• 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:
    A gear pump (4 ') operates to provide a determined flow rate, but with little or no pressure rise. In order to ensure the hydrodynamic lift of bearings (19) of the supports of the pinions (11), or of some of them, it is planned to add a seal (46) between them, in order to define a cavity close (47), to ensure the lift by a more viscous fluid and therefore more conducive, instead of doing it by the fluid itself which is pumped. Possible application to aircraft engine fuel pumps, where the pump (4 ') is a high pressure pump associated with a low pressure pump.
    公开号:FR3019856A1
    申请号:FR1453372
    申请日:2014-04-15
    公开日:2015-10-16
    发明作者:Philippe Vertenoeuil；Bellal Waissi
    申请人:SNECMA SAS；
    IPC主号:
    专利说明:

    [0001] A subject of the present invention is a gear pump provided in particular as a high-pressure fuel pump. Aircraft engines include a main fuel pump, which is at the heart of their control system. It provides fuel to the combustion chamber, pumping the flow required from the tanks. It also uses the flow it delivers as a hydraulic fluid to actuate cylinders, such as those used to open the discharge doors of the flow of air from the primary vein to the secondary vein of the engine. This pump comprises two stages, a low pressure pump and a high pressure pump, to which more specifically the invention. These two stages have a distinct function: the first delivers a fixed-rate pressure rise, the second a flow with a fixed pressure difference across it. These two stages are most often integrated in the same housing, for reasons of space saving and simplification of the engine, and constitute a single equipment, driven at the same speed by the same tree. The most widely used technology for the low pressure stage is a centrifugal pump with a blown wheel. Such a pump has pressure elevation characteristics which strongly depend on the rotational speed. The most commonly used technology for the high pressure stage is a fixed displacement gear pump. Its flow rate is therefore proportional to its rotational speed, with the volume yield close. This technology, used for its high reliability, implies an excess of pumped flow at certain flight regimes, where the rotational speed is high when there is no longer any need for flow, nor towards the injection into the chamber. combustion, nor to the actuators. This excess flow is then returned upstream of the high pressure pump.
    [0002] New engine developments often aim to reduce fuel consumption by reducing all energy losses. It is thus sought to greatly reduce the pressure difference across the high pressure pump, or even to cancel, thus relying only on the low pressure pump to ensure the necessary pressure rise. The high pressure pump would only serve to ensure the desired flow rate. The expected savings would consist on the one hand in a reduction of power necessary to drive the pump shaft, and on the other hand in a simplification of the pump, including in particular a reduction of the cubic capacity, since the decrease, or the suppression the elevation of pressure of which it is the seat, will inevitably diminish the leaks within it. Despite these advantages due to the reduction or the elimination of the pressure difference, the high-pressure gear pumps will have to receive some design modifications, which are the subject of the invention, since this pressure difference between the inlet and the output of the pump is operated to ensure its proper operation, as will now be detailed. According to a first aspect of the invention, this generally relates to a gear pump, comprising a housing, two gears meshing with each other in a chamber of the housing, two first bearings, respectively supporting first ends of axes. gears, two second bearings, respectively supporting second ends of axes of the gears, the first bearings and the second bearings being housed in the chamber of the housing, the first ends of axes journalled in the first bearings with first games and the second ends of axes journalled in the second bearings with second sets, the first and second sets receiving layers of hydrodynamic support fluid, characterized in that it comprises seals between the second bearings and the pinions, insulating closed cavities including the second clearances and delimited by the housing, the second bearings, the gables, closed cavities receiving a different fluid a fluid pumped by the gears. The fluid of the closed cavities may be rheo-thickening. According to a second aspect of the invention, springs are compressed between the casing and external axial faces, remote from the gears, second bearings; the springs extend on opposite portions of the circumference of said faces and thus exert a resultant of greater efforts to thereby strengthen pinching of the gears between their bearings, essential to reduce recirculation leakage within the pump.
