• 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:
    The present invention relates to a lubrication device (1) with a double circuit of a mechanical system (3), said lubricating device (1) being provided with two independent lubrication circuits (10, 20) and a reservoir (2). common to both lubrication circuits (10,20), and containing a lubricating liquid. A first lubrication circuit (10) has two first suction points (16,17) of said lubricating liquid in said reservoir (2) and a second lubrication circuit (20) has a second suction point (27). said lubricating liquid located in said reservoir (2). The double-circuit lubrication device (1) has a passage detection means below a limiting height of said lubricating liquid in said reservoir (2) formed by a first high suction point (16) located at said limit height, said second suction point (27) being below said limit height and a first suction low point (17) being below said second suction point (27).
    公开号:FR3027998A1
    申请号:FR1402464
    申请日:2014-10-31
    公开日:2016-05-06
    发明作者:Jean Guy Harreau
    申请人:Airbus Helicopters SAS；
    IPC主号:
    专利说明:

    [0001] FIELD OF THE INVENTION The present invention relates to the field of lubrication of gearboxes, in particular gearboxes intended for an aircraft with rotating wing. The present invention relates to a method and an augmented reliability double circuit lubrication device of a mechanical system. This method and lubricating device are particularly suitable for lubricating a main power transmission gearbox of a rotary wing aircraft. A mechanical system generally comprises rotating elements, such as shafts and bearings, as well as power transmission and speed reduction or increase elements, such as pinions and / or gears. It is therefore essential for the proper functioning of the mechanical system to lubricate and cool these elements, for example with pressurized oil. This lubrication is generally provided by a lubrication circuit and its main functions are to limit the wear and the heating of these elements of the mechanical system and, consequently, to prolong the life of the mechanical system. Without such lubrication, the operation of the mechanical system can be quickly degraded, if not impossible. Following this lubrication of the mechanical system, the oil flowing in the lubrication circuit can sometimes be very hot and then cooled in a cooling circuit generally outside the mechanical system before being used again for the lubrication of the mechanical system. This cooling circuit comprises a heat exchanger, for example an oil / air heat exchanger. This cooling system outside the mechanical system is a vulnerable part of a lubrication system of this mechanical system with respect to leaks. Indeed, this cooling circuit comprises pipes, numerous connections and the heat exchanger. This cooling circuit is then subjected to thermal stresses, such as a significant difference between the temperature of the oil and the outside temperature, and to vibratory stresses generated by the mechanical system and / or a vehicle using this mechanical system. In addition, this cooling circuit is exposed outside the mechanical system. In particular when this mechanical system equips an aircraft, this cooling circuit is located outside the mechanical system of the aircraft, for example under a hood. It can however be exposed to shocks with birds or with ice for example. In fact, one or more leaks may occur at these connections and these pipes and at the level of the heat exchanger, these leaks being essentially caused by these vibratory and thermal stresses. Such leaks generally make it possible to still ensure lubrication of the mechanical system, but for a limited time. Indeed, the oil stored in the lubrication circuit, for example in a tank, can then be discharged entirely outside the lubrication circuit by these leaks. Such leaks may possibly be detected by a drop in the oil pressure in the lubrication circuit.
    [0002] Furthermore, a lubrication circuit also comprises a pressure generator such as a pump to supply oil to the lubrication circuit and thus to allow its circulation in the lubrication circuit. In the event of a failure of this pressure generator, the circulation of the oil is interrupted and, consequently, the lubrication of the mechanical system is also interrupted immediately. In case of loss of this lubrication, degradations can therefore appear quickly on the operation of the mechanical system. The consequence of such degradations occurring on a mechanical system equipping a motor vehicle for example is the immobilization of the vehicle immediately or after the depletion of the lubricating circuit oil. On the other hand, if this mechanical system constitutes a main power transmission gearbox of a rotary wing aircraft, such degradations of the lubrication circuit of the main power transmission gearbox may then have catastrophic consequences such that a landing gear emergency or even a crash of the aircraft. In order to overcome these consequences, a mechanical system may include a backup lubrication circuit. Such a backup lubrication circuit ensures, when the main lubrication circuit is out of service, at least a lubrication of the essential organs of the mechanical system to ensure the operation of this mechanical system. For safety, it is preferable that the aircraft operates at a reduced power level in order to limit the stresses of the mechanical system. This auxiliary lubrication circuit then makes it possible, when this mechanical system is for example a main gearbox of power of an aircraft, the operation of the mechanical system and, consequently, that of the aircraft, in order to reach a place landing. Such an emergency lubrication circuit thus improves the safety of the aircraft. A backup lubrication circuit may be provided in parallel with a main lubrication circuit as described in US8230835. Each lubrication circuit has its own pump, but uses the same oil tank. However, if this backup circuit can sufficiently lubricate a mechanical system in case of failure of the main circuit, it is in fact rarely used. In fact, this back-up circuit constitutes an embedded mass which is rarely functional. In addition, the areas of occurrence of leakage of the main lubrication circuit are frequently at the heat exchanger and its connections. In fact, in order to prevent such leaks also appearing on the emergency lubrication circuit, the emergency circuit does not include a heat exchanger. In this way, the oil flowing through the emergency circuit is not cooled. As a result, the back-up lubrication circuit can only be used for a limited period of time in order to prevent the oil from reaching a too high temperature. This backup circuit is generally operated automatically following a loss of pressure detected in the main circuit following a failure of the pump of this main circuit or a leak in this main circuit. This emergency lubrication circuit can also be started manually by an operator. In order to reduce the risk of a failure of the main lubrication circuit from the emergency circuit, the backup circuit is generally equipped with a "bypass" system whose principle is to close the circulation in the circuit lines. emergency when there is sufficient oil pressure in the main lubrication circuit. Thus, in case of leakage on the emergency lubrication circuit, it is no longer operational, but does not interfere with the operation of the main lubrication circuit. The disadvantage of the "bypass" system is that it leaves the possibility of a dormant failure on the emergency circuit, this fault being detected only when the emergency circuit is started. In this case, it is a major anomaly that can be critical on a rotary wing aircraft. For certain applications on rotary wing aircraft, the main power transmission does not have a proper back-up lubrication circuit, but two identical and independent lubrication circuits.
