• 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 relief lubrication device (1) with simplified architecture of a mechanical system (10). Said emergency lubricating device (1) is provided with a reservoir (2), a triggering means (3), at least one pipe (4) and at least one distribution means (5) . Said tank (2) contains a lubricating liquid and is arranged inside said mechanical system (10) and above said pipes (4) and said dispensing means (5). Each distribution means (5) comprises at least one restriction means (6) for limiting the flow of said lubricating liquid. Said lubricating liquid is heated by said mechanical system (10) and the viscosity of said lubricating liquid decreases so that the flow rate of said lubricating liquid at each dispensing means (5) is substantially equal to or greater than a minimum flow rate as long as said reservoir contains said lubricating liquid.
    公开号:FR3045764A1
    申请号:FR1502623
    申请日:2015-12-17
    公开日:2017-06-23
    发明作者:Jean Victor Lapeyre；Duvernay Gilles Eymard
    申请人:Airbus Helicopters SAS；
    IPC主号:
    专利说明:

    Simplified architecture emergency lubrication device for a main gearbox of an aircraft
    The present invention relates to the field of emergency lubrication of transmission boxes, in particular power transmission boxes for a rotary wing aircraft.
    The present invention relates to an emergency lubrication device with simplified architecture for a mechanical system. This emergency lubrication device is 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 oil. This lubrication is generally provided by a lubrication circuit and has the main functions of limiting the wear and warming of these elements of the mechanical system and, consequently, to extend its life. 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 arranged 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 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 can be set in parallel with a main lubrication circuit as described in US 8230835. Each lubrication circuit has its own pump, but uses the same oil reservoir. 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.
    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.
    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 casing of the main power transmission gearbox. In fact, in the event of leakage of one of the lubrication circuits, the bottom of the main transmission gear box will, in a more or less long period, empty and cause the failure of the complete lubrication system.
    Some lubrication systems include an emergency reservoir, sometimes directly mounted within the mechanical system to be lubricated as described in EP 2505878 and US 2007/0261922. 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.
    In addition, according to US 2007/0261922, 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.
    In addition, the device described in document FR 2685758 also comprises an emergency tank supplying an oil distribution circuit via a pipe. The emergency tank can be pressurized and the opening of a valve allows the circulation of oil in the pipeline. This emergency tank can also be non-pressurized, a pump then supplying the pipeline. The relief tank can thus be positioned without particular constraint vis-à-vis the essential organs to lubricate. In case of failure of the main lubrication circuit, the opening of the valve or the starting of the pump is controlled manually or automatically according to a threshold value of the pressure or the temperature of the oil. The lubrication of these essential organs is ensured for a limited time corresponding to the depletion of the oil contained in this emergency tank.
    Moreover, the document WO 2008/091341 describes a lubricating device comprising an external circuit allowing only the cooling of the oil and an internal circuit ensuring the lubrication of the rotating elements of the mechanical system. If a leakage and a lowering of the level of lubricating liquid in the crankcase are detected, the air inside the crankcase is expelled outside the crankcase in order to create a vacuum inside the crankcase. crush and thus limit the flow of this leak. The internal circuit can then continue to lubricate these rotating elements for a limited time, as long as the housing contains lubricating liquid.
    The object of the present invention is therefore to provide an emergency lubricating device for a mechanical system making it possible to overcome the limitations mentioned above, enabling the essential components of this mechanical system to be lubricated despite the presence of a failure on the main lubrication circuit for a limited and guaranteed minimum duration. The present invention also aims to simplify the architecture of this relief lubrication device to improve its reliability while reducing its weight and cost.
    According to the invention, an emergency lubrication device of simplified architecture, intended for the lubrication of a mechanical system, is provided with a reservoir, a triggering means, at least one pipe and at least one a distribution means. The reservoir contains a lubricating liquid and the triggering means allows a circulation of the lubricating liquid between the reservoir and each distribution means in the event of detection of a malfunction of a main lubricating means of the mechanical system.
    This mechanical system is for example a main gearbox of power of a rotary wing aircraft.
    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. For this purpose, the mechanical system comprises at least one main lubrication means ensuring the lubrication of these rotating elements and of these transmission elements. Each main lubricating means may comprise in known manner an exchanger for cooling the lubricating liquid.
    For the sake of simplification, it is considered that the mechanical system comprises a single main lubrication means. In case of failure or malfunction of this main lubricating means, the emergency lubrication device according to the invention allows at least a lubrication of the essential organs of the mechanical system to ensure the operation of this mechanical system for a minimum period of time , of the order of thirty minutes to two hours. Each dispensing means is then arranged inside the mechanical system to lubricate at least these essential organs.
    The triggering means allows the start of the emergency lubrication device when a fault or a malfunction of the main lubricating means is detected. This failure and / or malfunction can be detected in different ways. For example, a decrease in the pressure of the lubricating liquid in the main lubricating means or a decrease in the level of the lubricating liquid in a reservoir of this main lubricating means can be detected. An increase in the temperature of the mechanical system subsequent to stopping the lubrication of this mechanical system can also be detected.
    The emergency lubrication device according to the invention is remarkable in that the reservoir is arranged above the pipes and distribution means so that the lubricating liquid circulates under the action of the Earth's gravity from the reservoir in each driving and each means of distribution. This emergency lubrication device is also remarkable in that each distribution means comprises at least one restriction means, in order to limit the flow of the lubricating liquid at each distribution means, and is arranged inside the system. mechanical, each pipe supplying each distribution means being also arranged at least partially inside the mechanical system. The lubricating liquid circulating in each pipe and in each distribution means is thus heated by the mechanical system due to a malfunction of the main lubricating means of the mechanical system and, consequently, the viscosity of the lubricating liquid decreases so that the flow rate of the lubricating liquid at each dispensing means is substantially equal to or greater than a minimum flow rate as long as the reservoir contains lubricating liquid.
