The present invention relates to the field of turbomachines of the type comprising a rotating spool comprising a drive shaft delivering mechanical power.
The invention applies to any type of turbomachine, in particular those used in aircraft such as turbojets, turboprops and turbomachines with unshrouded fans, also known by the designation of “Open Rotor.”
A conventional turbomachine includes, in known fashion, one or more rotating spools. Each rotating spool comprises a compressor, a turbine and a drive shaft connecting the turbine to the compressor to drive the compressor in rotation. A part of the power generated by the turbomachine is used to drive different accessories (or auxiliary machines) necessary for the operation of the turbojet or of the aircraft, such as for example a lubrication pump or a fuel pump.
To this end, the turbomachine generally comprises an accessory gearbox connecting the drive shaft to the pumps. When the drive shaft is driven in rotation, the accessory gearbox transmits the rotation movement to the different accessories. In other words, the mechanical energy produced by the drive shaft is transmitted to the pumps by the accessory gearbox.
This technical solution has, however, the following disadvantages:
The invention has as its purpose in particular to provide a turbomachine that does not have the aforementioned disadvantages.
This purpose is achieved due to a turbomachine comprising a rotating spool comprising a drive shaft delivering mechanical power, characterized in that it comprises at least one electromagnetic pump mechanically decoupled from the drive shaft, each electromagnetic pump comprising at least one stator delimiting an annular internal volume in which is present a rotor able to drive a fluid, a plurality of magnets distributed annularly on the rotor and at least one plurality of coils distributed annularly inside the stator, the coils of the plurality of coils facing the magnets along an axial direction.
The turbomachine according to the invention is thus equipped with one or more pumps which are mechanically decoupled from the drive shaft and which are controlled independently of the shaft speed. It is thus possible to have greater freedom of choice of the rotation seed of the pump and in the installation possibilities of the pump(s) in the turbomachine.
In addition, by placing the plurality of permanent magnets and the plurality of coils facing one another along the axial direction, the radial bulk of the pump is greatly optimized. A very compact pump is thereby obtained.
According to a particular characteristic of the turbomachine of the invention, the rotor comprises a wheel provided with a plurality of vanes, the magnets of the plurality of magnets being held at the outer periphery of the wheel.
According to another particular characteristic of the turbomachine of the invention, each electromagnetic pump comprises first and second pluralities of coils, present respectively on one side and on the other side of the wheel, the coils of the first and second pluralities of coils facing the magnets along the axial direction. Two pluralities of the coils allow ensuring redundancy in the event of a breakdown or failure of one plurality of coils. The redundancy of the plurality of coils can also be used to double the power of the electromagnetic fields to which the permanent magnets are subjected.
According to another particular feature of the turbomachine of the invention, the rotor comprises an inner gear cooperating with an outer ring gear with inner teeth, the magnets of the plurality of magnets being held at the outer periphery of the outer ring gear.
According to another particular feature of the turbomachine of the invention, each electromagnetic pump comprises first and second pluralities of coils, present respectively on one side and on the other side of the outer ring gear, the coils of the first and second pluralities of coils facing the magnets along the axial direction. The use of two pluralities of coils allows ensuring redundancy in the event of a breakdown or a failure of one plurality of coils and/or doubling the power of the electromagnetic fields to which the permanent magnets are subjected.
According to another particular feature of the turbomachine of the invention, the rotor comprises an inner gear cooperating with an outer ring gear with inner teeth, the magnets of the plurality of magnets being held on the inner gear.
According to another particular feature of the turbomachine of the invention, each electromagnetic pump comprises first and second pluralities of coils, present respectively on one side and on the other side of the gear, the coils of the first and second pluralities of coils facing the magnets along the axial direction. The use of two pluralities of coils allows ensuring redundancy in the event of a breakdown or a failure of one plurality of coils and/or doubling the power of the electromagnetic fields to which the permanent magnets are subjected.
According to another particular feature of the turbomachine of the invention, the magnets of the plurality of magnets are arranged annularly in a Halbach structure. This particular arrangement allows increasing the magnetic field on the outside of the rotor while the magnetic field on the inside of the rotor is substantially cancelled. The dissipation of the magnetic field is thus reduced, which improves the control of the rotor by the coils.
The invention also has as its object an aircraft comprising at least one turboprop or one turbojet comprising a turbomachine according to the invention.
The invention applies generally to any turbomachine equipped with at least one pump controlled independently of the engine speed of the turbomachine. It applies particularly, but not exclusively, to pumps of the liquid ring, with a lateral or regenerative channel, and gerotor type.
