• 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:
    Pilot stage (20) of a servovalve (100) having a hydraulic ejector (30) and a hydraulic receiver (6) displaceable relative to each other, one of the hydraulic elements (30) being secured to a movable member (21) movable relative to a body of the servovalve (100) by actuating means (40), characterized in that the actuating means (40) comprise two piezoelectric actuators (41, 42) connected in series. Control device comprising a servovalve (100) comprising such a control stage (20)
    公开号:FR3051026A1
    申请号:FR1653985
    申请日:2016-05-03
    公开日:2017-11-10
    发明作者:Jean-Luc Bertrand；Catherine Mailhan
    申请人:Zodiac Hydraulics SAS；
    IPC主号:
    专利说明:

    FIELD OF THE INVENTION The invention relates to a servo valve control stage, which can serve as a first stage in a two-stage servo valve.
    BACKGROUND OF THE INVENTION
    A conventional servovalve consists of a control stage controlling a mobile power distribution member of a power stage. The function of the power stage is to deliver a pressure or a flow proportional to an instruction transmitted to the control stage. The control stage comprises two hydraulic elements, namely a hydraulic transmitter (nozzle or ejector) and a hydraulic receiver (pallet, deflector or fixed receiver) whose modification of their relative position generates pressure differentials which are exploited to move finely. a movable power distribution member of the power stage of the servovalve. This mobile power distribution member slides in a cylindrical jacket implanted in the body of the servovalve. Generally, the relative position of the hydraulic elements is controlled by a torque motor comprising a set of coils acting on a mobile magnetic pallet integral with one of the hydraulic elements of the control stage. A setpoint current applied by a control unit to the coils of the torque motor causes a displacement of the pallet and therefore a modification of the relative position of the hydraulic element connected thereto relative to the fixed hydraulic element, integral with the body. The displacement of the mobile power distribution member in its jacket then communicates a set of drilled channels and lights whose arrangement allows to deliver a pressure or a flow, proportional to the displacement of said movable power distribution member.
    Such a servovalve is currently connected to a hydraulic actuator, such as an aircraft wing flap actuator, to form a control device for this actuator.
    For the particularly critical functions of an aircraft such as flight controls or braking circuits, it is common to have a second set of coils in the torque motor in parallel with the first so that the second set of coils take the relay in case of failure (short-circuit or open circuit) of the first set of coils. This obeys the principle of dependability by parallel redundancy of the systems.
    Such a servovalve requires a magnetic circuit and charged permanent magnets, which increases the complexity of the assembly and the dispersion of the performances. Indeed, the performance of such a servovalve is sensitive to variations in the magnetic properties of the materials used in the magnetic circuit. Finally, it is necessary, during the construction of such a servovalve, to provide a step of adjusting the magnetization of the permanent magnets.
    OBJECT OF THE INVENTION The object of the invention is to simplify the manufacturing operations of a servovalve and to reduce its dispersion of performance.
    SUMMARY OF THE INVENTION
    In order to achieve this goal, a servovalve control stage is proposed, the control stage comprising a hydraulic element for ejecting a jet of fluid and a hydraulic element for receiving the jet of fluid, the hydraulic elements being movable. relative to each other so as to modify their relative position and thus generate a pressure differential, one of the two hydraulic elements being fixedly mounted on a body of the servovalve and the other of the hydraulic elements being secured a movable element of the driving stage displaceable relative to a body of the servovalve by actuating means. According to the invention, the actuating means comprise a first and a second piezoelectric actuator connected in series.
    Advantageously, the maximum elongation of the first piezoelectric actuator is substantially equal to half of the maximum elongation of the second piezoelectric actuator. This particular arrangement allows the first stage to return to a safe position in all fault configurations. The invention also includes a hydraulic actuator control device comprising such a servovalve and a control unit in which the control unit selectively adopts a control configuration from among a plurality of control configurations, the plurality of control configurations. comprising a first so-called normal command configuration and a second so-called degraded command configuration, - in the normal configuration, the control unit supplies at least the first actuator; in the degraded configuration, the control unit supplies at least the second actuator. Other features and advantages of the invention will emerge in the light of the following description of particular non-limiting embodiments of the invention.