    [0003] Each lubrication circuit has its own pump and its own heat exchanger. However, the two lubrication circuits jointly use the same oil tank formed by the bottom of the main power transmission gearbox. In fact, in the event of leakage of one of the lubrication circuits, the bottom of the main power transmission box will, in a more or less long period, empty and cause the failure of the complete lubrication system. Some lubrication systems comprise an emergency reservoir, sometimes directly mounted inside the mechanical system to be lubricated as described in documents EP2505878 and FR2658577. This emergency tank is positioned above the essential organs to be lubricated and fed continuously by the lubrication circuit. The oil flows then by gravity and permanently from this relief tank on these essential organs. In fact, in case of failure of the lubrication circuit, this emergency tank is no longer supplied, but allows to ensure lubrication of these essential organs for a limited time corresponding to the depletion of the oil contained in this reservoir rescue. Moreover, the document US8459413 describes a different architecture that makes it possible to limit the effects of a leak present in an oil tank. This architecture does not have a backup circuit itself, but a pump generating a vacuum in the tank when a leak is detected in the tank. As a result, this depression makes it possible to limit the quantity of oil evacuated by this leak, thus increasing the operating time of the lubrication circuit despite the presence of this leak. However, the leak is still present and the operating life of the lubrication circuit is certainly increased, but remains limited until the depletion of the oil. The object of the present invention is therefore to propose a method and a device for lubricating a mechanical system making it possible to overcome the limitations mentioned above, allowing the lubrication of the mechanical system despite the presence of a failure on a circuit. lubrication, in particular without limiting the duration of this lubrication. According to the invention, a dual circuit lubrication process is intended for the lubrication of a mechanical system. This mechanical system comprises a reservoir in which the lubricating liquid is located. During this double circuit lubrication process: - the mechanical system is simultaneously lubricated by means of a first lubrication circuit and a second lubrication circuit by the lubricating liquid; level of the lubricating liquid 30 in the tank below a limiting height, - the circulation of the lubricating liquid in the first lubrication circuit is stopped, the pressure of the lubricating liquid is measured in the second lubrication circuit, and detecting a drop in the pressure of the lubricating liquid in the second lubrication circuit; - the circulation of the lubricating liquid in the first lubrication circuit is restored, and - the circulation of the lubricating liquid in the second lubrication circuit is stopped. This mechanical system comprises, for example, rotating elements and power transmission and reduction or speed increase elements which need to be lubricated and cooled by a lubricating liquid such as oil so that the mechanical system operates. effectively and sustainably. This mechanical system is for example a main gearbox of power of a rotary wing aircraft. In this case, the tank is generally constituted by a casing of this main power transmission gearbox. When a leak appears on one of the two lubrication circuits, a portion of the lubricating liquid is discharged by this leakage outside the lubrication device. As a result, the height of the lubricating liquid in the reservoir decreases. Subsequently, by detecting that the height of the lubricating liquid in the reservoir is less than a limit height, the presence of a leak on at least one of the two lubrication circuits is detected. According to a first embodiment of the method according to the invention, the lowering of the level of the lubricating liquid below the limit height in the tank is detected by detecting a drop in the pressure of the lubricating liquid in the first lubrication circuit. for example by means of a first pressure sensor that includes the first lubrication circuit. Indeed, if a first high suction point of the first lubrication circuit is located in the reservoir at the limit height, the suction and, consequently, the circulation, of the lubricating liquid in this first lubrication circuit is impossible when the height of the lubricating liquid in the tank is less than the limit height. As a result, the pressure of the lubricating liquid in this first lubrication circuit drops. According to a second embodiment of the method according to the invention, the decrease in the level of the lubricating liquid below the limit height in the reservoir is detected directly by means of a liquid presence sensor located in the reservoir at height limit level. Indeed, a liquid presence sensor positioned in the tank at the height limit can detect that the height of the lubricating liquid in the tank is either less than the limit height, or greater than or equal to this limit height. In this second embodiment, the first suction point of the first lubrication circuit is positioned in the reservoir below the limit height. Preferably this first suction point is located in the bottom of the tank. This detection of the lowering of the level of the lubricating liquid below the limit height makes it possible to determine the presence of a leak on one of the two lubrication circuits without determining on which circuit exactly this leak is located. For this purpose, the method according to the invention then makes it possible to determine the defective lubrication circuit by successively controlling the two lubrication circuits. Following this detection of the lowering of the level of the lubricating liquid below the limit height, it stops first the circulation of the lubricating liquid in the first lubrication circuit to test the operation of the second lubrication circuit. With regard to the first embodiment of this method according to the invention, the lowering of the level of the lubricating liquid below the first high point of aspiration normally leads to the defusing of a first pump and, consequently, to stopping the pump. circulation of the lubricating liquid in the first lubrication circuit. This first pump has the function of drawing the lubricating liquid in the tank and increasing its pressure so that the lubricating liquid flows in the first lubrication circuit. However, when the mechanical system equips a rotary wing aircraft, the attitude of the aircraft can vary during a flight and especially during turns. The first high suction point may then be temporarily below the level of the lubricating liquid in the reservoir despite the lowering of this level of the lubricating liquid below the limit height, causing the first pump to be rebooted and consequently , again the circulation of the lubricating liquid in the first lubrication circuit. The first pump will be defused again and the circulation of the lubricating liquid stopped in the first lubrication circuit as soon as the aircraft has taken a substantially zero attitude, that is to say substantially horizontal, the first high point of suction is then again above the level of the lubricating liquid in the tank.
    [0004] In order to avoid these recoveries and untimely stops of the circulation of the lubricating liquid in the first lubrication circuit, it can therefore be useful, even necessary, to completely stop this circulation of the lubricating liquid in the first lubrication circuit. Indeed, these unwanted reinstatements of the circulation of the lubricating liquid in the first lubrication circuit are to be avoided because they can, if the detected leakage is on this first lubrication circuit, contribute to emptying a part of the lubricating liquid lying in the tank. By cons, for the second embodiment of this method according to the invention, the first suction point of the first lubrication circuit being positioned below the limit height, there is no break in the supply of the first pump by the lubricating liquid and the circulation of the lubricating liquid in the first lubrication circuit is not stopped by the lowering of the level of the lubricating liquid below the limit height. It is therefore necessary to stop the circulation of the lubricating liquid in the first lubrication circuit in order to avoid emptying the lubricating liquid in the reservoir. The circulation of the lubricating liquid in the first lubrication circuit can be stopped by stopping the first pump included in the first lubrication circuit. For example, the first pump is an electric pump and the power supply of this first pump is cut off. The first pump can also be a mechanical pump driven by a gearbox and can then separate the first pump of the gearbox for example by means of a clutch means.
    [0005] It is also possible to stop the lubrication of the mechanical system by the first lubrication circuit without acting on this first pump but by means of a first valve that comprises the first lubrication circuit. Thus, this first valve is placed in a closed position cutting off any circulation of the lubricating liquid in the first lubrication circuit. This first valve in the closed position allows for example the circulation of the lubricating liquid between the reservoir and the first pump, but the lubricating liquid is then returned to the reservoir and can not then reach the first lubrication circuit. This closed position of the first valve advantageously makes it possible not to stop the first pump until it is certain that the failure is due to the first lubrication circuit. The control of this first valve in the closed position can be carried out automatically following the detection of the lowering of the level of the lubricating liquid below the limit height. The steering of this first valve in the closed position can also be carried out manually by an operator following the emission of a visual and / or audible alarm following the detection of the lowering of the level of the lubricating liquid below the height. limit. Then, the pressure of the lubricating liquid in the second lubrication circuit can be tested, for example, by means of a second pressure sensor in the second lubrication circuit. This second pressure sensor measures the pressure of the lubricating liquid in the second lubrication circuit.