    Advantageously, the tank positioned above the pipes and distribution means allows the emergency lubrication device according to the invention to use no pressure generator. Indeed, only the action of the Earth's gravity allows the circulation of the lubricating liquid of the reservoir to each pipe and each distribution means.
    A pressure generator traditionally used in a main or emergency backup lubricating device may be a pump or a pressurized tank. The absence of such a pressure generator advantageously eliminates the use of a mechanical component that may be malfunctioning or failure and thus eliminates a potential cause of malfunction of the emergency lubrication device. The reliability of the emergency lubrication device according to the invention is thus improved. In addition, the mass of the emergency lubrication device according to the invention is also reduced by the absence of a pressure generator, as well as its cost.
    In addition, each distribution means comprises at least one restriction means. A restriction means is a reduction in the dimensions of the section through which the lubricating liquid circulates, advantageously making it possible to limit the flow rate of the lubricating liquid circulating at each distribution means.
    For example, a restriction means is formed by a cone whose outlet section is an orifice of a first diameter less than one millimeter (1mm). The dispensing means comprising this restriction means thus allows a low flow rate of the lubricating liquid. This small outlet section combined with the viscosity of the lubricating liquid typically makes it possible to have a flow rate of the lubricating liquid in the form of droplets, the frequency of appearance of these drops being in particular a function of the dimensions of the outlet section of the lubricant. restriction means, the height of the lubricating liquid column located above this distribution means and the viscosity of the lubricating liquid.
    Preferably, a dispensing means comprises a restriction means and a filter. The filter makes it possible to filter the lubricating liquid in order to avoid clogging this restriction means.
    Such dispensing means replaces in particular a nozzle traditionally used on a main or emergency lubricating means in order to spread a mechanically pressurized lubricating liquid.
    Each distribution means of the emergency lubrication device according to the invention advantageously comprises no moving part, which greatly limits the risk of malfunction of this emergency lubrication device and thus improves its reliability. In addition, such a dispensing means has a mass equal to or less than a nozzle which is traditionally used on a main or emergency lubrication means.
    Each distribution means of the emergency lubrication device according to the invention is arranged above the rotating and transmission elements of the mechanical system and close to an essential member of this mechanical system in order to cool this essential organ.
    The lubricating liquid flows from the reservoir to the distribution means through the lines of the emergency lubrication device according to the invention.
    The triggering means for starting the emergency lubrication device according to the invention may comprise several first valves. These first valves are for example positioned at each distribution means. Such an arrangement of the first valves has the advantage of lubricating the mechanical system upon activation of the triggering means. Indeed, the first valves being positioned at each distribution means, the pipes near these distribution means are filled with lubricating liquid then flowing in each distribution means upon activation of the triggering means which controls the opening of the first valves. Thus, the mechanical system is lubricated as soon as the malfunction of the main lubricating means is detected.
    On the other hand, the emergency lubrication device according to the invention then comprises several first valves which increase firstly the mass and secondly the cost of this emergency lubrication device according to the invention.
    Preferably, the triggering means of this emergency lubrication device comprises a single first valve for communicating the reservoir and each pipe. This first valve is for example arranged directly at the outlet of the tank. In this case, upon activation of the triggering means, following the detection of a malfunction of the main lubricating means of the mechanical system, the liquid fills the pipes and reaches the distribution means after a start time. This start time is however low and of the order of a few seconds. This startup time therefore does not question the effectiveness of the emergency lubrication device according to the invention for lubricating and cooling the mechanical system. This triggering means comprising a single first valve thus advantageously makes it possible to minimize the mass and the cost of the emergency lubrication device according to the invention.
    The triggering means may also include a second valve for venting the tank. This second valve is necessary when the tank is closed and sealed to allow the exit of the lubricating liquid from the tank and the entry of air into the tank.
    Each first valve and each second valve of the triggering means may be reversible valves allowing several times their opening and closing. Such a reversible valve has the advantage of making it possible to stop the supply of the distribution means and the lubrication of the mechanical system after the detection of a malfunction of the main lubricating means and the activation of the triggering means. This stop of the supply of the dispensing means makes it possible to stop the flow of the lubricating liquid still present in the reservoir, for example when the mechanical system has been stopped or when the malfunction of the main lubricating means has disappeared.
    Preferably, each first valve and each second valve are valves that can be used once. Such a one-time valve has the advantage of being extremely reliable, especially vis-à-vis a reversible valve. In addition, the amount of lubricating liquid in the reservoir is limited to allow lubrication and cooling of the mechanical system for a limited time. As a result, the emergency lubrication device according to the invention gives priority to the reliability with respect to the loss of a limited quantity of lubricating liquid. In addition, the non-operation of an emergency lubrication device following a failure of a valve can be dramatic in the case where the mechanical system is for example a main power transmission gearbox of a rotary wing aircraft and the malfunction of the main lubricating means appears during a flight of the aircraft.
    In addition, when the trigger means comprises a single first valve, this first valve and the second valve can be grouped into a single component advantageously to have a single control means actuating the opening of these two valves.
    The tripping means is preferably pyrotechnically controlled to control the opening of the first valve and that of the second valve and thus allow the flow of the lubricating liquid from the reservoir to the distribution means via the pipes. Such a pyrotechnic control has the advantages of being extremely reliable, lightweight and having a very low maintenance cost. Indeed, the operation of a pyrotechnic control is generally guaranteed for a lifetime of between 10 and 20 years.
