourth step last during a predefined dead time depending on the characteristics of the primary windings and parasitic capacitances, so that the end of the dead time, the voltages at the terminals of the controllable transistors reach the maximum value if the voltage increases during the step, or the minimum value if the voltage decreases during the step. In practice, the optimal dead time Tm for an optimal voltage zero switching of a controllable transistor is expressed by the formula: ## EQU1 ## With TON the control time in the on state of the controllable transistor, CDS 15 parasitic capacitance of the controllable transistor and Lp the inductance of the primary winding located in the same loop as the controllable transistor considered. FIG. 3 represents three curves a, b and c respectively representing, as a function of time, the control voltages Vgs_mi and Vgs_m2 of respectively the first controllable transistor M1 and the second controllable transistor M2 (curves 30 and 32), the output voltages Vds_rml and Vds_rm2 across respectively the first controllable transistor M1 and the second controllable transistor M2 (curves 34 and 36), and the intensities Id_mi and Id_m2 respectively passing through the first controllable transistor M1 and the second controllable transistor M2 (curves 38 and 40) d a DC-DC converter 25 according to the first embodiment of the invention. The curves 30, 34, 38 in solid lines are associated with the first controllable transistor M1, and the curves 32, 36, 40 in dashed lines are associated with the second controllable transistor M2. The time zones numbered 1, 2, 3 and 4 correspond respectively to the first, second, third and fourth steps of the control method according to the invention. Curve a thus represents the commands sent to the controllable transistors, the high level representing a control of the transistor that can be controlled in the on state and the low level representing a control of the controllable transistor in the off state. The commands are transmitted for example by a dedicated circuit (not shown), or by an already existing control card, for example an FPGA. During the first step, in the time zone 1, the first controllable transistor M1 is controlled in the on state: the output voltage Vds_mi at its terminals is therefore zero, and the intensity Id_mi of the current passing through it non-zero. The second controllable transistor M2 is controlled in the off state: the output voltage Vds_m2 at its terminals is therefore non-zero and the intensity Id_m2 of the current passing through it is zero (or negligible). During the second step, in the time zone 2 of a duration equal to the dead time described above, the two controllable transistors are controlled in the off state: the output voltage Vds_mi across the first controllable transistor M1 is progressively increased by the load of the first parasitic capacitance CDsi, and the output voltage across the second controllable transistor M2 decreases due to the discharge of the second parasitic capacitance CD2. The intensities of the currents crossing the controllable transistors are close to zero, corresponding to the magnetizing currents crossing the parasitic capacitances. At the beginning of the dead time, the intensity Id_mi of the current flowing through the first controllable transistor M1 is brought to a zero or negligible value before the progressive increase of the output voltage Vds_mi across the first controllable transistor M1. There are therefore no losses due to the switching of the first controllable transistor M1 from the state to the off state at the end of the first step. At the end of the dead time, the intensity Id_m2 of the current flowing through the second controllable transistor M2 is zero or negligible and the output voltage Vds_m2 across the second controllable transistor M2 has progressively reached a zero or negligible value. There are therefore no losses due to the switching of the second controllable transistor M2 from the off-state to the on state at the beginning of the third step. The commutations of the two controllable transistors are therefore zero voltage switching ZVS (for Zero Voltage Switching). The third and fourth steps are similar to the first and second steps, the role of the two controllable transistors being reversed. By virtue of this zero-voltage switching, the efficiency of the DC-DC converter according to the invention is greater than 85% when the DC-DC converter is subjected to a temperature of between -50 ° C. and 115 ° C., which is 5 superior to the converters of the prior art. Figure 4 schematically shows a DC-DC converter 10 according to a second embodiment. The DC-DC converter comprises, identically to the first embodiment described above, a primary circuit and a first secondary circuit 42 comprising a first secondary winding, providing voltages VOUTP_HS and VOUTN_HS. In this embodiment, the DC-DC converter further comprises a second secondary circuit 44, identical to the first secondary circuit 42, comprising a second secondary winding. The transformer 16 'thus comprises the two primary windings described above, as well as the first secondary winding Ls1 and the second secondary winding Ls2. The second secondary circuit 44 makes it possible to obtain new output voltages, a voltage VOUTP_LS and a voltage VOUTN_LS, with a single primary circuit and a single primary power source. A possible use of these new output voltages is described hereinafter with reference to FIG. 5. FIG. 5 represents a supply chain comprising three DC-DC converters 10a, 10b, 10c according to the second embodiment of FIG. and a fan 50 according to one embodiment of the invention. The fan 50 is powered by a three-phase inverter 52 comprising three supply arms 54a, 54b, 54c, the supply arms 54a, 54b, 54c forming a control electronics. Each power supply arm 54a, 54b, 54c comprises two IGBT transistors (not shown), a high-level IGBT transistor (HS) and a low-floor (LS) transistor. . In the prior art, each IGBT transistor in each branch had to be fed by a DC-DC converter, the three-phase inverter being fed by six DC-DC converters.