    [0006] However, a pressure sensor does not necessarily detect a pressure drop following a leak present on a lubrication circuit as the lubricating liquid flows under pressure in this lubrication circuit. Indeed, if it is a slow leak, the vacuum of the lubricating liquid generated by this slow leak is not detected by the pressure sensors generally used in a lubrication circuit. On the other hand, if the leakage is on this second lubrication circuit, the lubricating liquid circulating under pressure in this second lubrication circuit, a portion of the lubricating liquid continues to evacuate through this leak. In fact, the level of the lubricating liquid in the tank also drops. As a result, when the level of the lubricating liquid in the reservoir is below a second suction point of this second lubrication circuit, the lubricating liquid can no longer circulate in the second lubrication circuit. In fact, the pressure of the lubricating liquid in this second lubrication circuit drops as soon as the level of the lubricating liquid in the reservoir is below the second suction point of this second lubrication circuit. This second suction point must be in the reservoir at a position below the limit height in order to supply the second lubrication circuit with lubricating liquid after detecting that the height of the lubricating liquid in the reservoir is less than the height limit. By cons, the second suction point must not be in the tank bottom to avoid emptying the tank completely before detecting that the leak is on the second lubrication circuit.
    [0007] On the other hand, if no leakage is present in the second lubrication circuit, the level of the lubricating liquid in the reservoir does not change and the pressure of the lubricating liquid in this second lubrication circuit does not change either. It can then be deduced that the leakage is present in the first lubrication circuit. It is therefore necessary to maintain the circulation of the lubricating liquid only in this second lubrication circuit, the circulation of the lubricating liquid in the first lubrication circuit being stopped. It is then possible, if this had not been done previously, especially when using a first valve, to stop the first pump. Following the detection of a drop in the pressure of the lubricating liquid in the second lubrication circuit, the circulation of the lubricating liquid in the first lubrication circuit is restored and the circulation of the lubricating liquid in the second circuit is stopped. lubrication. As with the first lubrication circuit, lowering the level of the lubricating liquid below the second suction point normally causes the circulation of the lubricating liquid in the second lubrication circuit to be stopped, a second pump present on the second lubrication circuit being defused. This second pump has the function of drawing the lubricating liquid into the reservoir and increasing its pressure so that the lubricating liquid circulates in the second lubrication circuit. However, in order to avoid re-establishment and untimely stops of the circulation of the lubricating liquid in the second lubrication circuit in the case where the mechanical system equips a rotary wing aircraft, it may be useful, if not necessary, to stop completely this circulation of the lubricating liquid in the second lubrication circuit.
    [0008] It is then possible to stop the circulation of the lubricating liquid in the second lubrication circuit by stopping the second pump of the second lubrication circuit. As for the first pump, the second pump can be an electric pump or a mechanical pump driven by a gearbox. It is then possible, as the case may be, to cut off the power supply of the second pump or to separate the second pump from the transmission box by means of a clutch means. It is also possible to stop the circulation of the lubricating liquid in the second lubrication circuit without acting on this second pump, but by means of a second valve that comprises the second lubrication circuit. Thus, this second valve is placed in a closed position cutting off any circulation of the lubricating liquid in the second lubrication circuit. This second valve in the closed position allows for example the circulation of the lubricating liquid between the reservoir and the second pump, but the lubricating liquid is then returned to the reservoir and can not then reach the second lubrication circuit.
    [0009] The control of this second valve in the closed position can be carried out automatically following the detection of a drop in the pressure of the lubricating liquid in the second lubrication circuit. The piloting of this second valve in the closed position can also be carried out manually by an operator following the emission of a visual and / or audible alarm following the detection of the drop in the pressure of the lubricating liquid in the second circuit. lubrication. In addition to stopping the circulation of the lubricating liquid in the second lubrication circuit, the circulation of the lubricating liquid in the first lubrication circuit is restored in order to ensure the lubrication of the mechanical system by the first lubrication circuit. If the first pump of the first lubrication circuit has been previously stopped, this first pump is then restarted. According to the second embodiment of the method according to the invention, this restarting of the first pump is sufficient, the first suction point of the first lubrication circuit being positioned in the reservoir below the limit height. However, this first suction point must also be located below the second suction point to allow to supply lubricating liquid to the first lubrication circuit. On the other hand, according to the first embodiment of the method according to the invention, this restarting of the first pump is not sufficient. Indeed, according to this first embodiment, a first high suction point of the first lubrication circuit is located in the reservoir at the limit height. In fact, the first lubrication circuit must also include a first low suction point located in the tank below the second suction point and preferably in the bottom of the tank. The first lubrication circuit may have two first suction points and a first valve to tilt the first pump to the first suction point or the first suction point. This first valve allows by default that the first pump is in connection with the first high suction point. The control of this first valve so that the first pump is connected to the first low suction point can be performed automatically following the detection of a drop in the pressure of the lubricating liquid in the second lubrication circuit. The piloting of this first valve can also be carried out manually by an operator following the emission of a visual and / or audible alarm following the detection of the drop in the pressure of the lubricating liquid in the second lubrication circuit. Furthermore, this first valve may also include a closed position as mentioned above, this closed position cutting any circulation of the lubricating liquid in the first lubrication circuit.
    [0010] In addition, according to the first embodiment of the invention, the first lubrication circuit may comprise a single first suction point which is then movable. This first suction point can move vertically in the tank from a high position at the height limit to a low position located for example at the bottom of the tank. By default, this first mobile suction point is in the up position, thus constituting the first high suction point. Then, to restore the circulation of the lubricating liquid in the first lubrication circuit, it moves the first movable suction point in the lower position thus constituting the first low suction point. The displacement of the first suction point from the high position to the low position can be controlled automatically following detection of the drop in the pressure of the lubricating liquid in the second lubrication circuit. This movement can also be controlled manually by an operator following the emission of a visual and / or audible alarm following the detection of the drop in the pressure of the lubricating liquid in the second lubrication circuit. Stopping of the circulation of the lubricating liquid in the second lubrication circuit and the restoration of the circulation of the lubricating liquid in the first lubrication circuit can be carried out simultaneously or sequentially, stopping the second lubrication circuit. can be performed before or after the restoration of the first lubrication circuit.