    BRIEF DESCRIPTION OF THE FIGURES
    Reference is made to the appended figures among which: FIG. 1 is a diagrammatic representation of a servovalve comprising a first stage according to the invention; FIG. 2 is a schematic view of the actuating means according to the invention; FIG. 3 is a partial schematic view of the first stage of the servo valve of FIG. 1 in a first particular position of a first control configuration; FIG. 4 is a partial schematic view of the first stage of the servo valve of FIG. 1 in a second particular position of a first control configuration; FIG. 5 is a partial schematic view of the first stage of the servo valve of FIG. 1 in a second particular position of a first control configuration; - Figures 6 and 7 are partial schematic views of the first stage of the servovalve of Figure 1 in particular positions of a second control configuration; - Figure 8 is a partial schematic view of the first stage of the servovalve of Figure 1 in particular positions of a third control configuration.
    DETAILED DESCRIPTION OF THE INVENTION
    With reference to FIG. 1, the invention is here illustrated in application to a two-stage barometric flow control servovalve including a control stage. Of course, the invention is not limited to this application, and may be used for other types of servovalves.
    The servovalve generally designated 100 comprises a body 1 in which a power distribution member 2 is mounted to slide sealingly in a cylindrical housing 3 forming the distribution stage. The power distribution member 2 is movable between two extreme positions and is shaped to define in the housing 3 of the sealed chambers C1, C2, C3, C4 and C5 and to put in communication respectively, according to the position of the organ of power distribution 2 with respect to a centered position (or neutral position): either a power supply port P with a first use port Ul, and a return port R with a second usage port U2; either the power supply port P with the second usage port U2, and the return port R with the first usage port Ul.
    The sliding control of the power distribution member 2 in the housing 3 is ensured by means of control chambers 4,5 which are fed with fluid under pressure by a pressure distribution member, in this case a receiver 6 fixed. The receiver 6 comprises two orifices 7 and 8 respectively in fluid communication, via conduits 10 and 11, with the control chambers 4 and 5. A receptacle 9 located substantially vertically above the receiver 6 collects the hydraulic fluid when the latter is directed towards none of the orifices 7 or 8. The receptacle 9 is connected to the return R by a conduit 12. A LVDT type linear sensor 13 measures the position of the mobile power distribution member 2 in its housing 3. The core 14 of the sensor 13 is connected to the movable power distribution member 2 by a rod passing through one end of the cylindrical housing 3. The piloting stage 20 of the servovalve 1 comprises a movable element 21 which comprises a first portion 22 of rectangular section and a second portion 23 tubular projecting orthogonal projection of the middle of the portion 22.
    The first and second portions 22 and 23 form a moving assembly 21 having substantially a T-shaped section. A first end 22.1 of the first portion 21 is articulated by an axis 24 on the body 1 of the servovalve 100. The other end 22.2 opposite the end 21.1 rests on actuating means 40 extending in a direction substantially perpendicular to a longitudinal axis (X) of the first portion 22. The second tubular portion 23 is fluidly connected to the power port P by a conduit 36 and comprises at its end 23.1 a fluid ejector 30 for ejecting a jet of fluid to the orifices 7 or 8 according to the relative position of the ejector 30 and the orifices 7 and 8.
    The actuating means 40 comprise a first piezoelectric actuator 41 and a second piezoelectric actuator 42 connected in series, as shown in FIG. 2. A metal cover 43 extends around the first and second actuators 41 and 42 and comprises a bellows. elastic 44 which makes it possible to subject the first and second actuators 41 and 42 to the same preload. For the purposes of the present application, two actuators are connected in series when they are arranged in such a way that their respective elongations add up.
