EP4452753A1 - Circuit de commande hydraulique de calage d'aubes de soufflante - Google Patents
Circuit de commande hydraulique de calage d'aubes de soufflanteInfo
- Publication number
- EP4452753A1 EP4452753A1 EP22847588.5A EP22847588A EP4452753A1 EP 4452753 A1 EP4452753 A1 EP 4452753A1 EP 22847588 A EP22847588 A EP 22847588A EP 4452753 A1 EP4452753 A1 EP 4452753A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- chamber
- control
- cylinder
- pump
- chambers
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
- F04B1/12—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis
- F04B1/26—Control
- F04B1/30—Control of machines or pumps with rotary cylinder blocks
- F04B1/32—Control of machines or pumps with rotary cylinder blocks by varying the relative positions of a swash plate and a cylinder block
- F04B1/324—Control of machines or pumps with rotary cylinder blocks by varying the relative positions of a swash plate and a cylinder block by changing the inclination of the swash plate
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B1/00—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders
- F04B1/12—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis
- F04B1/20—Multi-cylinder machines or pumps characterised by number or arrangement of cylinders having cylinder axes coaxial with, or parallel or inclined to, main shaft axis having rotary cylinder block
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/002—Hydraulic systems to change the pump delivery
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B49/00—Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
- F04B49/08—Regulating by delivery pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D7/00—Rotors with blades adjustable in operation; Control thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B2211/00—Circuits for servomotor systems
- F15B2211/20—Fluid pressure source, e.g. accumulator or variable axial piston pump
- F15B2211/205—Systems with pumps
- F15B2211/2053—Type of pump
- F15B2211/20546—Type of pump variable capacity
Definitions
- TITLE HYDRAULIC FAN BLADE TIMING CONTROL CIRCUIT
- the invention relates to a system comprising a circuit for hydraulically controlling the setting of turbojet fan blades.
- a turbomachine of the unducted turbojet type, such as an "open rotor” with two counter-rotating fans or even of the USF type for "Unducted Single FAN", that is to say with a single fan followed by non-rotating blading, there is no nacelle surrounding the fan(s).
- the angle of incidence of the blades of a fan is adjustable by a pitch setting system generally making it possible to control the pitch of all the blades according to the same angle (the same pitch).
- each blade 3 then comprises a base 11 carried by a rotor element 12 rotating around the axis AX, by means of a pivot connection allowing it to pivot around an axis radial with respect to to the AX axis.
- Figure 2 schematically provides an example of a mechanism among other possibilities that can be implemented, such as connecting rod-crank type systems, so that the setting of the blades 3 depends on the longitudinal position of the central shaft 13 .
- Maintaining the shaft 13 in a given longitudinal position is ensured by means of a hydraulic transfer bearing 15 surrounding the shaft 13, by pressurizing a first chamber 17 and a second chamber 18 of this bearing 15 at different pressures.
- the shaft 13 comprises a first internal channel placing the first chamber 17 in communication with a downstream chamber 21 of a cylinder body 22 carried by the rotor element 12 being rigidly integral with this one.
- This shaft 13 also includes a second internal channel putting the second chamber 18 in communication with an upstream chamber 19 of the cylinder body 22.
- the upstream end of the shaft 13 is housed in the cylinder body 22, and it ends with a plate 23 separating the upstream chamber 19 and the downstream chamber 21 from the cylinder body 22.
- the pressure difference between the first chamber 17 and the second chamber 18 is adjusted to correspond to the force exerted by the blades 3 on the disc 14, so as to maintain the shaft 13 at a given longitudinal position, to block the blades at a given pitch value.
- a decrease or an increase in the pressure of one or the other of the chambers 17 and 18 makes it possible to move the shaft 13 upstream or downstream to modify the pitch angle of the blades, before readjusting the modified pressure to restore an equilibrium in order to maintain the blades at their new pitch angle.
