• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
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  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention relates to a lubrication device (1) with a triple circuit of a mechanical system (3), said lubrication device (1) being provided with two independent lubrication circuits (10, 20), a reservoir (2 ) common to the two lubrication circuits (10,20) and containing a lubricating liquid and a tertiary circuit (30) in which circulates a tertiary liquid. Each lubrication circuit (10, 20) comprises pipes, a pressure sensor (12, 22), a pump (11, 21), a heat exchanger (13, 23), nozzles (14, 24) and a point suction (16,26) of said lubricating liquid located in said reservoir (2). Said second suction point (26) is located below said first high suction point (16). Said tertiary circuit (30) comprises a third pump (31), a third pressure sensor (32), said second heat exchanger (23) and a third heat exchanger (33) and thus makes it possible to cool the lubricating liquid flowing in said second lubrication circuit (20).
    公开号:FR3027992A1
    申请号:FR1402468
    申请日:2014-10-31
    公开日:2016-05-06
    发明作者:Damien Goujet
    申请人:Airbus Helicopters SAS；
    IPC主号:
    专利说明:

    [0001] Triple-circuit enhanced reliability lubrication device of a main gearbox of an aircraft. The present invention relates to the field of lubrication of gearboxes, particularly gearboxes for a rotary wing aircraft. The present invention relates to a lubrication device with increased reliability with a triple circuit of a mechanical system. This lubricating device is particularly adapted to the lubrication of a main gearbox 10 of a rotary wing aircraft. A mechanical system generally includes rotating members, 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 service 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 be 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. Furthermore, a lubrication circuit also comprises a pressure generator such as a pump for supplying the lubrication circuit with oil and thus allowing it to circulate 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.
    [0002] 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.
    [0003] A backup lubrication circuit can be set in parallel with a main lubrication circuit as described in US8230835. Each lubrication circuit has its own pump, but uses the same oil tank.
    [0004] 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 backup circuit is an embedded mass that is rarely functional.
    [0005] 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 appear 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 emergency lubrication circuit can only be used for a limited period of time in order to prevent the oil from reaching a too high temperature.
    [0006] 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 emergency circuit is generally equipped with a "bypass" system whose principle is to close the circulation in the lines of the circuit of 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. 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.
    [0007] Some lubrication systems include an emergency reservoir, sometimes directly mounted within the mechanical system to be lubricated as described in EP2505878 and US2007 / 0261922. 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.
    [0008] In addition, according to US2007 / 0261922, an additive may be added to the oil in this relief tank following the failure of the main lubrication circuit. This additive makes it possible to increase the characteristics of the oil thus improving its efficiency and the duration of operation of the emergency lubrication circuit formed by this emergency tank. Furthermore, US4717000 discloses a lubrication system for a turbine engine comprising an emergency reservoir supplied with oil by the lubrication system and used only in case of failure of the lubrication system. In addition, this emergency reservoir comprises a cylinder activated by the compressed air leaving a turbine engine compressor in order, following a failure of the lubrication system, to pressurize the oil stored in the emergency tank. Then, an oil-compressed air mixture is sprayed on essential organs of the turbine engine. The object of the present invention is therefore to provide a device for lubricating a mechanical system making it possible to overcome the abovementioned limitations, allowing the lubrication of the mechanical system despite the presence of a fault on a lubrication circuit, in particular without limitation of the duration of this lubrication. According to the invention, a triple-circuit lubrication device for lubricating a mechanical system 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 a first point of suction of the lubricating liquid, the first point of contact. suction being located in the tank. The first pump distributes through the first suction point the lubricating liquid present in the reservoir in the first pipes and up to the first sprinklers in order to lubricate the mechanical system. 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. 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.
    [0009] This triple circuit lubrication device is remarkable in that it comprises a tertiary circuit in which a tertiary liquid circulates. This tertiary circuit comprises a third pump, third pipes, a third pressure sensor, the second heat exchanger and a third heat exchanger.
    [0010] The third pump allows the circulation of the tertiary liquid in the third pipes, the second heat exchanger and the third heat exchanger. In addition, the second suction point is located below the first suction point in the reservoir.