    The triggering of this pyrotechnic control can be electric or thermal. An electric trip of the pyrotechnic control is obtained for example in known manner through a means for detecting a malfunction of the main lubricating means of the mechanical system.
    A thermal trip of the pyrotechnic control is advantageously obtained following the increase of the temperature of the mechanical system. The triggering means and the reservoir are then in the mechanical system. In case of malfunction of the main lubricating means, the temperature of the mechanical system will increase following the cessation of lubrication and cooling by the main lubricating means. As soon as the temperature of the triggering means located inside the mechanical system reaches a predetermined threshold, the pyrotechnic control is triggered, allowing the flow of the lubricating liquid from the reservoir to the distribution means via the pipes. The value of this predetermined threshold may for example be of the order of 150 ° C.
    Such a thermal trip of the pyrotechnic control advantageously avoids the use of a means for detecting a malfunction of the main lubricating means which may be subject to malfunctions and thus improves the reliability of the emergency lubrication device according to the invention .
    The triggering means can also be fully electrically controlled to control the opening of the first valve and the opening of the second valve via a means for detecting a malfunction of the main lubricating means of the mechanical system. .
    Furthermore, each distribution means is arranged inside the mechanical system and each pipe feeding each distribution means is arranged at least partially within this mechanical system.
    The temperature of the mechanical system will increase due to a malfunction of the main lubricating means and stopping lubrication and cooling by this main lubrication means.
    This temperature increases in fact firstly due to the start time of the emergency lubrication device between the stopping of the main lubricating means and the instant when the emergency lubrication device lubricates the essential organs of the mechanical system and of on the other hand, the lubrication and cooling carried out by the emergency lubrication device are less efficient than those carried out by the main lubricating means. The emergency lubrication device does not generally lubricate all the rotating and transmission elements of the mechanical system, but only the essential organs and the flow of the lubricating liquid is lower for an emergency lubrication device vis-à-vis a main lubrication means.
    The temperature of the mechanical system increases for example from a nominal temperature of the order of 80 ° C to a maximum temperature of about 150 ° C for certain areas of the mechanical system.
    Thus, following a malfunction of the main lubricating means of the mechanical system and the activation of the triggering means of the emergency lubrication device, lubricating liquid circulates in each pipe and in each distribution means. This lubricating liquid is then progressively heated by the mechanical system and, as a result, the viscosity of the lubricating liquid gradually decreases.
    At the same time, the lubrication of the essential organs of the mechanical system, the reservoir gradually empties the lubricating liquid that it contains. In addition, the lubricating liquid flows by the action of Earth's gravity. Consequently, the flow rate of the lubricating liquid leaving a dispensing means is a function, in particular, of the height of the lubricating liquid column situated above this dispensing means and the viscosity of the lubricating liquid.
    Advantageously, the lowering of the viscosity of the lubricating liquid, resulting in an increase in the flow rate of this lubricating liquid, makes it possible to compensate, as a minimum, for the decrease in the height of the column of lubricating liquid, which causes a decrease in this flow rate. . In this way, the flow of the lubricating liquid at each dispensing means is substantially constant or increases gradually during operation of the emergency lubrication device as the reservoir contains lubricating liquid.
    Thus, this flow rate of the lubricating liquid at each dispensing means is substantially equal to or greater than a minimum flow rate as long as the reservoir contains lubricating liquid. For a dispensing means, the minimum flow rate is equal to the flow rate of the lubricating liquid at this distribution means at the start of the emergency lubrication device.
    For the entire emergency lubrication device, the minimum flow rate is equal to the flow rate of the lowest lubricating liquid at the dispensing means at the start of the emergency lubrication device. The surrounding temperature and the first diameter of the restriction means have an influence on the flow rate of the dispensing means. This minimum flow rate is for example of the order of 0.2 liters per hour (0.21 / h).
    In order to promote this decrease in the viscosity of the lubricating liquid, the distribution means are preferably placed in an area of the mechanical system which undergoes a significant increase in temperature when using the emergency lubrication device. Advantageously, the dispensing means being arranged above the rotating elements and transmission of the mechanical system and near an essential organ. In fact, following the failure of the main lubricating means, this essential member is not lubricated or insufficiently lubricated, then heats and heats by heat conduction the distribution means and in particular the restriction means that comprises . The lubricating liquid contained by the restriction means and the dispensing means is then heated and its viscosity decreases. The flow rate of this lubricating liquid is in fact increased and this lubricating liquid flows over an area near this essential organ. In this way, the emergency lubrication device according to the invention makes it possible to lubricate and cool this zone and, also by thermal conduction, this essential organ in order to limit or even prevent the degradation of this essential organ.
    Moreover, the dispensing means can be arranged above and in line with an essential member so that the lubricating liquid flows directly on this essential member and thus cools and lubricates this essential member.
    In addition, in order to contribute to the flow rate of the lubricating liquid being substantially equal to or greater than the minimum flow rate, it is preferable for the lines of the emergency lubrication device to have dimensions making it possible on the one hand to limit the pressure drops. lubricating liquid flowing in these pipes and secondly to promote the increase of the temperature of the lubricating liquid and, consequently, the decrease in its viscosity. This limitation of the pressure drop of the lubricating liquid is mainly necessary when the lubricating liquid is still at a high viscosity, that is to say in the first moments of the use of the emergency lubrication device. In fact, the pressure drops then decrease when the viscosity of the lubricating liquid decreases.