    [0003] According to a third aspect of the invention, the casing comprises tappings communicating the first games and the outside of the casing, to further ensure the lubrication of the first bearings despite the absence of pressure at the terminals of the pump. The invention will now be described in detail by means of the following figures: FIG. 1 is a general view of the device; Figures 2, 3, 4, 5 and 6 are various views of the high pressure pump that the invention improves; FIG. 7 illustrates a first characteristic modification of the invention; FIGS. 8A, 8B, 8C, 8D and 9 explain the interest of this modification; and FIGS. 10 and 11 illustrate other characteristic modifications of the invention.
    [0004] We now use the description of the first figures. Figure 1 shows the fuel system of the engine. A tank 1 of an aircraft feeds a low pressure pump 2, then, by filters and exchangers 3, a high pressure pump 4. The pressurized fuel is supplied to a metering device 5, which feeds a combustion chamber 6 actuators and servo valves 7; the excess flow returns upstream of the high pressure pump 4 by a return line 8, and likewise the fluid used in the actuators and servo valves 7. Figures 2 and 3 are now commented. Figure 2 illustrates, in perspective, the essential portions of the known high pressure pump 4 and that the invention is to improve, and Figure 3 is a general plan of the device. The high pressure pump 4 is a gear pump, comprising a driving pinion 11 and a driven pinion 12, meshing together and driving fuel between their teeth to complete the pumping. Each of the pinions 11 and 12 comprises tails or ends of axes 13, 14 and 15, 16 at its two opposite sides, the first of which, to the right of FIGS. 2 and 3, are supported by respective first bearings 17, 18 said fixed bearings with first sets 9, and the second, left in the figures, are supported by second bearings, said movable bearings 19, 20 with second sets 10. These bearings 17 to 20 are all plain bearings, but the fixed bearings 17 and 18 are retained with a smaller clearance in housings of a housing 24 than the movable bearings 19 and 20, which can thus move axially to pinch the gears 11 and 12 and reduce games that could allow recirculation of the fluid pumped to low pressures. The drive gear 11 is driven by a high pressure shaft 21, and a low pressure shaft 22 drives the impeller 23 of the low pressure pump 2. The pumps 2 and 4 are both integrated in the housing 24 common. The low-pressure shaft 22 is supported by an additional bearing 25 in a bore of the housing 24.
    [0005] Stops 26 limit the axial movements of the wheel 23, relying on the bearing 25. The movement of the drive shaft 21 is communicated to the low-pressure shaft 22 by means of splines 27 between the pinion leading 11 and the ends of the shafts 21 and 22. A coupling of the pumps 2 and 4 is thus obtained. The proper functioning of the high pressure pump 4 depends on a sufficient seal between its various elements: it is necessary to avoid leakage of the pumped fluid to the outside of the casing 24, as well as around the gears 11 and 12, in recirculation to the inlet of the pump 4. The housing 24 is open at 28 around the inlet of the high-pressure shaft 21. A seal 29 is disposed at this point between the housing 24 and the end of the housing. adjacent axis, to eliminate leakage to the outside. Leaks for recirculation around the pinions 11 and 12 are minimized first by means of springs 30 compressed between the movable bearings 19 and 20 and a face 31 of the casing 24, adjacent to the inlet of the high-pressure shaft 21, in order to push the movable bearings 19 and 20 towards the pinions 11 and 12, and these towards the fixed bearings 17 and 18, thus decreasing the clearances 32 around the pinions 11 and 12 and producing the pinch already mentioned; and by means of constructional features of the bearings 17 to 20 which will be described with Figures 4 and 5. The friction between the bearings 17 to 20 and the pinions 11 and 12 are avoided by fluid layers, maintained hydrodynamically. Each of the bearings 17 to 20 is hollowed out with several reliefs, including a high pressure pool 33 and a low pressure pool 34 at the periphery of an inner axial face 35, on either side of a partition wall 60 The tanks 33 and 34 are respectively in communication with the volumes of fluids adjacent to the outlet and the inlet of the pump 4. The high-pressure pool 33 communicates with a high-pressure arc groove 36, which opens onto the inner axial face 35, and, through a bore not shown, a high pressure groove 37, which opens into an inner radial face 38 of the bearing 17 to 20. A low pressure groove 39 extends to the junction of the inner axial face 35 of the inner radial face 38 and communicates with the low pressure pool 34, by a collecting groove 40. In the bearings 17 to 20 constructed in this way, the operation of the pump thus maintains a circulation of fluid s ervant to the dynamic lubrication of the bearings 17 to 20, from the high pressure pool 33 to the low pressure pool 34, creating hydrodynamic