    [0011] 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 of the triple circuit lubricating device is generally constituted by a casing of this main power transmission gearbox. The first heat exchanger of the first lubrication circuit is an air / liquid heat exchanger conventionally used in such a lubrication circuit. This air / liquid heat exchanger thus makes it possible to cool the lubrication liquid which has been heated by lubricating the mechanical system. This air / liquid heat exchanger uses for this air generally located near the mechanical system. The second heat exchanger of the second lubrication circuit is a liquid / liquid heat exchanger. This liquid / liquid heat exchanger thus makes it possible to cool the lubrication liquid which has been heated by lubricating the mechanical system. This liquid / liquid heat exchanger uses the tertiary liquid circulating in the tertiary circuit.
    [0012] The third heat exchanger of the tertiary circuit is an air / liquid heat exchanger such as those conventionally used in a lubrication circuit. This air / liquid heat exchanger thus makes it possible to cool the tertiary liquid which has been heated by passing through the second heat exchanger. This air / liquid heat exchanger uses air generally located near the mechanical system. This tertiary liquid is for example water, glycol or oil. In addition, the lubricating liquid flows in the first lubrication circuit with a first pressure P1 and in the second lubrication circuit with a second pressure P2. This first pressure P1 is obtained via the first pump and this second pressure P2 is obtained via the second pump. The tertiary liquid circulates in the tertiary circuit with a third pressure P3 obtained via the third pump. In addition, each pressure sensor makes it possible respectively to measure the pressure P1, P2, P3 of the liquid flowing in the first and second lubrication circuits as well as in the tertiary circuit. Each pressure sensor has the particular function of detecting a fall of this pressure P1, P2, P3. 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, such a pressure sensor can detect a drop in the pressure of the lubricating liquid in a lubrication circuit caused by a major leak on this lubrication circuit, following, for example, a clean rupture on a pipe or at the level of a heat exchanger. Thus, when a leak appears on the first lubrication circuit, this leak is not necessarily immediately detected by the first pressure sensor. By cons, this leak on the first lubrication circuit probably appears at the first heat exchanger or that of the pipes connected to the first heat exchanger. Part of the lubricating liquid is then discharged by this leak outside the triple circuit lubrication device according to the invention. As a result, the height of the lubricating liquid in the reservoir decreases. As a result, when the first suction point is above the level of the lubricating liquid in the tank, the first pump is defused and can no longer supply the first lubricating liquid lubrication circuit. Preferably, this first suction point is located in a high zone of the volume of lubricating liquid present in the reservoir to allow rapid detection of such a leak. This position of the first suction point is defined with a margin of safety in order to take into account a consumption of the lubricating liquid and to avoid untimely detections of a leak not present. This safety margin on the position of the first point of suction also takes into account the possible movements of the mechanical system which can generate a movement of the lubricating liquid in the reservoir and possibly the defusing of the first pump from where, consequently, a stop of the lubrication of the mechanical system. Such movements occur in particular when the mechanical system equips a rotary wing aircraft, its attitude may vary during a flight and in particular during some stationary flights. In fact, the position of the first suction point automatically stops the circulation of the lubricating liquid in the first lubrication circuit when a slow leak occurs on the first lubrication circuit. The mechanical system is then no longer lubricated by the first lubrication circuit. The mechanical system is then lubricated only by the second lubrication circuit. The second suction point must be positioned below the first suction point to allow the second lubrication circuit to be fed through the second pump despite the lowering of the level of the lubricating liquid in the reservoir. . Preferably, the second suction point is located in the bottom of the tank. Since the mechanical system is lubricated only by the second lubrication circuit, it is necessary to limit the stresses of the mechanical system so that these stresses are in accordance with the reduced lubrication which is made on this mechanical system. For example, when the mechanical system is a main power gearbox fitted to a rotary wing aircraft, the speed of the aircraft must be reduced as soon as the lubrication of the mechanical system is reduced. This detection of a drop in the pressure of the lubricating liquid in the first lubrication circuit following a lowering of the level of the lubricating liquid in the reservoir below the position of the first suction point can trigger an audible signal and / or visual to alert an operator of the presence of this leak and reduced lubrication of the mechanical system. This operator can be a pilot of an aircraft when the mechanical system equips this aircraft. In addition, a leak can also appear on the second lubrication circuit.