    In this way, each pipe has a second internal diameter greater than or equal to a first minimum value in order to allow sufficient heating of the lubricating liquid. For example, the first minimum value is between 6 mm and 10 mm.
    Furthermore, the emergency lubrication device according to the invention preferably comprises a single first valve located at the outlet of the tank. In fact, the lines and the dispensing means do not contain lubricating liquid as long as no malfunction of the main lubricating means is detected and the triggering means is not activated. As a result, no risk of coking of the lubricating liquid in the pipes and the distribution means exists as long as the emergency lubrication device according to the invention does not work.
    Then, when the emergency lubrication device is operating and the lubricating liquid flowing in the pipes and the distribution means, the section of the restriction means must not be too weak in order not to generate a significant local heating of the lubricating liquid. . Indeed, if such a large local heating of the lubricating liquid occurs, a coking of the lubricating liquid could appear locally at a restriction means, cause the clogging of this restriction means and, consequently, a malfunction of the emergency lubrication device according to the invention.
    In this way, each restriction means comprises an orifice whose first diameter is greater than or equal to a second minimum value. For example, the second minimum value is between 0.3 mm and 1.0 mm.
    In addition, as long as the lubricating liquid circulates in the pipes and the distribution means, the risk of occurrence of coking of the lubricating liquid is also reduced, the lubricating liquid being in motion.
    Thus, the combination of adapted sections, restriction means and the absence of lubricating liquid in the pipes and the distribution means, as long as the triggering means is not activated, helps to limit the risk of occurrence. coking lubricating liquid.
    However, it is advisable not to position the dispensing means in an area of the mechanical system where the temperature is excessive in order to limit the risk of occurrence of coking of the lubricating liquid.
    However, this excessive temperature depends on the characteristics of the lubricating liquid used. This excessive temperature is for example of the order of 200 ° C or higher if the lubricating liquid used is a high performance oil.
    In addition, the tank can also be arranged inside the mechanical system. In fact, all the pipes are also arranged inside the mechanical system. As a result, the totality of the lubricating liquid of the emergency lubrication device according to the invention is subjected to the temperature increase of the mechanical system following a malfunction of the main lubricating means.
    Moreover, the position and the shape of the reservoir as well as the position of the distribution means can have an influence on the flow of the lubricating liquid at each distribution means and on the evolution of this flow rate.
    The value of this flow rate is particularly dependent on the height of the lubricating liquid column located above each distribution means. This column of lubricating liquid is formed by the sum of the height H1 of the lubricating liquid in the reservoir and the distance H21, H22 between the reservoir and each distribution means, the height H1 and the distance H21, H22 being defined according to the direction of gravity.
    In fact, depending on the shape of the tank, the drop in the height H1 of lubricating liquid will be more or less rapid. As a result, the evolution of the flow rate at each distribution means may also be more or less rapid. In particular, for a given volume of lubricating liquid, the lower the height H1 before the activation of the trigger means, the lower the height H1 will be slow during lubrication of the mechanical system by the emergency lubrication device.
    However, the shape of this tank can be imposed by the space available by the mechanical system when the tank is arranged in the mechanical system.
    In addition, the height H1 decreases during operation of the emergency lubrication device while the distance H21, H22 is constant. In fact, this distance H21, H22 is a dimensioning value to obtain a flow rate at each distribution means which varies only slightly whatever the height H1. In fact, the height H1 of the lubricating liquid in the reservoir is preferably less than the distance H21, H22 between the reservoir and each distribution means. The influence of the variation of the height H1 on the flow of the lubricating liquid at each distribution means is therefore reduced.
    In addition, as mentioned above, the viscosity of the lubricating liquid decreases during operation of the emergency lubrication device which, combined with the reduced influence of the variation of the height H1 on the flow of the lubricating liquid at the level of each distribution means, contributes that the flow rate at each distribution means is substantially equal to the minimum flow, or even greater than this minimum flow.
    It may also be interesting that the flow of the lubricating liquid increases during operation of the emergency lubrication device. Indeed, this relief lubrication device has a lower efficiency by means of main lubrication. In fact, the temperature of the mechanical system may continue to increase during operation of the emergency lubrication device.
    Thus, the increase in this flow rate during the operation of the emergency lubrication device makes it possible to increase the lubrication of the mechanical system in parallel with the increase in the temperature of this mechanical system.
    As a result, the height H1 and the distance H21, H22 are preferably initially defined so that the reduction in the height H1, when the emergency lubrication device lubricates the mechanical system, and the decrease in the viscosity of the lubricating liquid make it possible to have a flow of the lubricating liquid at each distribution means and throughout the operation of this relief lubrication device substantially equal to the minimum flow, or even greater than this minimum flow.
    The emergency lubrication device according to the invention therefore makes it possible to provide a flow of lubricating liquid at least substantially constant, or even increasing, this flow being ensured by the height of the column of lubricating liquid, by using the increase in the mechanical system temperature following the failure of the main lubricating means to improve the efficiency of this relief lubrication device.
    This emergency lubrication device according to the invention thus has the advantage of high reliability, the architecture of this emergency lubrication device being simplified by eliminating the use of nozzles, a pump or a pump. pressurized tank which were often the cause of dormant failures on such relief lubrication devices traditionally used. The only mechanical device of the emergency lubrication device according to the invention is the triggering means which is preferably a single use element to ensure its reliability.
    This high reliability is essential for a backup lubrication device which must absolutely ensure this function to allow lubrication of the essential organs of the mechanical system following a stop of the main lubrication.