layers on the inner axial face 35 and the inner radial face 38. The ends of axes 13 to 17 are therefore supported by these hydrodynamic layers in the inner radial faces 38, which occupy the sets 9 and 10, and the hydrodynamic layers on the inner axial faces 35 are formed against the flanks of the gears 11 and 12, holding them slightly separated from the bearings 17 to 20 and thus preventing the complete elimination of the games 32, despite the springs 30. As shown in FIG. 5, the movable bearings 19 and 20 still have, in their known construction, a construction feature on their face. external axial, remote from the pinions 11 and 12 and carrying springs 30: this face is divided into two portions in the form of croissants 42 and 43, which are located in planes di fferents, separated by a shoulder provided with a seal 45 (visible in Figure 6) for exposing the crescent 42 to the high pressure of the fluid and the crescent 43 at low pressure (despite pressure losses ): the resulting thrust in the axial direction is unbalanced and comprises a movement about a transverse axis of the movable bearings 19 and 20, in order to balance an opposite movement produced by the pressure differences of the pumped fluid on the inner axial faces 35; no tilting of the movable bearings 19 and 20 around this transverse axis is therefore produced, so that they remain well coaxial with the ends of axes 15 and 16 that they support despite the mounting sets of the movable bearings 19 and 20 in the housing 24. The movable bearings 19 and 20 are retained, at the location of the shoulder separating the crescents 42 and 43, in bores 44 of the housing 24, eccentric with respect to the axes of rotation of the gears 11 and 12. The springs 30 can be installed only where the crescent 42 is the widest, about a quarter of circumference about the movable bearings 19 and 20. Finally, the pressure difference between the inlet and the outlet of the pump exerts a radial resultant on the pinions 11 and 12, which approaches the housing 24 to an inlet side of the fluid.
    [0006] Thus, the chamber of the casing 24, occupied by the pinions 11 and 12 and the bearings 17 to 20, is the seat of very small leaks both outwards and around the different surfaces of the pinions 11 and 12, and allows a This is due primarily to the differential pressure forces on the movable elements inside the housing 24 which are the pinions 11 and 12 and the movable bearings 19 and 20, since these forces of Differential pressures maintain the hydrodynamic support layers of the ends of axes 13 to 16 and the pinching of the gears 11 and 12 between the bearings 17 to 20 with reduced clearances 32; the springs 30 which also contribute to this pinch are however only useful at the start of the pump 4, when no pressure difference is still created, since the forces they produce are then too low to exert a real influence. We now move to the modifications made in connection with the invention. The modified high pressure pump will be referenced by 4 '. Referring to Fig. 7, firstly, a second seal 46 has been added between the movable bearing 19 and the drive gear 11 so as to interrupt the axial clearance 32 at this point. The second seal 46 consists of a housing containing a spring which pushes a sealing lip: the housing is here in a housing of the movable bearing 19, and the lip rubs against an ice of the pinion 11. Without represents the arrangement, since it is similar, a similar seal is disposed at a corresponding location, between the movable bearing 20 and the driven pinion 12. It is seen that a closed cavity 47 is formed, defined by the housing 24, the movable bearing 19 or 20, the packing 46, the pinion 11 or 12, the end of axis 15 or 16, and a flange 48, belonging to the housing 24, and used to insert the seal 29. In the case of the movable bearing 20 and the driven pinion 12, it is the same in the absence of the gasket 29 and the flange 48, since the housing 24 is continuous at this location. This is why closed cavities 47 have been created. A relatively large radial clearance exists between the ends of the axes 15 and 16 and the movable bearings 19 and 20, the rest arrangement being shown in FIG. 8A, where the ends of the axes 15 and 16 are placed at the bottom of the faces. As the high-pressure pump 4 'is turned on, a hydrodynamic wedge 49 is created on the axle end 15 or 16 (FIG. 8B), detaching it completely from the inner radial face 38 when the rotational speed is sufficient (Figure 8C), and the axis end 15 or 16 is at the center of the movable bearing 19 or 20 at high speed, the hydrodynamic wedge has been replaced by a layer of uniform thickness (Figure 8D). The formation of this corner 49 and this layer 50 however depends on the properties of the fluid: it is easily formed under high pressure, but not otherwise with the most usual fluids (Newtonians), such as fuels. However, the pressure difference of the layer 50 no longer exists with the invention, where the fluid remains at approximately the same pressure between the inlet and the outlet of the high-pressure pump 4 '.