    [0013] If the leak is at the second exchanger, the lubricating liquid is then not discharged to the outside of the lubrication device according to the invention, but mixes with the tertiary liquid of the tertiary circuit. The level of the lubricating liquid in the reservoir then remains substantially unchanged despite this leakage on the second exchanger of the second lubrication circuit. Advantageously, the lubrication of the mechanical system by the second lubrication circuit is maintained, despite this leakage, this lubrication being provided by a mixture consisting of the lubricating liquid and the tertiary liquid.
    [0014] In addition, depending on the composition of the tertiary liquid and following this leak, it is generally necessary to purge the two circulation circuits and the tank to replace the mixture with lubricating liquid after repair of the leak. In addition, the second heat exchanger is preferably positioned above the tank or in abutment against a side wall of the tank. In fact, the set of second lines is located above the tank as well as the components of the second lubrication circuit except possibly the second heat exchanger.
    [0015] Thus, a leak appearing on a second pipe, one of the components of the second lubrication circuit with the exception of the second heat exchanger or one of the connections between the second pipes and the second heat exchanger advantageously generates no loss of lubricating liquid. . In fact, the lubricating liquid is evacuated by this leak in the tank and then joins the lubricating liquid stored in this tank. As a result, the level of the lubricating liquid in the reservoir is unchanged despite this leakage on the second lubrication circuit. The lubrication of the mechanical system by the second lubrication circuit is then maintained, in spite of this leakage, and the cooling of the lubricating liquid circulating in the second lubrication circuit is ensured, thereby guaranteeing the effectiveness of this lubrication. The second heat exchanger can be located inside the mechanical system while being placed above the tank. For example, the mechanical system is a main power gearbox for a rotary wing aircraft and the second heat exchanger is positioned above a casing of the main power transmission gearbox forming the reservoir of the lubricating device. triple circuit. On the other hand, if a leak appears on the tertiary circuit, the tertiary liquid is discharged outside the tertiary circuit, and generally outside the triple circuit lubrication device, ultimately causing the loss of all the tertiary liquid. . This loss of all the tertiary liquid is characterized by a fall of the third pressure P3 of this tertiary liquid in the tertiary circuit. This fall of the third pressure P3 is detected via the third pressure sensor. A fall of the third pressure P3 is also detected via the third pressure sensor in the event of a major leak on this tertiary circuit, such as a break in a third pipe or at the level of the third heat exchanger. No tertiary liquid then circulates in the second exchanger. As a result, cooling of the lubricating liquid circulating in the second lubrication circuit is not ensured. The lubrication of the mechanical system is then always carried out by the two lubrication circuits, but the cooling of the lubricating liquid is only ensured for the first lubrication circuit. The mechanical system is then effectively lubricated only by the first lubrication circuit. It is then necessary, as when the lubrication of the mechanical system is reduced and ensured only by the second lubrication circuit, to limit the stresses of the mechanical system. This detection of a drop in the tertiary liquid pressure in the tertiary circuit, whether resulting from the loss of all the tertiary liquid in the tertiary circuit or following a major leak on this tertiary circuit, can trigger an audible and / or visual signal to alert an operator of the presence of this leak and the reduced lubrication of the mechanical system. According to a first embodiment of the triple circuit lubricating device according to the invention, the second pressure P2 of the lubricating liquid in the second lubrication circuit is strictly greater than the third pressure P3 of the tertiary liquid in the tertiary circuit. Preferably, the second pressure P2 is substantially greater than the third pressure P3. For example, the second pressure P2 is equal to three bars while the third pressure P3 is equal to one bar. In fact, when a leak appears on the second circuit in the second exchanger, the lubricating liquid circulating in the second circuit with the second pressure P2 is evacuated in the tertiary circuit in which the tertiary liquid is at the third pressure P3 strictly less than the second pressure P2. The tertiary circuit must be a closed circuit in order to prevent the lubricating liquid present in the tank from being evacuated progressively and completely in the tertiary circuit by circulating in the second lubrication circuit. In fact, if the tertiary circuit were opened and the tertiary liquid was drawn into a tertiary reservoir, all of the lubricating liquid would be emptied into this tertiary reservoir, thereby stopping all lubrication of the mechanical system by the first and second lubrication circuits. Since the tertiary circuit is thus a closed circuit, the third pressure P3 increases until it is equal to the second pressure P2. Once this balance of the second and third pressures P2, P3 reaches or close to this balance, the tertiary liquid can also flow into the second lubrication circuit, without posing any problem of operation or safety. Indeed, the tertiary liquid is chosen in priority for these capabilities as heat transfer liquid. However, the tertiary liquid is also chosen taking into account this risk and allows this mixture of lubricating liquid and tertiary liquid to provide lubrication in degraded operation. The tertiary liquid can be, for example, glycol, water or oil.