    [0011] However, the restoration of the first lubrication circuit is preferably carried out before stopping the second lubrication circuit in order to minimize the time during which no lubrication of the mechanical system is ensured. In addition, after restoring the circulation of the lubricating liquid in the first lubrication circuit, the pressure of the lubricating liquid is measured in the first lubrication circuit. If this pressure of the lubricating liquid in the first lubrication circuit drops again, it means that a leak is also present on the first lubrication circuit or that the leak is in fact directly on the reservoir. The pressure of the lubricating liquid in this first lubrication circuit falls particularly as soon as the level of the lubricating liquid in the reservoir is below the first low point of suction of this first lubrication circuit. In this case, no lubrication of the mechanical system is ensured by one or the other of the lubrication circuits. On the other hand, after detecting the lowering of the level of the lubricating liquid below the limit height in the tank, the lubrication of the mechanical system is ensured only by a single lubrication circuit. In fact, the lubrication of the mechanical system is reduced. It is then necessary to reduce the stress of the mechanical system so as not to degrade this mechanical system, its operating level must be consistent with this reduced lubrication. For this purpose, an alarm, which may for example be visual and / or audible, is sent to an operator as soon as the level of the lubricating liquid in the tank is detected below the limit height. Thus, when the mechanical system is a main power transmission gearbox of a rotary wing aircraft, the load on this main power transmission gearbox must be reduced as soon as the level of the lubricating liquid is detected. below the limit height in the tank. For example, it reduces the speed of advance of the aircraft. The present invention also relates to a dual circuit lubrication device of a mechanical system. This lubrication device is provided with a reservoir and two independent lubrication circuits. The reservoir contains a lubricating liquid such as oil and is used jointly by the two lubrication circuits to lubricate the mechanical system. A first lubrication circuit comprises a first pump, first lines, a first pressure sensor, a first filter, a first heat exchanger, first nozzles and at least a first point of suction of the lubricating liquid, each first point of suction being located in the reservoir. The first pump distributes through a first suction point the lubricating liquid present in the reservoir in the first pipes and up to the first nozzles to lubricate the mechanical system.
    [0012] A second lubrication circuit comprises a second pump, second conduits, a second pressure sensor, a second filter, a second heat exchanger, second nozzles and a second suction point of the lubricating liquid, this second suction point. being located in the tank. The second pump distributes via the second suction point the lubricating liquid present in the reservoir in the second conduits and up to the second nozzles in order to lubricate the mechanical system.
    [0013] Thus, the two lubrication circuits make it possible to lubricate the mechanical system simultaneously. In addition, the first and second nozzles may be constituted by the same series of nozzles common to both lubrication circuits. Each lubrication circuit then comprises one or more non-return means, such as non-return valves, thus avoiding direct communication between the two lubrication circuits. This double circuit lubrication device is remarkable in that it comprises a passage detection means below the limit height of the liquid level of lubrication in the tank. In addition, the second suction point is below this limit height. The dual circuit lubrication device can then implement the previously described lubrication process.
    [0014] According to a first embodiment of the double circuit lubricating device according to the invention, the detection means is formed by a first high suction point and the first pressure sensor, this first high suction point being located at the the height limit.
    [0015] This first embodiment of this double circuit lubrication device can be broken down into several variants. According to a first variant of the first embodiment, the first lubrication circuit comprises two first suction points and a first two-position valve connecting the first pump with one or the other of these two first suction points. The first suction high point is located at the limit height and a first suction low point is located at a low position, below the limit height and also below the second suction point. Preferably, this first low suction point is located in the bottom of the tank. This first valve allows a circulation of the lubricating liquid is, in a first position between the first pump and the first high suction point, or, in a second position, between the first pump and the first low suction point. By default, this first valve is in the first position. The steering of this first valve to the second position is performed following a drop in the pressure of the lubricating liquid in the second lubrication circuit, this pressure drop being detected by the second pressure sensor. According to a second variant of the first embodiment, the first lubrication circuit comprises two first suction points and a first three-position valve connecting the first pump with one or the other of the first suction points so that the lubricating liquid circulates in the first lubrication circuit or interrupts this circulation of the lubricating liquid in the first lubrication circuit. As for the first variant, the first high suction point is located at the limit height and a first low suction point is located at a low position, below the limit height and also below the second point. suction. This first valve allows either, in a first position, a circulation of the lubricating liquid between the first pump and the first high suction point and in the first lubrication circuit, or, in a second closed position, no circulation of the liquid of lubricating in the first lubrication circuit, in a third position, a circulation of the lubricating liquid between the first pump and the first low suction point and in the first lubrication circuit. By default, this first valve is in the first position. The steering of this first valve to the second closed position is performed following a lower level of the lubricating liquid in the tank below the limit height detected by the detection means. The steering of this first valve to the third position is performed following a drop in the pressure of the lubricating liquid detected by the second pressure sensor in the second lubrication circuit. Furthermore, the lowering of the level of the lubricating liquid in the tank below the limit height is detected by means of the first pressure sensor that comprises the detection means. As a result, the control of this first valve to the second closed position is performed by this first pressure sensor. In fact, this second variant of the double circuit lubricating device according to the invention advantageously makes it possible to stop the circulation of the lubricating liquid in the first lubrication circuit as soon as a drop in the pressure of the lubricating liquid in the first circuit lubrication is detected by the first pressure sensor.
    [0016] This drop in the pressure of the lubricating liquid in the first lubrication circuit may be consecutive as previously mentioned to a drop in the level of the lubricating liquid in the reservoir below the limit height. This drop in the pressure of the lubricating liquid in the first lubrication circuit may also be caused by a significant leak on the first lubrication circuit, for example due to a clean break on a first pipe or at the first heat exchanger. Advantageously, this second variant thus makes it possible to stop the circulation of the lubricating liquid in the first lubrication circuit without waiting for the level of the lubricating liquid in the reservoir to drop below the limit height, thus making it possible to retain a quantity of liquid more lubrication in this tank. According to a third variant of the first embodiment of the invention, the first lubrication circuit comprises a single first suction point which is vertically movable in the reservoir. This first suction point is movable in the tank between the limit height and a low position at the bottom of the tank, that is to say below the limit height.
    [0017] This first suction point is positioned by default at the height limit to detect the lower level of the lubricating liquid in the tank below the limit height. Then, if it is proved that the leak detected by the detection means is on the second lubrication circuit, the first suction point moves in the reservoir to a low position to allow to feed the first circuit. lubricating fluid lubrication. This low position is located below the second suction point, and preferably in the bottom of the tank.
    [0018] This third variant advantageously makes it possible to use only one first suction point and to dispense with a first valve. In addition, the position of the first suction point being movable, the limit height can be adapted according to the amount of lubricating liquid actually present in the reservoir. According to a second embodiment of the double circuit lubricating device according to the invention, the detection means is formed by a liquid presence sensor positioned in the reservoir at the height limit. The first lubrication circuit then comprises a single first suction point located at a low position, below the limit height and also below the second suction point. Preferably, this first suction point is located in the bottom of the tank. According to this second embodiment, the first lubrication circuit may comprise a first two-position valve allowing the circulation of the lubricating liquid in the first lubrication circuit or cutting off this circulation. In fact, this first valve allows in either a first position, a circulation of the lubricating liquid between the first pump and the first suction point and in the first lubrication circuit, or in a second closed position, no circulation of the liquid of lubrication in the first lubrication circuit. By default, this first valve is in the first position. The steering of this first valve to the second closed position is performed following the detection of the lowering of the level of the lubricating liquid in the tank below the limit height.