    The first actuator 41 and the second actuator 42 are respectively connected to a control unit 45 by a first cable 46 and a second cable 47. The control unit 45 is arranged to power the first and second actuators 41 and 42. A module 48, known to those skilled in the art, monitors the operation of the first and second actuators 41 and 42 and informs the control unit 45 of the operating state of the first and second actuators 41 and 42 via a cable 49. The assembly formed by the servovalve 100 and the control unit 45 then constitutes a control device for a hydraulic actuator 500 for controlling a wing flap of an aircraft connected to the utilization ports U1 and U2. The control unit 45 is itself connected to a regulator 50 PID receiving an error signal coming from the difference between the setpoint exerted on a control drive 51 and a measurement of the position of the power distribution member 2 transmitted by the sensor 13 whose signal is previously processed by a conditioner 52.
    According to the setpoint applied to the control 51 and the information supplied to the regulator 50, an instruction is sent to the control unit 45. This applies a pair of voltages across the first and second actuators 41 and 42. The elongations Ά41 and A42 respectively actuators 41 and 42 are proportional to the voltages applied thereto. The total elongation A40 of the actuating means 40, which is equal to the sum of the elongations A41 and A42 of the actuators 41 and 42, causes a displacement of the ejector 30 opposite the orifices 7 and 8 of the receiver 6. The differential created pressure causes the displacement of the mobile power distribution member 2 and thus a change in the output pressures of the U1 and U2 use ports. The pressing torque U1 and U2 causes a displacement of the hydraulic actuator 500.
    In the present case, the first and second actuators 41 and 42 respectively have a maximum elongation Amax41 and Amax42. Here, the maximum elongation Amax41 = 5 of the first actuator 41 is substantially equal to half of the maximum elongation Amax42 = 25 of the second actuator 42. As a reminder, two types of failures can affect a piezoelectric actuator. Either it is short-circuited, this is usually due to an internal fault. Either it is open circuit, which can occur in case of failure of the connector to which it is connected. When a piezoelectric actuator is in short circuit, it discharges and resumes its initial length which corresponds to a zero voltage applied to its terminals. When a piezoelectric actuator is in open circuit, it retains its length and returns very slowly to its initial length in a time generally greater than one hour.
    Figures 3 to 8 show some particular control configurations that may be adopted by the control unit 45 and the state of the first and second actuators 41 and 42 subjected to these particular control configurations. In these figures, the elongations of the first and second actuators are represented in the form of blackened portions.
    In a first control configuration, called normal, the control unit 45 applies the following voltages to the actuators: - first actuator 41 supplied with a variable voltage which is a function of the setpoint applied to the control 51, possibly corrected by the regulator 50 ; second actuator 42 supplied with a constant voltage corresponding to an elongation A42 of the second actuator 42 equal to Amax42 / 2.
    In the normal control configuration the elongation A40 of the actuating means 40 is therefore equal to A40 = (Amax42 / 2) + Α41 = δ + Α41 and the end of the actuating means 40 can be positioned in a range of extension of the actuating means 40 in the range [δ; 2d]. In this configuration, the ejector 30 faces the orifice 7 (FIG. 3) of the receiver 6 when the elongation A41 of the first actuator 41 is zero (Α40 = δ). The differential pressure thus created between the control chambers 4 and 5 causes a displacement of the power distribution member 2 in its housing 3 to the right according to the representation of Figure 1 (increase of the volume of the control chamber 4 ).
    When the voltage applied across the first neural action 41 by the control unit 45 is equal to half of the applicable maximum voltage, the elongation of the first actuator 41 is equal to half of its maximum elongation and the elongation A40 of the actuating means 40 is A40 = (Amax42 / 2) + (Amax41 / 2) = 1.55. The ejector 30 is then located between the two orifices 7 and 8 of the receiver 6 and no pressure differential is created between the control chambers 4 and 5 (Figure 4). The power distribution member 2 remains immobile.
    When the voltage applied across the first actuator 41 by the control unit 45 is equal to the applicable maximum voltage, the elongation A41 of the first actuator 41 is equal to its maximum elongation Amax41 = 5 and the elongation A40 of the actuating means 40 is A40 = (Amax42 / 2) + Amax41 = 25. The ejector 30 faces the orifice 8 (FIG. 5) of the receiver 6. The pressure differential thus created between the control chambers 4 and 5 causes a displacement of the power distribution member 2 in its housing 3 towards the right according to the representation of Figure 1 (increase of the volume of the control chamber 4). In this normal control configuration, the first actuator 41 can also adopt a plurality of elongation values A41 which correspond to as many possible setpoints applied to the control 51.