    [0016] In addition, this mixture is always cooled via the third exchanger. The mechanical system can then continue to function normally without restriction. The second pressure P2 being substantially greater than the third pressure P3, the third pressure sensor makes it possible to detect the increase of the third pressure P3 to the value of the second pressure P2 and to trigger an audible and / or visual signal for alerting an operator on the one hand of the presence of this leak, and on the other hand of the normal lubrication of the mechanical system, the lubricating liquid flowing in the first and second lubrication circuits being sufficiently cooled. On the other hand, the first and second lubrication circuits as well as the tertiary circuit and the tank must then be purged after repair of the leak.
    [0017] According to a second embodiment of the triple circuit lubricating device according to the invention, the second pressure P2 of the lubricating liquid is strictly less than the third pressure P3 of the tertiary liquid. Again, the third pressure P3 is preferably substantially greater than the second pressure P2. For example, the second pressure P2 is equal to three bars while the third pressure P3 is between five and ten bars. In fact, when a leak appears on the second lubrication circuit in the second exchanger, the tertiary liquid circulating in the tertiary circuit with the third pressure P3 is evacuated in the second exchanger and then in the second lubrication circuit in which the liquid lubrication is at the second pressure P2 strictly less than the third pressure P3. In this way, the level of liquid in the reservoir increases, the reservoir then containing a mixture of lubricating liquid and tertiary liquid. On the other hand, the tertiary circuit thus empties completely of the tertiary liquid which it contains. As a result, the tertiary liquid no longer circulates in the third exchanger and, consequently, the lubricating liquid is no longer cooled in the second exchanger. The lubrication of the mechanical system is then always performed by the two lubrication circuits, but the cooling of the lubricating liquid is only ensured by the first lubrication circuit. The mechanical system is then effectively lubricated only by the first lubrication circuit. It is therefore necessary, as when the lubrication of the mechanical system is reduced and ensured only by the second lubrication circuit, to limit the stresses of the mechanical system.
    [0018] In addition, the third pressure P3 of the tertiary liquid in the tertiary circuit drops as soon as this tertiary circuit is empty. This detection of a fall of the third pressure P3 by the third pressure sensor may trigger an audible and / or visual signal to alert an operator of this loss of cooling of the lubricating liquid in the second lubrication circuit and the necessary reduction. solicitations of the mechanical system. When the tertiary circuit is a closed circuit, this tertiary circuit can empty rather quickly, depending on the flow at the level of the leak. The leak then has the rapid consequence of stopping the cooling of the lubricating liquid circulating in the second lubrication circuit and, consequently, a reduced lubrication of the mechanical system. In order to delay the loss of cooling of the lubricating liquid circulating in the second lubrication circuit following this leakage, it is possible to use a tertiary reservoir in which the tertiary circuit draws the tertiary liquid. The quantity of tertiary liquid that can be used by the tertiary circuit is then greater than in the case of a closed tertiary circuit, thus making it possible to cool the lubricating liquid in the second exchanger for a limited time, but greater than in the case of a closed tertiary circuit. This tertiary reservoir is separate and independent of the reservoir in which the first and second circuits draw the lubricating liquid. The tertiary circuit then comprises, in addition to this tertiary reservoir, a third suction point located in the tertiary reservoir. The third pump distributes via the third suction point the tertiary liquid in the third pipes and the second and third heat exchangers. Moreover, in the context of a variant applicable to the two embodiments of the invention, the tertiary circuit can also be used as a backup lubrication circuit in the event of simultaneous or sequential falls in the first and second phases of the invention. second pressures P1, P2 in the first and second lubrication circuits. These falls may be due to failures of the first and second pumps or more likely a leak appeared directly on the reservoir of the lubrication device. Following these drops of the first and second pressures P1, P2, no lubrication of the mechanical system is provided by the first and second lubrication circuits.