    [0017] In some prior art solutions, the three low-floor IGBT transistors are powered by a single power supply, the three-phase inverter being powered by four DC-DC converters. The 10 'DC-DC converter according to the second embodiment previously described with reference to FIG. 5 makes it possible to simultaneously power a high stage IGBT transistor, by virtue of the output voltages VOUTP_HS and VOUTN_HS. and a low stage IGBT transistor of a supply arm, thanks to the output voltages VOUTP_LS and VOUTN_LS. The three-phase inverter therefore requires only three converters 10a, 10b, 10c DC-DC. Thus, each supply arm 54a, 54b, 54c is fed by a converter 10a, 10b, 10c continuously, each DC-DC converter 10a, 10b, 10c being fed by a primary power source 56a, 56b, 56c. According to an alternative embodiment not shown, the DC-DC converter comprises six secondary circuits, thus making it possible to supply all the power supply arms of the control electronics of a three-phase inverter. 15
    权利要求:
    Claims (8)
    [0001]
    REVENDICATIONS1. DC-DC power converter adapted to be powered by a primary voltage source (56a, 56b, 56c) and to power a control electronics of a three-phase inverter (52), said three-phase inverter (52) being configured to drive a fan (50) of a ventilation system of an aircraft, characterized in that it comprises: - a transformer (16, 16 '), comprising two primary windings (41, Lp2) and at least one secondary winding (Lb , Ls1, Ls2), - a primary circuit (12), comprising a supply input (VIN) adapted to be connected to a first terminal of the primary voltage source, said supply input (VIN) being connected to two switching loops each comprising one of the primary windings of the transformer (16, 16 ') and a controllable transistor (M1, M2) comprising a parasitic capacitance (Cpsi, CDs2) and thus forming a symmetrical mounting, - at least one secondary circuit (14 , 42, 44), comprising a secondary winding (Lb, Ls1, Ls2) of the transformer, said secondary winding (Lb, Ls1, Ls2) comprising two terminals connected on the one hand to a capacitive rectification bridge, adapted to supply the control electronics of the inverter (52) an output voltage equal to twice the peak voltage across the secondary winding (Lb, Ls1, Ls2) and on the other hand to a branch of the circuit adapted to supply the control electronics of the inverter (52) an output voltage equal to the opposite of the peak voltage across the secondary winding (Lb, Ls1, Ls2), and in that the controllable transistors (M1, M2) are adapted to be each controlled by a control signal between an on state and a off state, so that when a controllable transistor is in an on state, the other controllable transistor is in a locked state and when a controllable transistor is controlled from the state going to the off state, the two transistors controllable (M1, M2) are held in the off state for a dead time so as to perform a zero voltage switching.
    [0002]
    2. DC-DC power converter according to claim 1, the three-phase inverter (52) comprising a plurality of insulated gate bipolar transistor, the DC-DC converter characterized in that it comprises a plurality of secondary circuit (42). , 44) each comprising a secondary winding (Ls1, Ls2) of the transformer (16, 16 '), each secondary circuit being adapted to supply at least one insulated gate bipolar transistor of the control electronics of the three-phase inverter. 10
    [0003]
    3. DC-DC power converter according to one of claims 1 or 2, characterized in that the controllable transistors (M1, M2) are field effect transistors. 15
    [0004]
    4. DC-DC power converter according to one of claims 1 to 3, characterized in that each loop comprises a capacitor connected to the controllable transistor in parallel with its parasitic capacitance.