    [0007] This is why we no longer use the pumped fluid for the formation and maintenance of the hydrodynamic layer 50, but to a particular fluid, which is therefore injected into the closed cavities 47 beforehand: a non-Newtonian fluid called rheo-thickener that is to say whose viscosity increases as a function of the shear rate. As indicated in FIG. 9, where the shear rates are on the abscissa and the shear stresses are on the ordinate, the Newtonian fluids follow a line 51 whose slope (the viscosity of the fluid) is constant, whatever the shear rate. The rheo-thickening fluids, for their part, follow a curve 52, whose slope becomes stronger and stronger, as the shear rate increases and therefore have an increasing viscosity, when they are subjected to shearing. . Such fluids include, for example, oils loaded with impurities, such as organic fibers. Their viscosity, greater when the shear rates are high, allows them to easily give the hydrodynamic lift. However, these conditions of high shear rates are always present in the present situation, since they exist in the hydrodynamic wedge 49 at the beginning of the rotation, where the velocity gradient is important, because of the small thickness of this wedge; and it is also important at high rotational speeds once the hydrodynamic layer 50 has been formed. It suffices to provide this particular fluid for two of the bearings 17 to 20 only, particularly the movable bearings 19 and 20, the fixed bearings 17 and 18 continuing to benefit from the lift by the pumped fluid.
    [0008] Referring to Figure 10, to expand the explanation of another aspect of the invention. The pinching force of the pinions 11 and 12 in the axial direction may become insufficient in the absence of overpressure. This is remedied by arranging additional springs 30 similar to the previous ones, in as many new cells 41 ', established on a sector of the circumference of the movable bearing 19 or 20 opposite in sector receiving the cells 40. This involves modifying the eccentric bore 44, concentric with the axis of the bearing 19 or 20. The portions 42 'and 43' subjected to the high pressure and the low pressure of the outer axial face of the movable bearings 19 and 20 are replaced by a bore 44 '. are now concentric. It should be noted that the elimination of the hydraulic clamping forces within the pump 4, following the absence of pressure difference between the inlet and the outlet of the pump 4, is no longer harmful and that the leaks remain unimportant, precisely because the pressure difference that arouses them no longer exists. However, it is still necessary to ensure a lubrication flow of the ends of the axes 13 and 14 in the fixed bearings 17 and 18 through the first sets 9, to allow a fluid inlet then forming the hydrodynamic lift, in place of non-Newtonian fluid closed cavities 47, absent fixed bearings 17 and 18. This function is provided conventionally by forming a recirculation flow between a region of the inner axial faces 35 exposed to the high pressure and a region of the outer axial faces exposed to the low pressure, through the games 9. It is carried out here, according to a third important aspect of the invention, shown in Figure 11, by arranging a pipe 53 between a tapping 54 of the housing 24, the side of the outer axial faces fixed bearings 17 and 18, remote from the pinions 11 and 12, and a point of the circuit upstream of the high pressure pump 4 ', subjected to a lower pressure, for example the upstream of a booster pump 62 that can be added to the device downstream of the low pressure pump 2 to supplement the pressure rise provided by the high pressure pump 4 known. This booster pump 62 is located for example upstream of the filter 55 of the filters and exchangers 3. The fluid conduit successively passing through the low pressure pump 2, the booster pump 62, and the high pressure pump 4 'carries the reference 63.