    [0019] The tertiary circuit then comprises a tertiary valve and third nozzles. Tertiary pipes allow the circulation of the tertiary liquid to the tertiary valve, then between the tertiary valve and the third nozzles. These nozzles then make it possible to spray the tertiary liquid on the mechanical system in order to lubricate it. Again, the first, second and third nozzles may be constituted by the same series of nozzles common to both lubrication circuits and the tertiary circuit. The first and second lubrication circuits as well as the tertiary circuit then respectively comprise one or more non-return means, such as non-return valves, thus avoiding direct communication between the two lubrication circuits and the tertiary circuit. Thus, a fall of the first and second pressures P1, P2 5 detected by the first and second pressure sensors controls the opening of the tertiary valve. The tertiary liquid then flows to the third nozzles to lubricate the mechanical system for a limited time. This limited time is a function of the amount of tertiary liquid circulating in the tertiary circuit. This limited time is generally greater for an open tertiary circuit comprising a tertiary reservoir than for a closed tertiary circuit. This detection of a fall of the first and second pressures P1, P2 by the first and second pressure sensors, can also trigger an audible and / or visual signal to alert an operator of the loss of lubrication of the mechanical system by the first and second lubrication circuits. This operator then knows that the lubrication of the mechanical system is provided by a backup circuit for a limited time and that he must stop the mechanical system quickly. Particularly if the mechanical system equips a rotary wing aircraft, this aircraft must be directed quickly to a landing site. This triple circuit lubrication device thus makes it possible to provide a global and secure lubrication system for a mechanical system with increased reliability, this lubrication device being composed of two complete and independent lubrication subsystems, with the exception of a common lubricating liquid reservoir, and a tertiary cooling circuit.
    [0020] 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 generally 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.
    [0021] The present invention also relates to a main power transmission gearbox for a rotary wing aircraft. This main power transmission is provided with a triple circuit lubrication device as previously described. The tank of the triple circuit lubrication device is constituted by a casing of the main power transmission gearbox. The second heat exchanger can then be positioned directly in this main power transmission box in order to limit the connections and the second pipes. In fact, any leakage on the second lubrication circuit will evacuate the lubricating liquid in the main transmission gearbox and, consequently, in the reservoir or in the second exchanger and, consequently, in the tertiary circuit. Advantageously, no specific emergency lubrication system, the use of which is very occasional and only in case of failure of a main lubrication system and whose mass can then be penalizing, is not installed on the main transmission gearbox. power. Indeed, the emergency lubrication circuit possibly present on the triple circuit lubrication device is an integral part of the tertiary circuit which is used continuously to cool the lubricating liquid flowing in the second lubrication circuit. 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 and 2, two embodiments of the triple lubrication device circuit. The elements present in several separate figures are assigned a single reference. Two embodiments of a triple-circuit lubrication device 1, shown in FIGS. 1 and 2, serve to lubricate a mechanical system 3 comprising in particular rotary elements 5, such as shafts and bearings, as well as power transmission and speed reduction or increase elements 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 triple-circuit lubrication device 1 comprises a reservoir 2, two lubrication circuits 10, 20 making it possible to lubricate simultaneously the mechanical system 3 and a tertiary circuit 30. The reservoir 2 is formed by a housing of the mechanical system 3 and contains a lubricating liquid. 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, a suction point 16,26 and conduits respectively connecting the components of each lubrication circuit 10,20. The suction points 16, 26 are located in the tank 2. The second suction point 26 is positioned at the bottom of this tank 2 while the first suction point 16 is positioned slightly below the surface of the liquid. In this way, the second suction point 26 is positioned below the first suction point 16 in the bottom of the tank 2. Each pump 11, 21 can draw the lubricating liquid in the tank 2 through via a suction point 16, 26 and distributing 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 first heat exchanger 13 is positioned outside the mechanical system 3. The first heat exchanger 13 is an air / liquid heat exchanger for cooling the lubricating liquid which has been heated by lubricating the mechanical system 3. This heat exchanger air / Liquid uses the air located near the mechanical system 3. A first ventilation system 18 activates the flow of air sweeping the first heat exchanger 13. The second heat exchanger 23 is a liquid / liquid heat exchanger. This liquid / liquid heat exchanger makes it possible to cool the lubrication liquid which has been heated by lubricating the mechanical system 3. This liquid / liquid heat exchanger uses a tertiary liquid circulating in the tertiary circuit 30. The tertiary circuit 30 comprises a third heat exchanger 33 which is an air / liquid heat exchanger. This third heat exchanger 33 is positioned outside the mechanical system 3 and is used to cool the tertiary liquid which has been heated through the second heat exchanger. This air / liquid heat exchanger uses the air located near the mechanical system 3. A second ventilation system 38 activates the circulation of the air sweeping this third heat exchanger 33. For example, the tertiary liquid 30 is water, glycol or oil while the lubricating liquid is oil. According to a first embodiment of the triple-circuit lubrication device 1 shown in FIG. 1, the tertiary circuit 30 is a closed circuit and comprises a third pump 31, a third pressure sensor 32, the second heat exchanger 23, the third heat exchanger 33 and third conduits respectively connecting the components of this tertiary circuit 30.