    [0005]
    5. Aircraft system ventilator, characterized in that it is controlled by a three-phase inverter (52) comprising a control electronics adapted to be powered via at least one electric converter (10, 10 ', 10a, 10b, 10c) according to one of claims 1 to 4.
    [0006]
    6. Aircraft system ventilator according to claim 5, characterized in that the three-phase inverter control electronics (52) comprises three supply arms (54a, 54b, 54c) each powered by a DC-DC converter (10 ', 10a, 10b, 10c) according to one of claims 1 to 4.
    [0007]
    Aircraft system ventilator according to claim 5, characterized in that the three-phase inverter control electronics (52) comprises three supply arms (54a, 54b, 54c), and in that it comprises an electric converter (10 ', 10a, 10b, 3037453 18 10c) according to one of claims 1 to 4 comprising six secondary circuits (14, 42, 44) adapted to supply the three supply arms (54a, 54b , 54c).
    [0008]
    8. A method of controlling a DC-DC converter (10, 10 ', 10a, 10b, 10c) according to one of claims 1 to 4, characterized in that it comprises the control of the two controllable transistors, said first controllable transistor (M1) and second controllable transistor (M2), according to the following steps: - a first step of controlling the first controllable transistor (M1) in the on state and the second controllable transistor (M2) in the state Blocked, - a second transition step of the first controllable transistor (M1) in the off state and the holding of the second controllable transistor (M2) in the off state during the dead time, - a third step of controlling the second transistor controllable (M2) in the on state and the first controllable transistor (M1) in the off state, - a fourth transition step of the second controllable transistor (M2) in the off state and the holding of the first controllable transistor ( M1) in the tat stuck during the timeout. 20
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    同族专利:
    公开号 | 公开日
    US20180138800A1|2018-05-17|
    EP3308455A1|2018-04-18|
    US10396650B2|2019-08-27|
    CN107852097A|2018-03-27|
    FR3037453B1|2017-06-02|
    WO2016198783A1|2016-12-15|
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    CN103078514A|2013-01-05|2013-05-01|浙江大学|Push-pull converter with voltage multiplying resonance capability|US10277128B2|2015-06-29|2019-04-30|Semiconductor Components Industries, Llc|Switch control circuit and buck converter comprising the same|
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    法律状态:
    2016-06-10| PLFP| Fee payment|Year of fee payment: 2 |
    2016-12-16| PLSC| Search report ready|Effective date: 20161216 |
    2017-04-26| PLFP| Fee payment|Year of fee payment: 3 |
    2018-06-05| PLFP| Fee payment|Year of fee payment: 4 |
    2018-08-17| CA| Change of address|Effective date: 20180717 |
    2018-08-17| CD| Change of name or company name|Owner name: SAFRAN ELECTRICAL & POWER, FR Effective date: 20180717 |
    2020-05-20| PLFP| Fee payment|Year of fee payment: 6 |
    2021-05-19| PLFP| Fee payment|Year of fee payment: 7 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1555330A|FR3037453B1|2015-06-11|2015-06-11|CONTINUOUS-CONTINUOUS CONVERTER FOR STEERING AN AIRCRAFT FAN INVERTER, CONTROL METHOD AND FAN THEREFOR|FR1555330A| FR3037453B1|2015-06-11|2015-06-11|CONTINUOUS-CONTINUOUS CONVERTER FOR STEERING AN AIRCRAFT FAN INVERTER, CONTROL METHOD AND FAN THEREFOR|
    US15/580,155| US10396650B2|2015-06-11|2016-06-07|Dc-DC converter for controlling an aircraft fan inverter, and associated control method and fan|
    EP16731243.8A| EP3308455A1|2015-06-11|2016-06-07|Dc-dc converter for controlling an aircraft fan inverter, and associated control method and fan|
    PCT/FR2016/051361| WO2016198783A1|2015-06-11|2016-06-07|Dc-dc converter for controlling an aircraft fan inverter, and associated control method and fan|
    CN201680038689.4A| CN107852097A|2015-06-11|2016-06-07|For controlling the DC DC converters and its corresponding control methods and blower fan of aircraft blower fan inverter|
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