    In addition, this simplified architecture of the emergency lubrication device according to the invention also makes it possible to limit the mass and the cost of this emergency lubrication device.
    This limitation of the mass of this emergency lubrication device is important for this function, which is, in general, very rarely used during the service life of the mechanical system, in order not to penalize in particular the performance of the aircraft when this mechanical system equips an aircraft.
    The present invention also relates to a main power transmission gearbox for a rotary wing aircraft. This main power transmission is provided with a relief lubrication device as previously described. 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: FIG. 1 a mechanical system comprising an emergency lubricating device according to FIG. invention, and - Figure 2, a sectional view of a distribution means of the relief lubrication device.
    The elements present in several separate figures are assigned a single reference.
    A mechanical system 10 comprising a main lubricating means 20 and a spare lubrication device 1 is shown in FIG. 1. This mechanical system 10 comprises in particular rotating elements 12, such as shafts and bearings, as well as transmission 13 of power and reduction or increase of speed, such as pinions and / or gears. This mechanical system 10 is for example a main power transmission gear equipping a rotary wing aircraft.
    The main lubricating means 20 and the emergency lubrication device 1 have the function of lubricating and cooling all or part of the mechanical elements 12, 13 of this mechanical system 10.
    The main lubricating means 20 comprises a suction point 21, a pump 22, a heat exchanger 23, a filter 24 and nozzles 25. The nozzles 25 are positioned above the rotating elements 12 and the transmission elements 13. The pump 22 can suck a lubricating liquid, such as oil, located in a housing 11 of the mechanical system 10 and spray through the nozzles 25 on the mechanical elements 12,13. The main lubricating means 20 thus makes it possible to lubricate and cool these mechanical elements 12, 13.
    The emergency lubrication device 1 comprises a reservoir 2 containing a lubricating liquid, a triggering means 3, lines 4 and distribution means 5. The emergency lubrication device 1 is entirely arranged inside the mechanical system. 10 and the tank 2 is positioned above the pipes 4 and dispensing means 5. The triggering means 3 is located at the outlet of the tank 2 and comprises two valves 31, 32. Two distribution means 5 are positioned above first essential members 14 among the rotating elements 12 and two distribution means 5 are respectively positioned above second essential members 15, 16 among the transmission elements 13.
    The triggering means 3 allows a circulation of the lubricating liquid between said reservoir and each distribution means 5 in the event of detection of a malfunction of the main lubricating means 20. For this purpose, the triggering means 3 comprises a first valve 31 arranged between the tank 2 and a first pipe 4 and a second valve 32 arranged on a pipe 8. The pipe 8 makes it possible to connect the inside of the tank 2 to the outside of this tank 2.
    Thus, the opening of the second valve 32 ensures a venting of the tank 2. This venting of the tank 2 is essential to allow the flow of the lubricating liquid to the first pipe 4 when the first valve 32 is open, the tank 2 being closed and sealed. A tank 2 closed and sealed avoids the intrusion into this tank 2 of foreign bodies and dust. A closed and sealed tank 2 is also useful when the mechanical system 10 equips an aircraft. Indeed, the attitude of an aircraft can vary during a flight and in particular during turns. The lubricating liquid could then leave the tank 2 if it had one or more openings allowing the permanent airing of the tank 2. The opening of the first valve 31 allows the flow of the lubricating liquid from the tank 2 in the first pipe 4, then to each distribution means 5 via the other pipes 4. This flow of the lubricating liquid is achieved solely by the action of Earth's gravity, the tank 2 being unpressurized and located above the lines 4 and the distribution means 5.
    The first and second valves 31, 32 are single-use valves. Such one-time valves 31, 32 have the advantages of being extremely reliable and of having a long service life without any particular maintenance operation. The opening of this first and second valve 31,32 is triggered simultaneously by the activation of the tripping means 3 as soon as a malfunction of the main lubricating means 20 is detected. This opening of the first and second valves 31, 32 allows the flow of the lubricating liquid from the tank 2 to the distribution means 5 via the lines 4. The activation of the triggering means 3 is pyrotechnically controlled, this pyrotechnic control being triggered thermally. Thus, this tripping means 3 is activated as soon as the ambient temperature of this tripping means 3 reaches a predetermined threshold. The emergency lubrication device 1 being entirely arranged inside the mechanical system 10, the ambient temperature of the tripping means 3 is substantially equal to the temperature of the mechanical system 10. In addition, following a malfunction of the main lubricating means 20, the lubrication and cooling of mechanical elements 12,13 are degraded or stopped. As a result, the temperature of the mechanical system 10 increases as a result of the degradation or stopping of this lubrication and cooling of the mechanical elements 12, 13.
    In this way, the tripping means 3 is activated as soon as the temperature of the mechanical system near the tripping means 3 reaches a predetermined threshold, which then characterizes a malfunction of the main lubricating means 20.
    The triggering of the pyrotechnic control of the tripping means 3 can also be electrical. This electric triggering of the pyrotechnic control is obtained by means of a detection means (not shown) of a malfunction of the main lubricating means 20. This detection means makes it possible, for example, to detect a drop in the pressure of the liquid lubricating in the main lubricating means 20 or a decrease in the level of the lubricating liquid in the housing 11 of the mechanical system 10.
    Furthermore, the tripping means 3 can also be totally electrically controlled and then also uses such a means for detecting a malfunction of the main lubricating means 20.
    A sectional view of a dispensing means 5 is shown in FIG. 2. This dispensing means 5 comprises a restriction means 6 and a filter 7. A restriction means is a reduction in the dimensions of the section through which circulates the lubricating liquid, advantageously making it possible to limit the flow rate of the lubricating liquid circulating at each distribution means 5.