    [0022] The second heat exchanger 23 is positioned against a wall of the tank 2. In fact, the second pipes of the second lubrication circuit 20 as well as the components 21,22,24,25 of this second lubrication circuit 20, with the exception of this second heat exchanger 23, are located inside the mechanical system 3 and above the tank 2. In fact, any leakage occurring on the second lubrication circuit 20 with the exception of a leak in the second exchanger 23 evacuated This is for example the case for a leak at the connections between the second pipes and the second heat exchanger 23. As a result, there is no loss of lubricating liquid at the level of the connections between the second pipes and the second heat exchanger. the outside of the lubrication device 1 following this leakage and the lubrication of the mechanical system 3 is effectively provided by the two lubrication circuits 10,20.
    [0023] The tertiary liquid 30 circulates in a closed loop through the third pump 32 in the second heat exchanger 23 where it is heated by cooling the lubricating liquid circulating in the second lubrication circuit 20, then in the third heat exchanger 33 in the second which is cooled by air. Furthermore, the lubricating liquid circulates in the second lubrication circuit 20 with a second pressure P2 which is strictly greater than the third pressure P 3 of the tertiary liquid flowing in the tertiary circuit 30. When the second lubricating circuit 20 leaks into the the heat exchanger 23, the lubricating liquid is then evacuated in the tertiary circuit 30. The third pressure P3 then increases until it is equal to the second pressure P2. In fact, the lubricating liquid does not drain outside the triple circuit lubrication device 1. In addition, the tertiary circuit 30 being a closed circuit, the amount of lubricating liquid draining into the tertiary circuit 30 remains limited. As a result, the level of the lubricating liquid is substantially unchanged in the reservoir 2. In addition, a mixture of the lubricating liquid and the tertiary liquid circulating in the tertiary circuit 30 passes through the third heat exchanger 33 and is thus cooled. As a result, the lubricating liquid flowing in the second lubrication circuit 20 is then cooled in the second heat exchanger 23 via this mixture. The lubrication of the mechanical system 3 is thus effected effectively by the first lubrication circuit 10 and the second lubrication circuit 20, without limitation of duration, despite the presence of this leak in the second heat exchanger 23. According to a second embodiment of triple circuit lubrication device 1 shown in FIG. 2, the tertiary circuit 30 is an open circuit and comprises a third pump 31, a tertiary reservoir 37, a third pressure sensor 32, the second heat exchanger 23, a third heat exchanger 33, nozzles 34, a third suction point 36 and third conduits respectively connecting the components of this tertiary circuit 30. This tertiary circuit 30 also comprises a tertiary valve 35 and third nozzles 34. The second heat exchanger 23 is positioned inside the mechanical system 3 and above the tank 2. In fact, the second condu ites of the second lubrication circuit 20 as well as all the components 21,22,23,24,25 of this second lubrication circuit 20 are located inside the mechanical system 3 and above the tank 2. As for the first embodiment of this lubrication device 1, any leakage occurring on the second lubrication circuit 20 with the exception of a leak in the second exchanger 23 discharges lubricating liquid directly into the reservoir 2. As a result, it There is no loss of lubricating liquid outside the lubricating device 1 as a result of this leakage and the lubrication of the mechanical system 3 is efficiently provided by the two lubrication circuits 10,20. The tertiary liquid is drawn by the third pump 32 into the tertiary reservoir 37, then flows into the second heat exchanger 23 where it is heated by cooling the lubricating liquid circulating in the second lubrication circuit 20, then in the third heat exchanger 33 in which it is cooled by air and finally returns to the tertiary tank 37. In addition, the lubricating liquid circulates in the second lubrication circuit 20 with a second pressure P2 which is strictly lower than the third pressure P3 of the tertiary liquid. circulating in the tertiary circuit 30. When a leakage of the second lubrication circuit 20 in the heat exchanger 23, the tertiary liquid is then evacuated in the second lubrication circuit 20. As a result, the totality of the tertiary liquid is thus drain into the second lubrication circuit 20, then into the reservoir 2. The reservoir 2 thus contains a mixture of nsituated by the lubricating liquid and the tertiary liquid. The lubricating liquid always circulates in the second circuit 20, passes through the second exchanger 23 and reaches the nozzles 24 to lubricate the mechanical system 3. On the other hand, there is no more tertiary liquid in the tertiary circuit 30. As a result, , the lubricating liquid is no longer cooled in the second heat exchanger 23. The lubrication provided by the second lubrication circuit 20 is not effective. The lubrication of the mechanical system 3 is thus effected effectively only by the first lubrication circuit 10 following the presence of this leak in the second heat exchanger 23.