    A second control configuration, called degraded, is implemented in the event of detection of a failure of the first actuator 41 by the monitoring module 48. In this configuration, the control unit 45 supplies the second actuator 42 to vary its elongation between 0 and Amax42 = 25 depending on the type of failure of the first actuator.
    If the first actuator is in open circuit with a value of its elongation between 0 and Amax41 = 5 (FIGS. 6a-6b) or short-circuited with an elongation equal to 0 (FIGS. 7a-7b), the control unit 45 can apply a voltage across the second actuator 42 allowing an elongation thereof between 0 and 25. In this degraded configuration, the actuating means 40 are still able to cover an elongation range equal to [5 ; 25] and thus to answer the instructions applied on the command 51.
    In case of detection of a failure of the second actuator 42, when it is in open circuit with a value of its elongation equal to 5, the operation is identical to that of the normal configuration, until the elongation the second actuator 42 becomes less than 5 (Figure 8a). A third, so-called security configuration is then implemented when the second actuator 42 has an elongation of less than 5. In this configuration, it is no longer possible for the actuating means 40 to cover the elongation range of [5; 25] and the first actuator 41 is then energized to reach a maximum elongation Amax41 = 5 so that the receiver 30 is at least partially facing the orifice 7 of the receiver 6 (Figure 8b). In this conservative configuration, the servovalve 100 adopts its safety position, namely a drawer abutting on one side (here the drawer 2 is in abutment against the right wall of the housing 3 according to the representation of Figure 1) and therefore a maximum flow between U1 and U2. This case is obtained in normal operation for a minimum setpoint of the servovalve 1. The safety position of the servovalve 1 is therefore very different from the hydraulic zero of the servovalve 1 which corresponds to a zero flow between U1 and U2.
    There is thus obtained a control device of a hydraulic actuator 500 comprising a first and a second piezoelectric actuator 41 and 42 redundant connected in series. The use of piezoelectric actuators intrinsically improves reliability because they are robust actuators and have lower failure rates than coils. For the same application of displacement of a fluid ejector facing a receiver, the piezoelectric actuators of the invention have a mass and a small footprint compared to the solutions of the prior art implementing coils. The invention is of course not limited to what has just been described, but encompasses any variant within the scope defined by the claims.
    In particular, although here the core of the LVDT sensor is connected to the mobile power distribution member by a rod passing through one of the ends of the cylindrical housing, the invention also applies to other means of detecting the position of the slide, such as other types of passive or active position sensors: resistive, capacitive, or optical for example; - Although here the mobile element is T-shaped, one end is articulated on the body of the servo valve, the invention also applies to other types of moving elements, such as an element mobile L-shaped member, a movable member extending in a single longitudinal direction, or a movable member of any shape. The movable element can be hinged to the body, mounted floating or recessed on the body, as the portion carrying one of the hydraulic elements is able to be displaced relative to the other hydraulic element under the action of the actuator; although here the movable element comprises a tubular portion that fluidly connects the supply port to the fluid ejector, the invention also applies to other types of fluid supply such as a power supply. by hose or by an external duct attached to the rod; - Although here the actuating means comprises a first and a second piezoelectric actuator, the invention is also applicable to other actuating means that can contain more than two piezoelectric actuators; although here a metal hood comprising an elastic bellows extends around the first and second piezoelectric actuator, the invention also applies to other means for precharging the first and second piezoelectric actuators, such as for example an elastic element. mounted at one end of the first or second piezoelectric actuators, the cover may also be in another material such as an elastomer; - although here the ratio a between the maximum elongation of the first and second piezoelectric actuator is substantially equal to 2 (the maximum elongation of the first actuator is substantially equal to half the maximum elongation of the second actuator), The invention also applies to other values of the ratio a between the maximum elongations of the first and second actuators. For example, if the compactness of the actuator is preferred over its ability to retain the full performance