    The restriction means 6 is formed by a cone whose output section is an orifice of a first small diameter D1. This restriction means 6 makes it possible to reduce the flow rate of the lubricating liquid leaving the dispensing means 5. The filter 7 makes it possible to filter the lubricating liquid entering the dispensing means 5 via the line 4 in order in particular to avoid clogging the Restriction means 6. This low first diameter D1 typically allows a flow of the lubricating liquid in the form of droplets at the outlet of each distribution means 5.
    In addition, the first diameter D1 is greater than or equal to a second minimum value so as not to generate a significant local heating of the lubricating liquid and, consequently, a coking of the lubricating liquid. The second minimum value is for example between 0.3 mm and 1.0 mm.
    Furthermore, the emergency lubrication device 1 being entirely arranged inside the mechanical system 10, the lubricating liquid in the reservoir 2 and the lubricating liquid circulating in the lines 4 and the distribution means 5 are subject at the increasing temperature of the mechanical system 10. This lubricating liquid is then gradually heated and its viscosity also decreases gradually.
    In addition, the lubrication of the essential organs 14, 15, 16 causes a gradual decrease in the level of the lubricating liquid in the tank 2. As a result, the decrease in the height of the column of lubricating liquid located above each means 5 also tends to reduce the value of the flow of the lubricating liquid leaving each distribution means 5.
    Advantageously, the drop in the viscosity of the lubricating liquid following the increase in the temperature of the mechanical system 10 makes it possible to compensate for this decrease in the height of the column of lubricating liquid and contributes to keeping at least a flow rate of the lubricating liquid. substantially constant, even increasing.
    In addition, it can be seen in FIG. 1 that the height H1 of the lubricating liquid in the reservoir 2 is clearly smaller than the distances H21, H22 between the reservoir 2 and the various distribution means 5, the height H1 and the distance H21. H22 being defined according to the direction of gravity. In fact, the lowering of the height H1 of the lubricating liquid in the tank 2 causes only a very slight drop in the height of the column of lubricating liquid situated above each distribution means 5.
    As a result, the flow rate of the lubricating liquid at each dispensing means 5 is substantially equal to or greater than a minimum flow rate during operation of the emergency lubricating device 1 as long as the reservoir 2 contains lubricating liquid. For each distribution means 5, this minimum flow rate is equal to the flow rate of the lubricating liquid at this dispensing means 5 at the start of the emergency lubrication device 1. This minimum flow rate is, for example, equal to 0.2 l / h.
    Furthermore, in order to limit the disturbances that can limit the flow of the lubricating liquid, the pipes 4 have dimensions making it possible, on the one hand, to limit the pressure drops of the lubricating liquid circulating in these pipes 4 and, on the other hand, to favor the increase of the temperature of the lubricating liquid and, consequently, the decrease of its viscosity. Each pipe 4 thus has a second inner diameter D2 greater than or equal to a first minimum value, for example between 6 mm and 10 mm.
    This relief lubrication device 1 therefore has a simplified architecture, without the use of pumps, sprinklers or a pressurized tank, and a mass and a reduced cost. This reduced mass is important for this function, which is very rarely used during the service life of the mechanical system, but which is nevertheless indispensable to the mechanical system 10 in the event of a malfunction of the main lubricating means 20. Moreover, this simplified architecture ensures a high level of reliability. to this emergency lubrication device 1.
    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 (16)
    [1" id="c-fr-0001]
    1. Emergency lubrication device (1) with simplified architecture of a mechanical system (10), said emergency lubrication device (1) being provided with a reservoir (2), a triggering means (3) at least one pipe (4) and at least one dispensing means (5), said tank (2) containing a lubricating liquid and said triggering means (3) allowing a circulation of said lubricating liquid between said reservoir (2) and each distribution means (5) in the event of detection of a malfunction of the main lubricating means (20) of said mechanical system (10), characterized in that said reservoir (2) is arranged above said pipes (4) and said distribution means (5) so that said lubricating liquid circulates under the action of earth gravity from said reservoir (2) in each pipe (4) and each distribution means (5), each distribution means (5) comprising the self ns a restriction means (6) for limiting the flow of said lubricating liquid at each dispensing means (5) and being arranged inside said mechanical system (10), each line (4) feeding each means of dispensing (5) being arranged at least partially inside said mechanical system (10), said lubricating liquid circulating in each pipe (4) and in each dispensing means (5) thus being heated by said mechanical system (10) and the viscosity of said lubricating liquid decreasing due to a malfunction of said main lubricating means (20) so that a flow rate of said lubricating liquid at each dispensing means (5) is substantially equal to or greater than a minimum flow rate as long as said reservoir contains said lubricating liquid.
    [2" id="c-fr-0002]
    2. Emergency lubrication device (1) according to claim 1, characterized in that said reservoir (2) is arranged inside said mechanical system (10).
    [3" id="c-fr-0003]
    3. Emergency lubrication device (1) according to any one of claims 1 to 2, characterized in that the height H1 of said lubricating liquid in said reservoir (2) is less than the distance H21, H22 between said reservoir ( 2) and each distribution means (5), said height H1 and said distance H21, H22 being defined in the direction of gravity.
    [4" id="c-fr-0004]
    4. Emergency lubrication device (1) according to claim 3, characterized in that said height H1 and said distance H21, H22 are initially defined so that the decrease of said height H1, when said relief lubrication device (1) lubricates said mechanical system (10), and said decrease in said viscosity of said lubricating liquid makes it possible to have said flow rate of said lubricating liquid at each dispensing means (5) substantially equal to or greater than said minimum flow rate as long as said reservoir contains said lubricating liquid.