    [0024] It is then necessary to reduce the stresses of the mechanical system 3, the lubrication of this mechanical system 3 being reduced. Furthermore, the tertiary circuit 30 also acts as a backup lubrication circuit following a pressure drop in the two lubrication circuits 10,20. Indeed, during such a drop in the pressure in these two lubrication circuits 10,20, the tertiary valve 35 is open to allow the tertiary liquid flowing in the tertiary circuit 30 to reach the nozzles 34 and lubricate and the mechanical system 3. On the other hand, this lubrication is carried out for a limited time, according to the amount of tertiary liquid contained in the tertiary tank 37. In this case, the mechanical system 3 must be stopped rapidly so as not to undergo degradation. when it will no longer be lubricated. When a leak appears on the tertiary circuit 30, whether for the first or the second embodiment of the lubrication device 1 to triple circuit, the tertiary liquid is then evacuated outside the lubricating device 1 to 3 circuit and the mechanical system 3. The tertiary circuit 30 thus completely empties tertiary liquid following this leakage. Cooling of the lubricating liquid of the second lubrication circuit 20 is then no longer ensured in the second heat exchanger 23.
    [0025] The lubrication of the mechanical system 3 is thus effected effectively only by the first lubrication circuit 10 following the presence of this leak on the tertiary circuit 30. It is then necessary to reduce the stresses on the mechanical system 3, the lubrication of this mechanical system 3 being reduced.
    [0026] Likewise, when a leak appears on the first lubrication circuit 10, whether for the first or the second embodiment of the lubrication device 1 with a triple circuit, the lubricating liquid circulating in this first lubrication circuit 10 it then escapes outside the triple circuit lubrication device 1 and the mechanical system 3. The level of lubricating liquid present in the reservoir 2 decreases and as soon as it is below the level of the first suction point 16, the first pump 11 is defused and the circulation of the lubricating liquid in the first lubrication circuit 10 is stopped following this leakage. The lubrication of the mechanical system 3 is then no longer ensured by the first lubrication circuit 10. The lubrication of the mechanical system 3 is thus effected effectively only by the second lubrication circuit 20 following the presence of this leak on the first circuit of Lubrication 10. It is then necessary to reduce the stresses of the mechanical system 3, the lubrication of this mechanical system 3 being reduced. This lubrication device 1 with triple circuit thus makes it possible to propose a lubrication system of a mechanical system 3 with increased reliability. This triple circuit lubrication device 1 ensures a continuous cooling of the lubricating liquid and does not have a limitation of the lubrication time following the detection of a leak, except in the exceptional case of a loss. simultaneous of the two lubrication circuits 10,20.
    [0027] 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 (11)
    [0001]
    REVENDICATIONS1. Triple 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), a first heat exchanger (13), first nozzles (14) and a first suction point (16) of said lubricating liquid, a second lubrication circuit (20) having a second pump (21), second lines, a second pressure sensor (22), a second heat exchanger (23). ), second nozzles (24) and a second suction point (26) of said lubricating liquid, said first and second suction points (16, 26) being located in said reservoir (2), each pump (11, 21) distributing through said first and second suction points (16,2 6) 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 triple lubrication device (1) circuit comprises a tertiary circuit (30) in which a tertiary liquid circulates, said tertiary circuit (30) comprising a third pump (31), third conduits, a third pressure sensor (32), said second heat exchanger (23) and a third heat exchanger (33), said third pump (31) for circulating said tertiary liquid in said second heat exchanger (23) and said third heat exchanger (33), said second suction point (26) being located below said first suction point (16).