- the pressurization of the chambers 17 and 18 is ensured with a hydraulic pump generating a sufficiently high nominal pressure to allow the blades to be maneuvered over their entire range of pitch angles.
- This nominal pressure which is the highest pressure of the two chambers 17 and 18, thus corresponds to the maximum force that can be exerted by the blades on the disc 14 according to all the possible operating conditions of the engine.
- the object of the invention is to provide a solution for limiting the energy loss of such a fan blade hydraulic control system.
- the subject of the invention is a hydraulic control circuit for a double slewing cylinder for slewing the fan blades of a turbojet engine, comprising an oil tank, a variable displacement axial piston pump comprising a tilting plate as well as a control chamber and a compensation chamber, the tilting of the plate being controlled by pressurizing these chambers, the pump being supplied by the reservoir and having its outlet configured to be able to be connected by a supply line supply to one of the chambers of the slewing cylinder, the other chamber of the slewing cylinder being connected to the tank, the control chamber and the compensation chamber being both pressurized with a pressure corresponding to the outlet pressure pump, the control chamber and the compensation chamber being arranged to increase the inclination of the plate in order to increase the displacement of the pump when the pressurization pressure of these chambers increases.
- the invention also relates to a circuit thus defined, comprising a control jack comprising the control chamber, and a compensation jack comprising the compensation chamber, the control jack and the compensation jack being separate.
- the invention also relates to a circuit thus defined, comprising a double-acting control and compensation actuator integrating the control chamber and the compensation chamber.
- the invention also relates to a circuit thus defined, in which the pump has its outlet connected to a distributing valve by a supply pipe, in which the compensation jack of the pump is supplied by the outlet of the pump, in which the slewing cylinder has two chambers connected to the distributing valve, in which the distributing valve can occupy a position in which it connects one of the chambers to the supply line and the other chamber to the tank, or another position in which it connects one of the chambers to the tank and the other chamber to the supply line, the circuit further comprising a selection valve connected to the two chambers of the orientation jack and to the pump control jack by via a control line to pressurize the control chamber of the pump with the highest pressure among the two chambers of the slewing cylinder.
- the invention also relates to a circuit thus defined, in which the control conduit is connected to the two chambers by additional conduits provided with restrictions, and in which the distributing valve can occupy a position in which the pump and the reservoir are isolated from the chambers of the orientation cylinder.
- the invention also relates to a circuit thus defined, comprising a purge line connecting the supply line to the tank via a non-return valve.
- the invention also relates to a circuit thus defined, comprising a purge line connecting the control line to the reservoir via a non-return valve.
- the invention also relates to a circuit thus defined, in which the control chamber incorporates a spring tending to deploy the actuator.
- the invention also relates to a turbojet engine comprising a circuit thus defined and variable-pitch fan blades which are controlled by this circuit.
- FIG 1 is a longitudinal sectional view of a known turbofan engine
- FIG 2 is a schematic view of a known hydraulic fan blade pitch adjustment system
- FIG 3 is a longitudinal section view schematically representing a variable displacement axial piston pump
- FIG 4 is a front view of a variable displacement axial piston pump distribution window
- FIG 5 is a schematic view of the control circuit according to the invention when its dispensing valve occupies a first position
- FIG 6 is a schematic view of the control circuit according to the invention when its dispensing valve occupies a second position
- FIG 7 is a schematic view of the control circuit according to the invention when its dispensing valve occupies a third position
- FIG 8 is a longitudinal sectional view of a variable displacement axial piston pump equipped with a double-acting control and compensation cylinder.
- an axial piston pump 26 comprises a drive shaft T1 which is rotated by a shaft of the turbojet that this pump equips.
- This shaft T1 rotates around an axis AP and it carries a barrel 28 to which it is rigidly secured, this barrel here carrying two pistons 29, 31.
- the piston 29 is slidably mounted in a corresponding cylindrical chamber 32 of the barrel 28 to be mobile in translation in this chamber in the direction AP.