    [0009] According to the invention, the high pressure pump 4 'delivers only a flow, but without adding substantially additional pressure, which is ensured by the addition of a return valve 56, mounted on a pipe 57, connecting the inlet and the outlet of the high-pressure pump 4 ', preventing the formation of a pressure between them.
    权利要求:
    Claims (10)
    [0001]
    CLAIMS1) Gear pump (4 '), comprising a housing (24), two pinions (11, 12) meshing with each other in a chamber of the housing, two first bearings (17, 18) respectively supporting first ends of axes (13, 14) of the gears, two second bearings (19, 20), respectively supporting second pin ends (15, 16) of the gears, the first bearings and the second bearings being housed in the housing chamber, the first ends of axes journalled in the first bearings (17, 18) with first sets (9) and the second ends of axes journalled in the second bearings (19, 20) with second sets (10), the first and the second second sets accommodating layers of hydrodynamic support fluid, characterized in that it comprises sealing gaskets (46) between the second bearings (19, 20) and the gears (11, 12), said gaskets insulating the closed cavities (47) encompassing the second sets (10) and delimited by the housing (24), the second ones gears (19, 20) and the gears (11, 12), the closed cavities receiving a fluid different from a fluid pumped by the gears.
    [0002]
    2) Gear pump according to claim 1, characterized in that the fluid of the closed cavities (47) is rheo-thickening.
    [0003]
    3) Gear pump according to any one of claims 1 or 2, characterized in that the housing comprises connections (54) connecting the first games (9) and the outside of the housing (24).
    [0004]
    4) Gear pump according to any one of claims 1 to 3, wherein springs (30) are compressed between the housing (24) and outer axial faces, remote gears, second bearings, characterized in that the springs extend over opposite sectors of circumference of said faces.
    [0005]
    5) Gear pump according to any one of claims 1 to 4, characterized in that it is coupled to another pump (2), also included in the housing (24), the gear pump and said other pump having drive shafts (21, 22) interconnected.
    [0006]
    6) A gear pump according to claim 5, characterized in that it is a high-pressure fuel pump, said other pump being a low-pressure fuel pump, having a fuel outlet connected to a fuel inlet of the pump with gears by a fluid circuit.
    [0007]
    7) Gear pump according to claims 3 and 6, characterized in that the connections (54) are connected to the fluid circuit between said fuel outlet and said fuel inlet, through a pipe (53) of the fluid.
    [0008]
    8) Gear pump according to any one of claims 6 or 7, characterized in that it comprises a pressure relief device (56, 57) between the inlet and the outlet of the fuel of the high-pressure pump. pressure (4 ').
    [0009]
    9) A pump device comprising a gear pump (4 ') according to any one of claims 1, 2, 3 or 4, the gear pump being a high pressure pump, the device further comprising a low pressure pump ( 2), and a conduit (63) of fluid passing through the low pressure pump (2) and the high pressure pump (4 ').
    [0010]
    10) A pumping device according to claim 9, characterized in that it further comprises a booster pump (62), through which the duct (63) passes downstream of the low pressure pump (2), the casing ( 24) comprising tappings (54) communicating the first sets (9) and the outside of the housing (24), and the connections being connected to a pipe (53) terminating in the conduit (63) upstream of the booster pump (62) .20
    类似技术:
    公开号 | 公开日 | 专利标题
    CA2945890C|2021-12-14|Fuel gear pump intended, in particular, as a high-pressure pump
    CA2719472C|2016-09-13|Device and method for balancing pressure in a turbojet bearing housing
    EP1559913A1|2005-08-03|Progressive cavity pump
    RU2681824C2|2019-03-12|Transmission assembly including transmission member and oil distribution system
    FR3017413A1|2015-08-14|TURBOMACHINE EQUIPPED WITH A LUBRICATION GROUP.