    [0002]
    2. Lubrication device (1) according to claim 1, characterized in that said tertiary circuit (30) is a closed circuit.
    [0003]
    3. Lubricating device (1) according to claim 1, characterized in that said tertiary circuit (30) comprises a tertiary reservoir (37) and a third suction point (36), said third suction point (36). being located in said tertiary reservoir (37), said third pump (31) distributing via said third suction point (36) said tertiary liquid in said third conduits and said second and third heat exchangers (23,33).
    [0004]
    4. Lubricating device (1) according to any one of claims 1 to 2, characterized in that, said lubricating liquid flowing in said second lubrication circuit (20) with a second pressure P2, said tertiary liquid flowing in said tertiary circuit (30) with a third pressure P3, the second pressure P2 of said lubricating liquid is strictly greater than said third pressure P3 of said tertiary liquid.
    [0005]
    5. Lubricating device (1) according to any one of claims 1 to 3, characterized in that, said lubricating liquid flowing in said second lubrication circuit (20) with a second pressure P2, said tertiary liquid flowing in said tertiary circuit (30) with a third pressure P3, the second pressure P2 of said lubricating liquid is strictly less than said third pressure P3 of said tertiary liquid.
    [0006]
    6. Lubrication device (1) according to any one of claims 1 to 5, characterized in that said second heat exchanger (23) is adapted to be located within said mechanical system (3).
    [0007]
    7. Lubrication device (1) according to any one of claims 1 to 6, characterized in that said second heat exchanger (23) is adapted to be located above said tank (2).
    [0008]
    8. Lubrication device (1) according to any one of claims 1 to 5, characterized in that said second heat exchanger (23) is adapted to be located against a wall of said tank (2).
    [0009]
    9. The lubricating device according to claim 1, wherein said tertiary circuit comprises a tertiary valve and third nozzles.
    [0010]
    Lubricating device (1) according to any one of claims 1 to 9, characterized in that said mechanical system (3) is a main gearbox (31) of a rotary wing aircraft (30) .
    [0011]
    11. 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 10, 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
    CN105570441B|2018-01-12|
    KR101787739B1|2017-10-18|
    KR20160051646A|2016-05-11|
    US9829088B2|2017-11-28|
    EP3015743A1|2016-05-04|
    FR3027992B1|2016-12-09|
    CN105570441A|2016-05-11|
    US20160123456A1|2016-05-05|
    EP3015743B1|2017-05-24|
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    法律状态:
    2015-10-23| PLFP| Fee payment|Year of fee payment: 2 |
    2016-05-06| PLSC| Publication of the preliminary search report|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
    FR1402468A|FR3027992B1|2014-10-31|2014-10-31|LUBRICATION DEVICE WITH INCREASED TRIPLE CIRCUIT RELIABILITY OF A MAIN POWER TRANSMISSION BOX OF AN AIRCRAFT|FR1402468A| FR3027992B1|2014-10-31|2014-10-31|LUBRICATION DEVICE WITH INCREASED TRIPLE CIRCUIT RELIABILITY OF A MAIN POWER TRANSMISSION BOX OF AN AIRCRAFT|
    EP15186803.1A| EP3015743B1|2014-10-31|2015-09-25|A triple circuit lubrication device with increased reliability for a main power transmission gearbox of an aircraft|
    CN201510695500.6A| CN105570441B|2014-10-31|2015-10-23|Active force for aircraft transmits high reliability No. three lubricating arrangement of gear-box|
    US14/924,776| US9829088B2|2014-10-31|2015-10-28|Triple circuit lubrication device with increased reliability for a main power transmission gearbox of an aircraft|
    KR1020150150937A| KR101787739B1|2014-10-31|2015-10-29|A TlRIPLE CIRCUIT LUBRICATION DEVICE WITH INCREASED RELIABILITY FOR A MAIN POWER TRANSMISSION GEARBOX OF AN AIRCRAFT|
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