    [5" id="c-fr-0005]
    5. Emergency lubrication device (1) according to any one of claims 1 to 4, characterized in that said triggering means (3) comprises a first valve (31) for communicating said reservoir (2) and each pipe (4).
    [6" id="c-fr-0006]
    6. Emergency lubrication device (1) according to any one of claims 1 to 4, characterized in that said triggering means (3) comprises a plurality of first valves (31) positioned at each distribution means (5) .
    [7" id="c-fr-0007]
    7. Emergency lubrication device (1) according to any one of claims 1 to 6, characterized in that said triggering means (3) comprises a second valve (32) for venting said reservoir (2). ), said reservoir (2) being closed and sealed.
    [8" id="c-fr-0008]
    8. Emergency lubrication device (1) according to any one of claims 1 to 7, characterized in that each restriction means (6) comprises an orifice whose first diameter is greater than or equal to a second minimum value in order to avoid coking of said lubricating liquid.
    [9" id="c-fr-0009]
    9. Emergency lubrication device (1) according to claim 8, characterized in that said second minimum value is between 0.3 mm and 1.0 mm.
    [10" id="c-fr-0010]
    10. Emergency lubrication device (1) according to any one of claims 1 to 9, characterized in that each pipe (4) has a second diameter greater than or equal to a first minimum value to allow sufficient heating of said liquid lubrication.
    [11" id="c-fr-0011]
    11. Emergency lubrication device (1) according to claim 10, characterized in that said first minimum value is between 6 mm and 10 mm.
    [12" id="c-fr-0012]
    12. Emergency lubrication device (1) according to any one of claims 1 to 11, characterized in that said minimum flow rate is equal to the flow rate of said lowest lubricating liquid at each distribution means (5) at starting said emergency lubricating device (1).
    [13" id="c-fr-0013]
    13. Emergency lubrication device (1) according to any one of claims 1 to 12, characterized in that said tripping means (3) is electrically controlled.
    [14" id="c-fr-0014]
    14. Emergency lubrication device (1) according to any one of claims 1 to 12, characterized in that said triggering means (3) is pyrotechnically controlled.
    [15" id="c-fr-0015]
    15. Emergency lubrication device (1) according to claim 14, characterized in that, said triggering means (3) and said reservoir (2) being in said mechanical system (10), said pyrotechnic control is thermal triggering obtained as soon as the temperature of said triggering means (3) reaches a predetermined threshold.
    [16" id="c-fr-0016]
    16. Main power transmission gearbox for a rotary wing aircraft, characterized in that said main power transmission gearbox is provided with an emergency lubricating device (1) according to any one of claims 1 to 15 said mechanical system (10) being said main power transmission gearbox.
    类似技术:
    公开号 | 公开日 | 专利标题
    EP3181951B1|2018-08-15|Backup lubrication device with simplified architecture for a main power-transmission gearbox of an aircraft
    EP3015743B1|2017-05-24|A triple circuit lubrication device with increased reliability for a main power transmission gearbox of an aircraft
    EP3021030B1|2017-03-22|A dual circuit lubrication method and device with increased reliability for a main power transmission gearbox of an aircraft
    WO2014037652A2|2014-03-13|Speed-reducing unit having an epicyclic gear train, in particular for a turbine engine
    CA2762767C|2013-06-04|Shock absorber and landing gear provided with such a shock absorber
    EP3247924A1|2017-11-29|Integration of a pump on a pinion shank
    EP3084187B1|2020-02-26|Fluid-draining device for an aircraft engine
    EP2643069B1|2016-02-03|Oil discharge device and turbomachine comprising such a device
    FR2685758A1|1993-07-02|System for emergency lubrication and cooling of a mechanical stepup/stepdown gearing of the "transmission box" type for a helicopter in the event of failure of the lubrication circuit
    FR2500578A1|1982-08-27|DUAL-FUNCTION NOZZLE FOR OIL FOG BACKUP LUBRICATION
    FR3020093A1|2015-10-23|LUBRICANT STORAGE DEVICE FOR A LUBRICATION CIRCUIT OF AN AIRCRAFT ENGINE
    US20210246834A1|2021-08-12|Assembly for aircraft turbine engine comprising an improved system for lubricating a fan drive reduction gear in case of autorotation of the fan
    FR3075875B1|2019-11-15|OIL CIRCUIT FOR AUXILIARY OIL RING TURBOMACHINE
    FR3083266A1|2020-01-03|ASSEMBLY FOR AN AIRCRAFT TURBOMACHINE COMPRISING AN IMPROVED LUBRICATION SYSTEM OF A BLOWER DRIVE REDUCER IN THE EVENT OF A BLOWER AUTOROTATION
    FR3083283A1|2020-01-03|LUBRICATION SYSTEM FOR AN AIRCRAFT MAIN POWER TRANSMISSION WITH IMPROVED METAL PARTICLE SENSING AND DETECTION DEVICE
    EP3601765B1|2021-02-17|Improved device for temporarily increasing turbomachine power
    EP3943783A1|2022-01-26|Method for monitoring a fluid system lubricating a mechanical system