    EP3430243B1|2021-01-06|Turbojet engine comprising a simplified bearing lubrication assembly
    FR2913061A1|2008-08-29|SHEATHING SYSTEM FOR AN AIRCRAFT ENGINE.
    FR2525697A1|1983-10-28|TWO STAGE VOLUMETRIC PUMP FOR LIQUEFIED LIQUID PHASE OIL GASES, AND FUEL INJECTION METHOD FOR MOTOR VEHICLE ENGINE USING SUCH PUMP
    FR3022951A1|2016-01-01|TWO-STAGE PUMP, ESPECIALLY PROVIDED AS THE MAIN PUMP FOR FEEDING A FUELED AIRCRAFT ENGINE
    FR2784143A1|2000-04-07|VOLUMETRIC FUEL PUMP WITH CAVITATION NOISE REDUCTION
    EP0494008B1|1995-08-23|Turbopump with axial throughflow booster
    FR2528918A1|1983-12-23|SEALING DEVICE FOR A SHAFT IN A CENTRIFUGAL PUMP AND METHOD FOR THE USE OF THIS DEVICE
    EP1972798B1|2009-12-09|Device for controlling the position of an actuator by a servo-valve with position memory in the event of a breakdown
    FR3039224B1|2019-08-30|ENHANCED GEAR PUMP WITH IMPROVED HYDRODYNAMIC BEARING
    EP1473462B1|2006-01-25|Cartridge compressor unit
    WO2021005315A1|2021-01-14|Recirculation of lubricant in a turbomachine rolling-element bearing
    FR3106630A1|2021-07-30|Dry vacuum pump
    FR3098258A1|2021-01-08|Tilting gear pump for turbomachines, which can be incorporated into an aircraft engine lubrication circuit
    EP0043881A1|1982-01-20|Rotary hydraulic converting and distributing device with multiple synchronized cylinders
    FR2906849A3|2008-04-11|Vane pump for engine of motor vehicle, has inner ring inserted between inner wall of guiding ring and outer surface of wall of housing for defining pumping stage that is formed by three chambers along direction of vanes rotating direction
    FR2634828A1|1990-02-02|CENTRIFUGAL COMPRESSOR WITH SEALING OIL RESERVOIR
    BE483670A|
    BE537755A|
    BE538835A|
    同族专利:
    公开号 | 公开日
    RU2016144149A|2018-05-16|
    WO2015159018A1|2015-10-22|
    US10094291B2|2018-10-09|
    CN106415011A|2017-02-15|
    CN106415011B|2019-03-01|
    BR112016023339A2|2017-12-12|
    RU2016144149A3|2018-08-21|
    EP3132123A1|2017-02-22|
    CA2945890A1|2015-10-22|
    FR3019856B1|2019-05-31|
    EP3132123B1|2020-09-09|
    RU2680902C2|2019-02-28|
    CA2945890C|2021-12-14|
    US20170044986A1|2017-02-16|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US3528756A|1968-12-04|1970-09-15|Borg Warner|Pressure loaded pump|
    US3574492A|1969-09-26|1971-04-13|Gen Signal Corp|Bushing arrangement for rotary shafts|
    US4787332A|1986-02-12|1988-11-29|Robotics, Inc.|Adhesive dispensing pump control system|
    US20140003987A1|2009-04-16|2014-01-02|Simon Martin-Dye|Aircraft main engine fuel pump with multiple gear stages using shared journals|
    US2891483A|1956-04-13|1959-06-23|Thompson Ramo Wooldridge Inc|Movable bushing for pressure loaded gear pumps|
    BE625348A|1961-12-11|
    DD159097A1|1981-05-25|1983-02-16|Gerhard Willner|HYDROSTATIC GEARING MACHINE|