    [0019] Moreover, a fourth variant is applicable to both embodiments of the double circuit lubrication device according to the invention. According to this fourth variant, the second lubrication circuit comprises a second valve with two positions allowing a circulation of the lubricating liquid between the second pump and the second suction point and then in the second lubrication circuit or cutting the circulation of the liquid of lubrication in the second lubrication circuit. This second valve thus allows in an open position to supply the second lubrication circuit with the lubricating liquid and in a closed position to stop the circulation of the lubricating liquid in the second lubrication circuit. By default, this second valve is in the open position. The steering of this second valve to the closed position is performed following a drop in the pressure of the lubricating liquid in the second lubrication circuit, this pressure drop being detected by the second pressure sensor. Furthermore, this drop in the pressure of the lubricating liquid in the second lubrication circuit may be consecutive to a drop in the level of the lubricating liquid in the reservoir below the position of the second suction point.
    [0020] This drop in the pressure of the lubricating liquid in the second lubrication circuit may also be caused by a significant leak on the second lubrication circuit, for example due to a clean break on a second pipe or at the level of the second heat exchanger. Advantageously, this fourth variant thus makes it possible to cut off the supply of the second lubrication circuit without waiting for the level of the lubricating liquid in the reservoir to drop below the position of the second suction point, thus making it possible to retain a quantity of liquid more lubrication in this tank.
    [0021] This double circuit lubrication device thus makes it possible to propose a global lubrication system for a mechanical system with increased reliability, this lubrication device consisting exclusively of two complete and independent lubrication subsystems, with the exception of one common lubricating liquid tank. In addition, this lubricating device avoids the complete failure of the lubrication of the mechanical system following the depletion of the lubricating liquid of the reservoir in the event of a slow leak, for example on a lubrication circuit, such a slow leak not being detectable. by pressure sensors. There is thus no limitation of the lubrication time following the detection of a leak on a lubrication circuit while ensuring cooling by at least one lubricating circuit of the lubricating liquid. In addition, the first and second pumps as well as the first and second valves may be located inside the mechanical system, for example above the tank. Advantageously, following a leak at a pump or a valve, the lubricating liquid flows into the tank, thus avoiding partially emptying the lubricating liquid from the tank. The present invention also relates to a main power transmission gearbox for a rotary wing aircraft. This main power transmission is provided with a double circuit lubrication device as previously described. The tank of the dual circuit lubrication device is constituted by a housing of the main power transmission gearbox.
    [0022] Advantageously, no emergency lubrication system, the use of which is very occasional and only in the event of failure of a main lubrication system and whose mass can then be penalizing, is not installed on the main transmission gearbox. . The invention and its advantages will appear in more detail in the context of the following description with examples given by way of illustration with reference to the appended figures which represent: FIGS. 1 to 3, variants of a first embodiment of the dual circuit lubricating device; - Fig. 4, a second embodiment of the dual circuit lubricating device; and - Fig. 5, a block diagram of a dual circuit lubrication process. The elements present in several separate figures are assigned a single reference. Double-circuit lubrication devices 1 shown in FIGS. 1 to 4 serve to lubricate a mechanical system 3 comprising in particular rotating elements 5, such as shafts and bearings, as well as power transmission elements and reducing or increasing speed 5, such as pinions and / or gears. This mechanical system 3 is for example a main power transmission gear equipping a rotary wing aircraft. Each double-circuit lubrication device 1 comprises a reservoir 2 and two lubrication circuits 10, 20 enabling the mechanical system 3 to be lubricated simultaneously. The reservoir 2 is formed by a housing of the mechanical system 3 and contains a lubricating liquid such as oil. Each lubrication circuit 10,20 comprises a pump 11,21, a pressure sensor 12,22, a heat exchanger 13,23, a filter 15,25, nozzles 14,24, at least one suction point 16, 17,27 and conduits respectively connecting the components of each lubrication circuit 10,20. The second lubrication circuit 20 comprises a single second suction point 27 while the first lubrication circuit 10 may comprise one or two first suction points 16, 17. The suction points 16, 17, 27 are located in the reservoir 2, the second suction point 27 being positioned at an intermediate position B in this reservoir 2. Each pump 11, 21 makes it possible to draw the lubricating liquid into the reservoir. tank 2 via a suction point 16,17,27 and distribute the lubricating liquid in each lubrication circuit 10,20. Each heat exchanger 13,23 is used to cool the lubricating liquid before it reaches the nozzles 14,24 by passing through the filters 15,25. The nozzles 14,24 are specific and distinct for each lubrication circuit 10,20, but can however be confused and common to the two lubrication circuits 10,20. According to a first variant of a first embodiment of the double-circuit lubrication device 1 shown in FIG. 1, the first lubrication circuit 10 comprises two first suction points 16, 17 and a first two-position valve 19. This first valve 19 makes it possible to connect the first pump 11 with one or other of these two first suction points 16, 17 in order to distribute the lubricating liquid in the first lubrication circuit 10. A first high point of suction 16 and a first low suction point 17 are respectively located at a high position A and at a low position C in this tank 2. The low position C is located at the bottom of the tank 2 and the intermediate position B is located between the high position A and the low position C. A second variant of the first embodiment of the double circuit lubricating device 1 shown in FIG. 2 differs from the first two-point variant. The first two-position valve 19 is replaced by a first three-position valve 19 connecting the first pump 11 with one or other of the first suction points 16, 17 so that the lubricating liquid circulates in the first stage. first lubricating circuit 10 or cutting the circulation of the lubricating liquid in the first lubrication circuit 10. This first valve 19 controls both the suction and the discharge of the first pump 11, a first secondary valve 19 'connected to the first valve 19 located at the discharge of the first pump 11. This first valve 19 thus allows, in a first position, to distribute the lubricating liquid in the first lubrication circuit 10 via the first high suction point. 16, in a second closed position, no circulation of the lubricating liquid in the first lubrication circuit 10, or in a third position , distributing the lubricating liquid in the first lubrication circuit 10 via the first low suction point 17. At the first secondary valve 19 ', the first and third positions put in communication the discharge of the first pump 11 with the first lubrication circuit 10 thus allowing the lubricating liquid coming out of the first pump 11 to reach the first spray nozzles 14. On the other hand, the second position of this first secondary valve 19 'puts in communication the discharge of the first pump 11 with a first return line 31 allowing the lubricating liquid leaving the first pump 11 to return to the tank 2. In addition, the second and third positions of the first valve 19 itself are connected to the first low point of suction 17 while the first position is connected to the first high suction point 16.
    [0023] These first and third positions of the first valve 19 of this second variant also correspond to the two positions of the first valve 19 of the first variant. By default, this first valve 19 is in the first position for the first and second variants.