- the piston 31 is, in the same way, slidably mounted in another cylindrical chamber 33 of the barrel 28.
- This pump also comprises a tilting plate 34 which is carried by fixed elements of the pump 26 while being capable of pivoting around an axis of rotation AR normal to the axis AP.
- the piston 29 has a free end protruding from the barrel 28 which is equipped with a ball 36 resting on the plate 34 via a pad 37.
- the piston 31 has a free end equipped with a ball 38 resting on the plate 34 via another shoe 39.
- a return spring 41 located in chamber 32 continually tends to pull piston 29 out of this chamber so that its free end is kept flat against plate 34 at all times.
- return spring 42 is arranged in chamber 33 to keep the end of piston 31 pressed against plate 34.
- This pump further comprises a distribution glass 43 attached to the face of the barrel 28 which is opposite the pistons along the axis AP.
- This glass 43 which is a fixed element of the pump, and which appears alone in FIG. 4, is crossed by the shaft T1 and comprises an oil inlet port 44 in the shape of an arc of circle extending over a little less than half a turn, and an oil discharge port 46 also extending over a little less than a half turn, being arranged diametrically opposite to the intake port 44.
- each chamber 32, 33 is terminated on the side opposite the piston it houses, by a channel passing through the barrel to be able to be placed in communication with one or the other of the slots 44, 46 of ice cream 43.
- the intake port 44 is connected to a supply oil reservoir of the pump, at atmospheric pressure, and the discharge port 46 is connected to an outlet conduit of the pump.
- each piston is deployed to draw in oil throughout the rotation phase where its chamber communicates with port 44, and it retracts to discharge pressurized oil through port 46 throughout the phase where its chamber communicates with this other port 46 .
- a pump 26 generally comprises a greater number of axial pistons housed in its barrel, such as for example five, seven or nine pistons.
- the inclination of the plate 34 determines the stroke of movement of each piston, so that the adjustment of this inclination makes it possible to adjust the displacement of the pump, that is to say its flow per barrel turn.
- the inclination of the plate 34 is adjustable by means of a control cylinder 47 and a compensation cylinder 48 which extend parallel to the axis AP while being arranged diametrically opposite around this axis. PA.
- the plate 34 is for its part mounted tilting around an unmarked axis which intersects the axis AP while being oriented perpendicular to a plane passing through the axis AP and through the cylinders 47 and 48.
- the control cylinder 47 comprises a body 49 in which slides a rod terminated by a plate 51 separating this body 49 into two chambers, with a return spring 52 housed in the control chamber marked 50 which is opposite to the rod, this spring 52 having one end resting on the plate and its other end resting on the bottom of the body 49.
- This spring 52 continually tends to deploy the cylinder, to cause its rod to come out of the body, and this rod has its free end resting on one side of the plate 34.
- the cylinder 48 comprises a body 54 in which slides a rod terminated by a plate 56 separating the body into two chambers, and its rod rests on one side of the plate 34. Its chamber opposite its rod is, which constitutes the compensation chamber identified by 55 is pressurized by an oil tap coming out of the pump 26.
- This flow has the effect of pressurizing the compensation cylinder 48 which extends its rod thus tending to reduce the inclination of the plate.
- the control cylinder is pressurized to another pressure value, so that once in service, the pump rotates with a flow rate value, resulting from the inclination of its plate, which is conditioned by the forces exerted by the cylinders 47 and 48 on the plate.
- the cylinders 47 and 48 are depressurized, and the plate resumes an inclined position due to the return spring 52.
- the control cylinder 47 also has its control chamber 50 pressurized with a pressure corresponding to the outlet pressure of the pump. It is arranged to exert on the plate 34 a greater torque than the compensation cylinder 48 when they are supplied at the same pressure. This can be obtained with a control cylinder 47 having a larger section than the compensation cylinder 48, or possibly by placing this control cylinder 47 at a greater distance from the rear axis of rotation of the plate 34 than the compensation 48.