    US5417556A|1994-03-08|1995-05-23|Alliedsignal Inc.|Bearing for gear pump|
    US5641281A|1995-11-20|1997-06-24|Lci Corporation|Lubricating means for a gear pump|
    RU2395719C1|2008-12-29|2010-07-27|Государственное образовательное учреждение высшего профессионального образования "Братский государственный университет"|Gear pump with pressure lubrication of plain bearings|
    JP5984534B2|2012-07-02|2016-09-06|日立オートモティブシステムズ株式会社|Pump device|
    CN202746190U|2012-07-03|2013-02-20|泊姆克液压有限公司|High-pressure gear pump|
    FR2995053B1|2012-09-03|2016-03-04|Snecma|TURBOMACHINE MOVEMENT GEAR BOX COMPRISING A GEAR-LINKED CINEMA CHAIN EXTENDING IN NON-PARALLEL PLANS|
    FR3022951B1|2014-06-26|2020-01-24|Safran Aircraft Engines|TWO-STAGE PUMP, ESPECIALLY PROVIDED AS A MAIN PUMP FOR SUPPLYING AN AIRCRAFT ENGINE WITH FUEL|FR3036137B1|2015-05-13|2017-06-02|Snecma|COMPRESSOR PRESSURE DISCHARGE VALVE VALVE FOR AIRCRAFT TURBOMACHINE|
    FR3059718B1|2016-12-02|2019-06-21|Safran Aircraft Engines|HYDROMECHANICAL HYSTERESIS CUTTING DEVICE FOR TURBOMACHINE LUBRICATION SYSTEM|
    CN110685806A|2019-11-06|2020-01-14|四川航天中天动力装备有限责任公司|Sliding bearing structure for oil supply mechanism of turbojet engine|
    RU195531U1|2019-11-18|2020-01-30|Акционерное общество "Ярославский завод дизельной аппаратуры"|FUEL SUPPLY PUMP|
    CN111765062A|2020-06-10|2020-10-13|中国航发北京航科发动机控制系统科技有限公司|High-low pressure combination formula fuel pump structure|
    法律状态:
    2016-04-14| PLFP| Fee payment|Year of fee payment: 3 |
    2017-04-06| PLFP| Fee payment|Year of fee payment: 4 |
    2018-02-09| CD| Change of name or company name|Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
    2018-03-22| PLFP| Fee payment|Year of fee payment: 5 |
    2020-03-19| PLFP| Fee payment|Year of fee payment: 7 |
    2021-03-23| PLFP| Fee payment|Year of fee payment: 8 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1453372A|FR3019856B1|2014-04-15|2014-04-15|GEAR PUMP, ESPECIALLY PROVIDED AS A HIGH-PRESSURE FUEL PUMP|
    FR1453372|2014-04-15|FR1453372A| FR3019856B1|2014-04-15|2014-04-15|GEAR PUMP, ESPECIALLY PROVIDED AS A HIGH-PRESSURE FUEL PUMP|
    RU2016144149A| RU2680902C2|2014-04-15|2015-04-14|Gear pump and pumping device|
    US15/304,212| US10094291B2|2014-04-15|2015-04-14|Gear pump intended, in particular, as a high pressure fuel pump|
    EP15720387.8A| EP3132123B1|2014-04-15|2015-04-14|Fuel gear pump intended, in particular, as a high-pressure pump|
    PCT/FR2015/051001| WO2015159018A1|2014-04-15|2015-04-14|Fuel gear pump intended, in particular, as a high-pressure pump|
    CA2945890A| CA2945890C|2014-04-15|2015-04-14|Fuel gear pump intended, in particular, as a high-pressure pump|
    CN201580020343.7A| CN106415011B|2014-04-15|2015-04-14|Gear petrolift|
    BR112016023339A| BR112016023339A2|2014-04-15|2015-04-14|fuel-driven pump, notably intended as a high-pressure pump|
    [返回顶部]