    [0024] In addition, the second lubrication circuit 20 comprises a second valve 29 with two positions for connecting the second pump 21 to the second suction point 27 so that the lubricating liquid flows in the second lubrication circuit 20 or to cut the circulation of the lubricating liquid in the second lubrication circuit 20. By default, this second valve 29 is in an open position connecting the delivery of the second pump 21 to the second lubrication circuit 20 thus allowing the lubricating liquid coming out of the second pump 21 A closed position of this second valve 29 connects the discharge of the second pump 21 to a second return line 32 allowing the lubricating liquid leaving the second pump 21 to return to the tank 2. A third variant of the first embodiment of the double circuit lubrication device 1 is shown in FIG. This third variant differs from the first variant in the presence of a single first suction point 16 and the absence of a first valve 19. This first suction point 16 is movable in the tank 2 between the high position A and the low position C.
    [0025] In addition, the first and second pumps 11, 21 are located inside the mechanical system 3 and above the tank 2. In fact, following a leak at a pump 11, 21, the lubricating liquid is discharges into the reservoir 2, thus avoiding partially emptying the lubricating liquid from the reservoir 2. According to a second embodiment of the double circuit lubricating device shown in FIG. 4, the first lubrication circuit 10 comprises a single first point suction device 16, a liquid presence sensor 18 and a first two-position valve 19. This first valve 19 makes it possible to connect the first pump 11 to the first suction point 16 so that the lubricating liquid circulates in the first lubrication circuit 10 or to cut off this circulation of the lubricating liquid in the first lubrication circuit 10. The open position of this first valve 19 communicates the discharge of the first pump 11 with the first lubrication circuit 10 thus allowing the lubricating liquid coming out of the first pump 11 to reach the first spray nozzles 14. The closed position of this pump first valve 19 communicates the discharge of the first pump 11 with a first return line 31 allowing the lubricating liquid leaving the first pump 11 to return to the tank 2. The first suction point 16 is positioned in the reservoir 2 at the low position C. The liquid presence sensor 18 is located in the tank 2 at the position In addition, the second lubrication circuit 20 comprises a second valve 29 with two positions, this second valve 29 being identical to that of the second variant of the first embodiment of the double circuit lubrication device 1.
    [0026] The double-circuit lubrication devices 1 shown in FIGS. 1 to 4 are capable of implementing the lubrication method according to the invention, a block diagram of which is shown in FIG. 5. This lubrication process comprises several steps. During a first step 51, the mechanical system 3 is simultaneously lubricated via the first lubrication circuit 10 and the second lubrication circuit 20 by virtue of the lubricating liquid. The lubricating liquid is drawn by the first and second pumps 11,21 in the tank 2 and distributed respectively in the first and second lubrication circuits 10,20. The nozzles 14, 24 can then diffuse this lubricating liquid onto the mechanical system 3. In a second step 52, a decrease in the level of the lubricating liquid in the reservoir 2 is detected below a limit height intermediate of a passage detection means below this limit height of the level of the lubricating liquid in the reservoir 2. For the first embodiment of the double circuit lubrication device 1, the detection means is formed by the first high suction point 16 and the first pressure sensor 12. For the third variant, the first mobile suction point 16 must then be in the high position A. For the second embodiment of the lubricating device 1 to dual circuit, the detection means is formed by the liquid presence sensor 18. The high position A corresponds to the limit height in the tank 2 and the detection means allows determination reduce the level of the lubricating liquid below this limit. This lowering of the level of the lubricating liquid in the tank 2 below a limiting height means that the tank 2 is progressively emptied of the lubricating liquid and, consequently, that a leak has occurred on one of the lubrication circuits 10.20. For the first embodiment of the double circuit lubricating device 1, following this drop in the level of the lubricating liquid in the tank 2 below the limit height, the first high suction point 16, located at the up position A, is above the level of the lubricating liquid. In fact, the first pump 11 can no longer distribute the lubricating liquid in the first lubrication circuit 10. The pressure of the lubricating liquid therefore falls in this first lubrication circuit 10, this pressure drop being detected by the first sensor of pressure 12. For the second embodiment of the double circuit lubrication device 1, this lowering of the level of the lubricating liquid in the tank 2 below the limit height is detected directly by the liquid presence sensor 18.
    [0027] During a third step 53, the circulation of the lubricating liquid in the first lubrication circuit 10 is stopped in order to test the operation of the second lubrication circuit 20. In fact, the detection means makes it possible to determine the presence of a leak on a lubrication circuit 10,20, without identifying on which lubrication circuit 10,20 is actually this leak. As a result, by stopping the circulation of the lubricating liquid in the first lubrication circuit 10, the lubricating liquid circulates only in the second lubrication circuit 20.
    [0028] Since the lubricating liquid is below the limit height in the tank 2, the first pump 11 no longer makes it possible to supply the first lubrication circuit 10 for the first embodiment of the double circuit lubrication device 1. Consequently, the circulation of the lubricating liquid is stopped in this first circulation circuit 10. On the other hand, for the second embodiment of the double-circuit lubrication device 1, the only first suction point 16 is at the low position C, therefore below the limit height. It is therefore necessary to stop the circulation of the lubricating liquid in the first lubrication circuit 10 either by directly stopping the first pump 11, or by means of the first valve 19. This first valve 19 must then be put in the position closed to stop the circulation of the lubricating liquid in the first lubrication circuit 10. This setting in the closed position of the first valve 19 is controlled by the detection of the lowering of the level of the lubricating liquid in the tank 2 below the height limit and performed automatically. However, this setting in the closed position of the first valve 19 can also be performed manually by an operator following the emission of a visual and / or audible alarm following the detection of the lowering of the level of the lubricating liquid below the height limit. The first pump 11 can be stopped by cutting off its power supply when this first pump 11 is an electric pump. The first pump can also be stopped by means of a clutch means when the first pump 11 is a mechanical pump driven by a gearbox which may be the mechanical system 3.
    [0029] It is also possible according to a first specific stop mode, for the first embodiment of the double circuit lubrication device 1, to stop the circulation of the lubricating liquid in the first lubrication circuit 10 by stopping the first pump directly. 11. It is also possible according to a second specific stop mode, but only for the second variant of this first embodiment, to put the first valve 19 in the second closed position. These specific stopping modes make it possible to avoid unwanted restarts and stops of the circulation of the lubricating liquid in the first lubrication circuit 10, for example following agitation of the lubricating liquid in the reservoir 2 which may be consecutive to changes in the attitude of an aircraft equipped with this mechanical system 3. In a fourth step 54, the pressure of the lubricating liquid in the second lubrication circuit 20 is measured by means of the second pressure sensor 22 During a fifth step 55, the presence or absence of a drop in the pressure of the lubricating liquid in the second lubrication circuit 20 is detected. The pressure of the lubricating liquid in the second lubrication circuit 20 can drop. 20 either following a significant leak directly on this second lubrication circuit 20 or following a drop in the level of the lubricating liquid in the tank 2 below the second suction point 27. If no drop in the pressure of the lubricating liquid in the second lubrication circuit 20 is detected, it switches to a sixth step 56. It can then be concluded that the failure of the Lubricating device probably comes from the first lubrication circuit 10 which must contain a leak. This sixth step 56 then terminates the process, a first alarm 30 in the form of a first light signal and / or sound, informing an operator that the first lubrication circuit 10 probably has a leak, can then be sent. If a drop in the pressure of the lubricating liquid is detected in the second lubrication circuit 20, the process is continued to additional steps. This drop in the pressure of the lubricating liquid in the second lubrication circuit 20 probably confirms the presence of a leak on this second lubrication circuit 20. During a seventh step 57, the circulation of the lubricating liquid is restored in the first lubrication circuit 10 to allow lubrication of the mechanical system 3. For the first and second variants which have two first suction points 16,17, the first valve 19 must be tilted to the third position to connect the first pump 11 at the first low suction point 17. This third setting of the first valve 19 is controlled by the detection of the drop of the pressure of the lubricating liquid in the second lubrication circuit 20. For the third variant, the first movable suction point 16 must be lowered below the level of the lubricating liquid to allow the first pump of p uiser the lubricating liquid in the tank 2 and thereby supply the first lubrication circuit 10. This first mobile suction point 16 must be lowered at least below the intermediate position B and preferably at the low position C. In addition, for these three variants, if the first pump 19 has been stopped during the third step 53, it is necessary to restart this first pump 11.