- the control cylinder exerts a torque on the plate 34 (relative to its rear axis) which is greater than that exerted by the compensation cylinder, so that the plate assumes a certain inclination to which corresponds a certain displacement of the pump.
- variable displacement axial piston pump 26 is integrated into the control circuit 57 represented in FIG. 5, to ensure the pressurization of the upstream chamber 58 or the downstream chamber 59 of a cylinder 61 acting on the longitudinal position of a central shaft of an engine. This makes it possible to maintain the blades at a predetermined pitch angle by maintaining this shaft at a given position and to modify the pitch angle of these blades by moving this shaft.
- This cylinder 61 is carried by the central shaft which rotates while being supplied by the control circuit which is carried by fixed elements of the engine, thanks to a hydraulic transfer bearing 62 surrounding the central shaft, this bearing being the seat hydraulic leaks.
- this circuit 57 includes an oil tank 63 which is connected to the pump 26 to supply it.
- the pump 26 has its outlet connected to a supply line 64 connected to a three-position distributing valve 66, and the chamber 55 of the compensating cylinder 48 of the pump is pressurized to the outlet pressure by being connected to the line 64 by a prick.
- This distributor valve 66 which here is a distributor drawer, is connected to a first chamber of the transfer bearing 62 via an upstream pipe 67, and this first chamber of the bearing 62 directly supplies the upstream chamber 58 of the cylinder 61.
- the distributor valve 66 is connected to a second chamber of the transfer bearing 62 via a downstream pipe 68, and this second chamber of the bearing 62 directly supplies the downstream chamber 59 of the jack 61.
- the distributor valve 66 occupies a first position corresponding for example to a cruising flight situation, in which it connects on the one hand the downstream chamber 59 to the outlet of the pump 26, and on the other leaves the upstream chamber 58 to a purge line 69 opening into the tank 63.
- the circuit 57 comprises a selection valve 71 connected to the upstream pipe 67, to the downstream pipe 68, and to a control pipe nor supplying the chamber 50 of the control cylinder 47.
- This selector valve 71 which is here a shuttle valve, continuously connects the control pipe 72 to the pipe having the highest pressure among the upstream pipe 67 and the downstream pipe 68 .
- the pressure in the downstream chamber 59 automatically adjusts to the force exerted by the blades on the rod of the cylinder 61.
- the output flow rate of the pump 26 increases, which makes it possible to increase the pressure in the chamber 59 to counter the increase in the force exerted by the blades while compensating for the increase in leaks in the bearing. 62 resulting from the increase in pressure.
- the hydraulic control circuit 57 thus makes it possible to automatically regulate the pressure in the cylinder 61 to adapt it continuously to the value of the forces exerted by the fan blades.
- the pitch of the blades does not change when the forces which they exert (which correspond to the aerodynamic forces which they undergo) fluctuate, and the control pressure used is the lowest possible since it is continuously adjusted to this force. This makes it possible to limit the consumption of the pump, and thereby to optimize the efficiency of the motor.
- the circuit 57 also includes a purge line 73 of the control line 72 which connects the latter to the reservoir 63, and which includes a non-return valve 74 which is here a ball valve.
- a purge line 73 of the control line 72 which connects the latter to the reservoir 63, and which includes a non-return valve 74 which is here a ball valve.
- another purge pipe 76 connects the supply pipe 64 to the reservoir 63, this other purge pipe 76 also being equipped with a non-return valve 77 which here is a ball valve to lower the pressure. of the supply line as soon as it becomes greater than a threshold value.
- This other purge pipe 76 can be integrated directly into the pump to connect its outlet to its inlet via the non-return valve.
- control pipe 72 is connected to the selector valve 71 via a restriction 78 which makes it possible to smooth out the peaks or irregularities in the pressure to avoid unnecessarily disturbing the flow rate of the pump.