    CA2977151C|2019-06-11|Lubrication device equipped with recovery reservoirs for the lubricating liquid and optimized and dependable delivery means towards a main reservoir
    FR3013075A1|2015-05-15|JET PUMP OIL SUPPLY SYSTEM
    FR3108952A1|2021-10-08|AIRCRAFT TURBOMACHINE ASSEMBLY INCLUDING AN IMPROVED BLOWER DRIVE REDUCER LUBRICATION SYSTEM
    FR3101666A1|2021-04-09|Turbomachine oil circuit including a relief valve
    FR3088956A1|2020-05-29|LUBRICATION SYSTEM FOR AN AIRCRAFT TURBOMACHINE, INCLUDING IMPROVED LEAKAGE DETECTION MEANS
    FR3108936A1|2021-10-08|Turbomachine assembly comprising a lubrication pump
    FR2977277A1|2013-01-04|Circuit for supplying oil to rolling bearing of twin spool turboshaft engine, has alarm varying unit varying alarm threshold according to engine speed from measurement of oil pressure, and for triggering alarm
    EP0291370A1|1988-11-17|Supervisory device for the pressure of an oil pump driven by the transmission of an automotive vehicle
    同族专利:
    公开号 | 公开日
    FR3045764B1|2017-12-22|
    US20170175875A1|2017-06-22|
    US10415692B2|2019-09-17|
    EP3181951A1|2017-06-21|
    EP3181951B1|2018-08-15|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    FR2685758A1|1991-12-26|1993-07-02|Aerospatiale|System for emergency lubrication and cooling of a mechanical stepup/stepdown gearing of the "transmission box" type for a helicopter in the event of failure of the lubrication circuit|
    FR2826094A1|2001-06-15|2002-12-20|Eurocopter France|Lubricating and cooling system for transmission box comprises principal and auxiliary safety devices, and lubricating and cooling liquid reservoir and pressurized gas source supplying spray nozzles|
    US20070261922A1|2006-01-05|2007-11-15|Sikorsky Aircraft Corporation|Secondary lubrication system with injectable additive|EP3943783A1|2020-07-21|2022-01-26|Airbus Helicopters|Method for monitoring a fluid system lubricating a mechanical system|FR2658577B1|1990-02-20|1995-01-20|Aerospatiale|
    US5176174A|1991-08-09|1993-01-05|General Electric Company|Flow metering and distribution devices|
    US6793042B2|2002-07-24|2004-09-21|Pratt & Whitney Canada Corp.|Dual independent tank and oil system with single port filling|
    FR2911168B1|2007-01-10|2009-04-10|Snpe Materiaux Energetiques Sa|METHOD AND PYROTECHNIC DEVICE, INDEPENDENT, FOR INJECTING A FLUID|
    AT533929T|2007-01-19|2011-12-15|Sikorsky Aircraft Corp|LOL EXTENDED LOL LUBRICANT LUBRICANT|
    US8230835B2|2009-03-10|2012-07-31|Honeywell International Inc.|Emergency engine lubrication systems and methods|
    US9458923B2|2011-03-31|2016-10-04|Textron Innovations Inc.|Gearbox with passive lubrication system|
    US8651240B1|2012-12-24|2014-02-18|United Technologies Corporation|Pressurized reserve lubrication system for a gas turbine engine|DE102014016173A1|2014-11-03|2016-05-04|Audi Ag|Drive device for a motor vehicle|
    US10746284B2|2015-04-21|2020-08-18|Sikorsky Aircraft Corporation|Gearbox lubrication system for aircraft|
    FR3037355B1|2015-06-11|2017-05-19|Airbus Helicopters|TRANSMISSION BOX OF POWER AND AIRCRAFT|
    EP3332103A4|2015-08-07|2019-01-02|Sikorsky Aircraft Corporation|Lubrication systems for transmissions|
    JP6545217B2|2017-03-24|2019-07-17|本田技研工業株式会社|Lubricating fluid supply structure of power transmission device|
    JP6846301B2|2017-06-27|2021-03-24|川崎重工業株式会社|Power transmission device for helicopters|
    JP6929143B2|2017-06-27|2021-09-01|川崎重工業株式会社|Lubrication 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|
    JP2020045042A|2018-09-21|2020-03-26|川崎重工業株式会社|Transmission lubrication structure for helicopter|
    DE102019126914A1|2019-10-08|2021-04-08|Audi Ag|Lubricant supply system for a drive device of an electrically operated vehicle|
    EP3835623B1|2019-12-12|2022-03-16|FCA Italy S.p.A.|Gear transmission unit with a forced lubrication system including one or more lubricant distribution boxes|
    法律状态:
    2016-12-22| PLFP| Fee payment|Year of fee payment: 2 |
    2017-06-23| PLSC| Publication of the preliminary search report|Effective date: 20170623 |
    2017-12-21| PLFP| Fee payment|Year of fee payment: 3 |
    2018-12-19| PLFP| Fee payment|Year of fee payment: 4 |
    2020-10-16| ST| Notification of lapse|Effective date: 20200910 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1502623A|FR3045764B1|2015-12-17|2015-12-17|SIMPLIFIED ARCHITECTURE BACKUP LUBRICATION DEVICE FOR A MAIN POWER TRANSMISSION BOX OF AN AIRCRAFT|FR1502623A| FR3045764B1|2015-12-17|2015-12-17|SIMPLIFIED ARCHITECTURE BACKUP LUBRICATION DEVICE FOR A MAIN POWER TRANSMISSION BOX OF AN AIRCRAFT|
    EP16197779.8A| EP3181951B1|2015-12-17|2016-11-08|Backup lubrication device with simplified architecture for a main power-transmission gearbox of an aircraft|
    US15/372,634| US10415692B2|2015-12-17|2016-12-08|Emergency lubrication device of simplified architecture for a power transmission main gearbox of an aircraft|
    [返回顶部]