    [0030] During an eighth step 58, the circulation of the lubricating liquid in the second lubrication circuit 20 is stopped. The lubricating liquid below the second suction point 27 in the reservoir 2, the second pump 21 allows more to feed the second lubrication circuit 20. As a result, the circulation of the lubricating liquid is stopped in this second lubrication circuit 20. On the other hand, it is also possible according to the first specific stop mode to stop the circulation of the lubricating liquid 10 in the second lubrication circuit 20 by directly stopping the second pump 21. It is also possible according to the second specific stop mode to put the second valve 19 in the closed position in order to cut the circulation of the liquid lubrication in the second lubrication circuit 20. This placing in the closed position 15 of the second valve 29 is controlled by the detection of the fall of the pressure of the lubricating liquid in the second lubrication circuit 20. The seventh and eighth steps can be performed sequentially or simultaneously. However, the seventh step is preferably performed before the eighth step to minimize the time during which no lubrication of the mechanical system 3 is ensured. During a ninth step 59, the pressure of the lubricating liquid is measured in the first lubrication circuit 10 via the first pressure sensor 12 to verify that no leakage is also present on the first Lubrication circuit 10. During a tenth step 60, the presence or absence of a drop in the pressure of the lubricating liquid in the first lubrication circuit 10 is detected. The pressure of the lubricating liquid in the first circuit lubricant 10 may drop either following a significant leak directly on the first lubrication circuit 10 or following a drop in the level of the lubricating liquid in the tank 2 below the first low suction point 17. If one detects no drop in the pressure of the lubricating liquid in the first lubrication circuit 10, it switches to an eleventh step 61. It can then be concluded that the failure of the device lubrication comes from the second lubrication circuit 20 which must contain a leak. This eleventh step 61 then terminates the process, a second alarm in the form of a second light signal and / or sound, informing an operator that the second lubrication circuit 20 probably has a leak, can then be sent.
    [0031] If a drop in the pressure of the lubricating liquid is detected in the first lubrication circuit 10, it switches to a twelfth step 62. This drop in the pressure of the lubricating liquid in the first lubrication circuit 10 reveals the presence of a leak also on this first lubrication circuit 10 or more likely that the leak is actually directly on the reservoir 2. This twelfth step 62 also terminates the process, a third alarm in the form of a third light signal and / or sound, informing an operator that the entire double circuit lubrication device 1 is faulty, can then be sent. In this case, no lubrication of the mechanical system 3 is ensured by the lubrication circuits 10 and 20. This double circuit lubrication device 1 thus makes it possible to propose a lubrication system of a mechanical system 3 with increased reliability, without the use of an emergency circuit, or of several reservoirs of lubricating liquid. In addition, this double circuit lubrication device 1 ensures a continuous cooling of the lubricating liquid and has no limitation of the lubrication time following the detection of a leak. Naturally, the present invention is subject to many variations as to its implementation. Although several embodiments have been described, it is well understood that it is not conceivable to exhaustively identify all the possible modes. It is of course conceivable to replace a means described by equivalent means without departing from the scope of the present invention.
    权利要求:
    Claims (20)
    [0001]
    REVENDICATIONS1. A dual-circuit lubrication process of a mechanical system (3), said mechanical system (3) having a reservoir (2) in which a lubricating liquid is located, in which said mechanical system (3) is simultaneously lubricated by via a first lubricating circuit (10) and a second lubricating circuit (20) by said lubricating liquid, - decreasing the level of said lubricating liquid in said reservoir (2) below a limiting height, - the circulation of said lubricating liquid in said first lubrication circuit (10) is stopped, - the pressure of said lubricating liquid is measured in said second lubrication circuit (20), - a fall of said lubricating liquid is detected. pressurizing said lubricating liquid in said second lubrication circuit (20), - circulating said lubricating liquid in said first lubrication circuit (10), and stopping circulation supplying said lubricating liquid to said second lubrication circuit (20).
    [0002]
    2. Lubrication method according to claim 1, characterized in that, said first lubrication circuit (10) comprising a first valve (19), said first valve (19) is piloted by said lowering of said level of said lubricating liquid in said tank (2) below said limit height and stopping said circulation of said lubricating liquid in said first lubrication circuit (10) through said first valve (19).
    [0003]
    3. Lubrication method according to any one of claims 1 to 2, characterized in that said first lubrication circuit (10) having a first valve (19), said first valve (19) is piloted by a detection of a lowering the pressure of said lubricating liquid in said second lubrication circuit (20) and returning said circulation of said lubricating liquid to said first lubrication circuit (10) through said first valve (19).
    [0004]
    The lubrication method according to claim 1, characterized in that, said first lubrication circuit (10) having a first pump (11), stopping said circulation of said lubricating liquid in said first lubrication circuit (10) by stopping said first pump (11) and said circulation of said lubricating liquid is restored in said first lubrication circuit (10) by restarting said first pump (11).
    [0005]
    A lubrication method according to any one of claims 1 to 4, characterized in that, said second lubrication circuit (20) comprising a second pump (21), stopping said circulation of said lubricating liquid in said second circuit of lubricating (20) by stopping said second pump (21).
    [0006]
    The lubrication method as claimed in any one of claims 1 to 4, characterized in that, said second lubrication circuit (20) comprising a second valve (29), said second valve (29) is piloted by a detection device. a pressure drop of said lubricating fluid in said second lubrication circuit (20) and stopping said circulation of said lubricating liquid in said second lubrication circuit (20) through said second valve (29).
    [0007]
    A lubrication method according to any one of claims 1 to 6, characterized in that said lowering of said level of said lubricating liquid below said limit height in said reservoir (2) is detected by detecting a fall of said pressurizing said lubricating liquid in said first lubrication circuit (10).