- this control pipe 72 is also connected to the upstream pipe 67 by a restriction 79, and it is also connected to the downstream pipe 68 by another restriction 81.
- the distributing valve 66 which occupies a first position in the configuration of FIG. 5 can also occupy a second position corresponding to its configuration in FIG. communication between supply line 64 and cylinder 61, and any communication between purge line 69 and cylinder 61.
- the cylinder 61 is not blocked, but on the contrary it is capable of being moved at a relatively slow speed when forces are applied to it.
- the distributing valve can still occupy a third position, corresponding to the situation illustrated in FIG. 7.
- This third position is similar to its first position, except that the supply to the jack 61 is then reversed: upstream chamber 58 which is pressurized to the supply pressure leaving the pump, and its downstream chamber 59 is connected to the purge 69 to have a substantially zero pressure.
- This third position of the distributing valve may correspond to a situation in which the forces are applied by the blades to the cylinder in the opposite direction to the case of FIG. 5.
- the cylinder is regulated to exert a force of the upstream to downstream in order to oppose the force exerted by the blades which is then oriented from downstream to upstream.
- the control circuit has been described for operation ensuring that the blades are maintained at a given pitch angle, including when the forces undergone and exerted by these blades fluctuate, while generating a minimum pressure, that is to say necessary and sufficient. to maintain them in the given position.
- This control circuit 57 also makes it possible to modify the pitch angle of the blades.
- the distributing valve 66 which has been described schematically according to an operation of the “all-or-nothing” type is advantageously a valve of the progressive type to suit a concrete application.
- this valve 66 When this valve 66 is in its first position, it can also be controlled to provide the fluid with a more or less large passage section. If it is controlled to offer a maximum passage section, the entire flow delivered by the pump is transferred to chamber 59, so that the pressure in this chamber reaches a value greater than that necessary to balance the force exerted by the blades, which generates a displacement of the ram which deploys thereby modifying the pitch angle of the blades.
- the valve In the first position, if the valve is controlled to offer the fluid a partial passage section, corresponding to a predetermined value, the flow transferred to the chamber 59 is lower, to generate in the chamber 59 a pressure value which can be provided just sufficient to balance the forces exerted by the blades, so as only to ensure their maintenance at the pitch angle which they occupy.
- valve when the valve occupies the third position, it can also be controlled to provide the fluid with a more or less large passage section, so as to, depending on the case, generate in the chamber 58 a pressure greater than the pressure balance to retract the actuator, or a pressure corresponding to the balance pressure to maintain the blades at the pitch angle they occupy.
- the control and piloting of the distributing valve are ensured from an engine computer (Fadec) which continuously adjusts the signals sent to this valve according to the operating conditions of the engine.
- Fadec engine computer
- the inclination of the plate 34 of the pump 26 is ensured by a control cylinder 47 of the single-acting type, and by a compensation cylinder 48 of smaller section which is also of the simple type. effect.
- the control chamber and the compensation chamber can also be located in a space delimited by a substantially cylindrical casing surrounding the plate while being closed by a bottom and an internal dividing wall. The dividing wall then extends along a plane passing through the axes AP and AR to separate the control chamber and the compensation chamber, this internal wall being able to be formed in two parts extending on either side of the tree 27.
- the plate can then have a smaller useful surface on the side of the compensation chamber than on the side of the control chamber in order to tilt when the two chambers are pressurized at the same pressure.
- the plate may have a generally circular contour but having a rectilinear flat parallel to the axis AP on the side of the compensation chamber.
- the generally cylindrical casing then has a corresponding flat surface, and a seal carried by the periphery of the plate then provides a seal with the casing.
- control and compensation functions can also be provided with the same double-acting control and compensation cylinder 82 comprising the control chamber 50 and the compensation chamber 55, located at the same position as the control cylinder 47 of the Figure 5, as shown schematically in Figure 8.
- control chamber 50 which incorporates the return spring 52 is located on the side opposite the rod of the cylinder 82 while the compensation chamber 55 is traversed by this rod.