after a failure of the first piezoelectric actuator, the ratio may be between one and two and thus guarantee a return to the safety position. . If, on the other hand, the reliability of the actuating means is preferred, the ratio a may be chosen greater than two, which makes it possible to reduce the control voltage applied to the second piezoelectric actuator and thus reduce its level of stress and fatigue; although here the actuator is connected to a PID regulator, the invention is also applicable to other types of regulator, for example pure proportional regulators or pure derivative or proportional derivative regulators; although here the fixed hydraulic element is a fluid receiver and the element mounted at the end of the rod is a fluid emitter, the invention also applies to a fluid emitter fixed on a body of fluid. the servovalve and a fluid receiver, such as a deflector or a pallet, mounted on the movable element; - Although here the supply pressure is delivered to the chambers C4 and C1 and the C5 chamber is put back, the invention also applies to a power stage in which these supplies would be reversed; -but here the servovalve is a two-stage servovalve comprising a power stage comprising a power distribution member whose position modification is controlled by the pressure differential generated by the first stage, the invention applies also to a single-stage servovalve in which the pressure differential is directly used to control an actuator or a hydraulic load; - Although here the control unit exclusively powers the second actuator in the degraded control configuration, the invention also applies to a degraded control configuration in which the control unit continues to supply the first piezoelectric actuator; - although here the control unit exclusively powers the first actuator in the safety control configuration, the invention also applies to a safety control configuration in which the control unit continues to supply the second actuator piezoelectric; - although here the control unit, in the safety control configuration, supplies the first actuator so that it reaches its maximum elongation, the invention also applies to a safety control configuration in which control unit feeds the first piezoelectric actuator so that the fluid ejector is permanently facing the orifice 7, regardless of the elongation of the second actuator; -but that here the maintenance of the movable element in a position such that the servo valve is in its safety position is ensured by the power supply of the piezoelectric actuators, the invention also applies to a holding in the safety position of the movable element so that the servovalve is in the safety position by other means such as for example an automatic return (by its own elasticity or otherwise) of the movable element in the safety position or a stop now the movable element in the safety position; although here the servovalve and the control unit 45 control a hydraulic actuator for controlling a wing flap of an aircraft, the invention also applies to the control of other types of actuators, as for example hydraulic actuators for braking, direction of inclination of blades.
    权利要求:
    Claims (11)
    [1" id="c-fr-0001]
    1. Control stage (20) of a servovalve (100), the control stage (20) comprising a hydraulic element (30) for ejecting a jet of fluid and a hydraulic element (6) for receiving the jet of fluid the hydraulic elements (30, 6) being movable relative to each other so as to modify their relative position and thereby generate a pressure differential, one of the two hydraulic elements (6) being fixed mounted on a body (1) of the servovalve (100) and the other of the hydraulic elements (30) being integral with a movable element (21) of the driving stage (20) displaceable relative to a body of the servovalve (100) by actuating means (40), characterized in that the actuating means (40) comprises a first piezoelectric actuator (41) and a second piezoelectric actuator (42) connected in series.
    [2" id="c-fr-0002]
    2. Control stage (20) according to claim 1, wherein the fixed hydraulic element is a fluid receiver (6) and the hydraulic element integral with the movable element (21) is a fluid ejector (30) .
    [3" id="c-fr-0003]
    3. Control stage (20) according to one of the preceding claims, wherein the actuating means (40) comprise a cover (43) extending around the first and second piezoelectric actuators (41; 42), the hood (43) comprising precharging means (44) for the first and second piezoelectric actuators (41; 42).
    [4" id="c-fr-0004]
    Pilot stage (20) according to claim 3, wherein the precharging means (44) comprise an elastic bellows (44).
    [5" id="c-fr-0005]
    5. Control stage (20) according to one of the preceding claims, wherein the maximum elongation (Amax41) of the first piezoelectric actuator (41) is substantially equal to half of the maximum elongation (Amax42) of the second piezoelectric actuator (42).