    [0008]
    8. Lubrication process according to any one of claims 1 to 6, characterized in that said lowering of said level of said lubricating liquid below said limit height in said reservoir (2) is detected by means of a liquid presence sensor (18) located in said reservoir (2) at said limit height.
    [0009]
    A lubrication method according to any one of claims 1 to 8, characterized in that, after detecting said drop of said pressure of said lubricating liquid in said second lubrication circuit (20), distributing said lubricating liquid in said first lubrication circuit (10) via a first suction point (17) located in said reservoir (2) below said limit height.
    [0010]
    Lubrication method according to any one of claims 1 to 9, characterized in that, after restoring said circulation of said lubricating liquid in said first lubrication circuit (10), the pressure of said lubricating liquid is measured in said first lubrication circuit (10).
    [0011]
    11. Double circuit lubrication device (1) of a mechanical system (3), said lubricating device (1) being provided with a reservoir (2) and two lubrication circuits (10, 20), said reservoir (2) containing a lubricating liquid, a first lubrication circuit (10) having a first pump (11), first lines, a first pressure sensor (12), first nozzles (14) and at least a first point suction (16,17) of said lubricating liquid, each first suction point (16,17) being located in said reservoir (2), a second lubrication circuit (20) having a second pump (21), second conduits, a second pressure sensor (22), second nozzles (24) and a second suction point (27) of said lubricating liquid, said second suction point (27) being located in said reservoir (2) , each pump (11,21) distributing via said first and second suction point (16,17,27) said lubricating liquid respectively in said first and second conduits, then in said first and second nozzles (14,24) for lubricating said mechanical system (3), characterized in that, said lubricating device (1) double circuit includes passage detection means below said limit height of said lubricating liquid in said reservoir (2), said second suction point (27) being located below said limit height, said device lubrication system (1) employing the lubrication process according to any of claims 1 to 10.
    [0012]
    Lubricating device (1) according to claim 11, characterized in that said first lubrication circuit (10) comprises two first suction points (16, 17) and a first valve (19) connecting said first pump (11). ) with said first two suction points (16,17), said detection means being formed by a first suction point (16) and said first pressure sensor (12), said first suction point ( 16) being located at said limit height and a first low suction point (17) being at a low position below said second suction point (27).
    [0013]
    13. Lubricating device (1) according to claim 12, characterized in that said first valve (19) is a two-position valve connecting said first pump (11) with one or the other of said first points. suction (16,17), said first valve (19) being controlled by said second pressure sensor (22).
    [0014]
    14. A lubricating device (1) according to claim 12, characterized in that said first valve (19) is a three-position valve allowing a circulation of said lubricating liquid between said first pump (11) and one or the another of said first suction points (16, 17) for said lubricating liquid to flow into said first lubrication circuit (10) or to cut off said circulation of the lubricating liquid in said first lubrication circuit (10), said first valve (19) being driven by said first pressure sensor (12) and said second pressure sensor (22).
    [0015]
    The lubricating device (1) according to claim 11, characterized in that said first lubrication circuit (10) comprises a single first movable suction point (16), said detecting means being formed by said first point of contact. suction (16) and said first pressure sensor (12), said first suction point (16) being movable in said reservoir (2) between said limit height and a low position below said second suction point (27). ).
    [0016]
    The lubricating device (1) according to claim 11, characterized in that said first lubrication circuit (10) comprises a single first suction point (16) and a liquid presence sensor (18), said means for sensing being formed by said liquid presence sensor (18) positioned in said reservoir (2) at said limit height, said first suction point (16) being located at a low position below said second point of suction (27).
    [0017]
    Lubricating device (1) according to claim 16, characterized in that said first lubrication circuit (10) comprises a first valve (19) with two positions allowing a circulation of said lubricating liquid between said first pump (11) and said first suction point (16) then in said first lubrication circuit (10) or cutting said circulation of said lubricating liquid in said first lubrication circuit (10), said first valve (19) being driven by said presence of liquid (18).
    [0018]
    The lubricating device (1) according to any one of claims 11 to 17, characterized in that said second lubrication circuit (20) comprises a second valve (29) with two positions allowing a circulation of said lubricating liquid between said second pump (21) and said second suction point (27) then in said second lubrication circuit (20) or cutting said circulation of said lubricating liquid in said second lubrication circuit (20), said second valve (29) being driven by said second pressure sensor (22).
    [0019]
    19. Lubricating device (1) according to any one of claims 11 to 18, characterized in that said mechanical system (3) is a main gearbox of power of a rotary wing aircraft.
    [0020]
    20. Main power transmission gearbox for a rotary wing aircraft, characterized in that said main power transmission gearbox is provided with a lubricating device (1) according to claim 19, said reservoir (2) consisting of by a casing of said main power transmission gearbox.
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    同族专利:
    公开号 | 公开日
    FR3027998B1|2017-08-25|
    US9732840B2|2017-08-15|
    EP3021030B1|2017-03-22|
    US20160123457A1|2016-05-05|
    EP3021030A1|2016-05-18|
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    US10746284B2|2015-04-21|2020-08-18|Sikorsky Aircraft Corporation|Gearbox lubrication system for aircraft|
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    JP6846301B2|2017-06-27|2021-03-24|川崎重工業株式会社|Power transmission device for helicopters|
    FR3074558B1|2017-12-05|2020-01-10|Airbus Helicopters|FLUIDIC SYSTEM FOR LUBRICATING AND / OR COOLING A MECHANICAL ASSEMBLY|
    US10816085B2|2018-01-18|2020-10-27|Bell Helicopter Textron Inc.|Aircraft lubrication system|
    FR3083283B1|2018-06-28|2021-12-24|Airbus Helicopters|LUBRICATION SYSTEM FOR AN AIRCRAFT MAIN POWER TRANSMISSION BOX WITH AN IMPROVED METAL PARTICLE CAPTURE AND DETECTION DEVICE|
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    法律状态:
    2015-10-23| PLFP| Fee payment|Year of fee payment: 2 |
    2016-05-06| PLSC| Search report ready|Effective date: 20160506 |
    2016-10-20| PLFP| Fee payment|Year of fee payment: 3 |
    2017-10-24| PLFP| Fee payment|Year of fee payment: 4 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1402464A|FR3027998B1|2014-10-31|2014-10-31|DUAL CIRCUIT RELIABLE LUBRICATION METHOD AND DEVICE OF A MAIN POWER TRANSMISSION BOX OF AN AIRCRAFT|FR1402464A| FR3027998B1|2014-10-31|2014-10-31|DUAL CIRCUIT RELIABLE LUBRICATION METHOD AND DEVICE OF A MAIN POWER TRANSMISSION BOX OF AN AIRCRAFT|
    EP15186183.8A| EP3021030B1|2014-10-31|2015-09-22|A dual circuit lubrication method and device with increased reliability for a main power transmission gearbox of an aircraft|
    US14/924,790| US9732840B2|2014-10-31|2015-10-28|Dual circuit lubrication method and device with increased reliability for a main power transmission gearbox of an aircraft|
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