- This compensation chamber 55 thus has a useful section smaller than that of the control chamber 50, the difference in useful section of the two chambers corresponding to the section of the rod.
- the invention makes it possible to regulate the counterpressure of the variable-displacement axial piston pump with a pressure which depends on the forces applied to the actuator controlling the pitch of the blades, instead of regulating it to a high fixed value.
- a pressure which depends on the forces applied to the actuator controlling the pitch of the blades, instead of regulating it to a high fixed value.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Fluid-Pressure Circuits (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR2114426A FR3131274A1 (fr) | 2021-12-23 | 2021-12-23 | Circuit de commande hydraulique de calage d’aubes de soufflante |
| PCT/FR2022/052432 WO2023118724A1 (fr) | 2021-12-23 | 2022-12-20 | Circuit de commande hydraulique de calage d'aubes de soufflante |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP4452753A1 true EP4452753A1 (fr) | 2024-10-30 |
Family
ID=81327673
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP22847588.5A Pending EP4452753A1 (fr) | 2021-12-23 | 2022-12-20 | Circuit de commande hydraulique de calage d'aubes de soufflante |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US20250084836A1 (fr) |
| EP (1) | EP4452753A1 (fr) |
| CN (1) | CN118632810A (fr) |
| FR (1) | FR3131274A1 (fr) |
| WO (1) | WO2023118724A1 (fr) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3163693A1 (fr) | 2024-06-19 | 2025-12-26 | Safran Aircraft Engines | Circuit de commande hydraulique de calage d’aubes de soufflante à pompe désactivable |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3486334A (en) * | 1968-05-16 | 1969-12-30 | Cessna Aircraft Co | Hydraulic power transmission control |
| FR2435604A1 (fr) * | 1978-07-25 | 1980-04-04 | Snecma | Dispositif de commande hydraulique d'inversion de poussee pour moteur a reaction |
| US6468046B1 (en) * | 2000-09-18 | 2002-10-22 | Caterpillar Inc | Apparatus and method for controlling a discharge pressure of a variable displacement hydraulic pump |
| FR2831225B1 (fr) * | 2001-10-24 | 2004-01-02 | Snecma Moteurs | Dispositif electrohydraulique de changement de pas d'helice |
| CN101842590B (zh) * | 2007-08-20 | 2012-12-05 | 罗伯特-博世有限公司 | 具有可调静液压机的液压系统 |
| CN101981313B (zh) * | 2008-07-04 | 2013-07-10 | 三菱重工业株式会社 | 风力发电装置 |
| FR2978953B1 (fr) * | 2011-08-08 | 2013-09-20 | Snecma | Systeme de commande hydraulique de l'orientation de pales de soufflante |
| FR3011288B1 (fr) * | 2013-09-30 | 2018-02-16 | Poclain Hydraulics Industrie | Commande de cylindree de pompe avec pilotage par pression |
| DE102020211285A1 (de) * | 2020-02-13 | 2021-08-19 | Robert Bosch Gesellschaft mit beschränkter Haftung | Hydraulischer Lüfterantrieb |
-
2021
- 2021-12-23 FR FR2114426A patent/FR3131274A1/fr active Pending
-
2022
- 2022-12-20 CN CN202280085414.1A patent/CN118632810A/zh active Pending
- 2022-12-20 WO PCT/FR2022/052432 patent/WO2023118724A1/fr not_active Ceased
- 2022-12-20 US US18/721,235 patent/US20250084836A1/en active Pending
- 2022-12-20 EP EP22847588.5A patent/EP4452753A1/fr active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US20250084836A1 (en) | 2025-03-13 |
| FR3131274A1 (fr) | 2023-06-30 |
| CN118632810A (zh) | 2024-09-10 |
| WO2023118724A1 (fr) | 2023-06-29 |
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Legal Events
| Date | Code | Title | Description |
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