    [6" id="c-fr-0006]
    A control device of a hydraulic actuator (500) comprising a servovalve (100) having a control stage (20) according to claim 5 and a control unit (45), the control unit (45) selectively adopting a control configuration of a plurality of control configurations, the plurality of control configurations comprising a first so-called normal control configuration and a second degraded control configuration, - in the normal configuration, the control unit (45) powers at least the first piezoelectric actuator (41); in the degraded configuration, the control unit (45) supplies at least the second piezoelectric actuator (42).
    [7" id="c-fr-0007]
    The apparatus of claim 6 wherein in the normal configuration the control unit (45) powers the first and second piezoelectric actuators (41; 42).
    [8" id="c-fr-0008]
    8. Device according to one of claims 6 or 7, wherein in the degraded configuration, the control unit (45) supplies only the second piezoelectric actuator (42).
    [9" id="c-fr-0009]
    Apparatus according to any one of claims 6 to 8, wherein the plurality of control configurations comprises a third so-called safety control configuration, in which only one of the piezoelectric actuators (41; 42) is energized.
    [10" id="c-fr-0010]
    10. Device according to claim 9, wherein, in the safety configuration, only the first piezoelectric actuator (41) is powered.
    [11" id="c-fr-0011]
    11. Device according to any one of claims 6 to 10, wherein: in the normal configuration, the control unit (45) supplies the second piezoelectric actuator (42) so that it extends at half of its maximum elongation (Amax42) regardless of the supply voltage of the first piezoelectric actuator (41); - In the degraded configuration, the control unit (45) supplies the second piezoelectric actuator (42) so that it extends beyond half of its maximum elongation (Amax42).
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    同族专利:
    公开号 | 公开日
    ES2716157T3|2019-06-10|
    EP3242041B1|2019-01-02|
    EP3242041A1|2017-11-08|
    FR3051026B1|2019-06-07|
    US10651364B2|2020-05-12|
    US20170324021A1|2017-11-09|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    EP0012743A1|1978-12-18|1980-06-25|United Technologies Corporation|Piezoelectric control valve|
    EP0504465A1|1991-03-21|1992-09-23|MOOG GmbH|Fluid transducer with piezo-electric actuator|
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    FR3051027B1|2016-05-03|2019-06-14|Zodiac Hydraulics|SERVOVALVE PILOTAGE STAGE, WHICH CAN SERVE AS A FIRST FLOOR IN A SERVOVALVE WITH TWO FLOORS.|EP3412921A1|2017-06-05|2018-12-12|Hamilton Sundstrand Corporation|Servovalve assembly|
    EP3418586B1|2017-06-24|2021-12-08|Hamilton Sundstrand Corporation|Servovalve|
    EP3587831A1|2018-06-25|2020-01-01|Microtecnica S.r.l.|Hydraulic stage|
    法律状态:
    2017-05-23| PLFP| Fee payment|Year of fee payment: 2 |
    2017-11-10| PLSC| Search report ready|Effective date: 20171110 |
    2018-05-22| PLFP| Fee payment|Year of fee payment: 3 |
    2019-05-23| PLFP| Fee payment|Year of fee payment: 4 |
    2020-04-22| PLFP| Fee payment|Year of fee payment: 5 |
    2021-04-16| CD| Change of name or company name|Owner name: SAFRAN AEROSYSTEMS HYDRAULICS, FR Effective date: 20210308 |
    2021-04-21| PLFP| Fee payment|Year of fee payment: 6 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1653985|2016-05-03|
    FR1653985A|FR3051026B1|2016-05-03|2016-05-03|SERVOVALVE WITH ASYMMETRICALLY REDUNDANT PIEZO ELECTRIC ACTUATOR.|FR1653985A| FR3051026B1|2016-05-03|2016-05-03|SERVOVALVE WITH ASYMMETRICALLY REDUNDANT PIEZO ELECTRIC ACTUATOR.|
    EP17168612.4A| EP3242041B1|2016-05-03|2017-04-28|Servo valve with asymmetric redundant piezoelectric actuator|
    ES17168612T| ES2716157T3|2016-05-03|2017-04-28|Asymmetric redundant piezoelectric actuator servo valve|
    US15/585,825| US10651364B2|2016-05-03|2017-05-03|Servo valve with asymmetrical redundant piezoelectric actuator|
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