The electromagnetic pump 100 also comprises an impeller or rotor 120 comprising a wheel 121 provided with a plurality of vanes 122 extending from the wheel in a radial direction DR, a ring 123 being present at the outer periphery of the wheel. In the example described here, the ring 123 is fixed on the radially outer ends of the vanes 122. The impeller 120 includes a rotation shaft 124 intended to be supported by bearings 1114 and 1124 present respectively on the casing 111 and the flange 112. In known fashion in pumps of the liquid ring type, the shaft is placed eccentrically on the impeller 120, for example by means of a crossbar (not shown in
Once all the elements constituting the pump 100 are assembled, the coils 140 are located facing permanent magnets 130 along an axial direction DA. In known fashion, the control of the electromagnetic pump 100 (torque and rotation speed) is accomplished by control of the current circulating in the coils.
By fixing the permanent magnets 130 directly to the impeller 120, a portion of the drive means of the pump are integrated directly within the moving elements, which allows obtaining a high level of integration of the drive means and therefore a reduced bulk for the pump.
In addition, by placing the plurality of permanent magnets and the plurality of coils facing one another along the axial direction, the radial bulk of the pump is greatly optimized. A very compact pump is thus obtained, which can be controlled independently relative to the engine speed of the turbomachine with which it is associated.
The electromagnetic pump 200 also comprising a fixed pump body or stator 210 consisting of a first casing 211 and of a second casing 212. The casings 211 and 212 each include respectively a solid cylindrical central portion 2110, 2120 provided with an aspiration/discharge port 2111, 2121 and a circular outer wall 2112, 2122 extending concentrically around the central portion 2110, 2120. First annular recesses 2113 are delimited in the first casing 211 between the central portion 2110 and the outer wall 2112. Second annular recesses 2123 are delimited in the second casing 212 between the central portion 2120 and the outer wall 2122.
The electromagnetic pump 200 also comprises a plurality of permanent magnets 230 held annularly in recesses 2230 present in the ring 223, and first and second pluralities of coils 240 and 250. The first plurality of coils 240 is distributed annularly in the first annular recesses 2113 while the second plurality of coils 250 is distributed annularly in the second annular recesses 2123.
Once the pump 200 is assembled, the rotation shaft 224 of the impeller 220 is supported by the bearings 2214 and 2224, present respectively on the first and second casings 211 and 212, while the first and second pluralities of coils 240 and 250 are present respectively on one side and on the other side of the wheel 220 and facing the magnets along an axial direction DA.
In addition to the advantages of integration and compactness already mentioned earlier for the pump 100, the electromagnetic pump 200 comprises two pluralities of coils which allow ensuring redundancy in the case of a breakdown or a failure of one plurality of coils, each plurality of coils having its own connections to the control system. The redundancy of the plurality of coils can also be used to double the power of the electromagnetic fields to which the permanent magnets are subjected. It will also be noted that, always for the purpose of optimizing the bulk of the pump, only the plurality of coils is redundant, and this as close as possible to the permanent magnets.
The pump 200 can also be a lateral channel pump, also called a regenerative pump as previously explained in relation with the pump 100.
The electromagnetic pump 300 also comprises a rotor 320 comprising an inner gear 321 and an outer ring gear 322, present around the inner gear 321 along a radial direction DR. The inner gear comprises outer teeth consisting here of six teeth 3210 while the outer ring gear 322 comprises inner teeth consisting here of 7 teeth 3220. The inner gear 321 includes a rotation shaft 324 intended to be supported by bearings 3114 and 3124, present respectively on the casing 311 and the flange 312. In a manner known for pumps of the gerotor type, the fluid is aspired from the port 3120, then discharged via the port 3121 in capsules created between the teeth 3210 and 3220 respectively of the inner gear 321 and of the outer ring gear 322 during the rotation of these two elements.
The electromagnetic pump 300 also includes a plurality of permanent magnets 330 distributed annularly over the outer periphery of the outer ring gear 322, and a plurality of coils 340 distributed annularly inside the fixed pump body or stator 310. More precisely, in the example described here, the permanent magnets 330 are held in the recesses 3221 present in the outer ring gear 322 while the coils 340 are held in the annular recesses 3113 present in the casing 311.
Once all the elements constituting the pump 300 are assembled, the coils 340 are located facing the permanent magnets 330 along an axial direction DA. In known fashion, the control of the electromagnetic pump 300 (torque and speed of rotation) is accomplished by controlling the current circulating in the coils.
By fixing the permanent magnets directly 330 on the outer ring gear 322, a portion of the means for driving the pump is integrated directly within the moving elements, which allows obtaining a high level of integration of the driving means and therefor a reduced bulk for the pump.
In addition, by placing the plurality of permanent magnets and the plurality of coils facing one another along the axial direction, the radial bulk of the pump is greatly optimized. A very compact pump is thus obtained, which can be controlled independently relative to the engine speed of the turbomachine with which it is associated.
The electromagnetic pump 400 also comprises a plurality of permanent magnets 430 held annularly in recesses 4221 present in the outer ring gear 422 and first and second pluralities of coils 440 and 450.
The first plurality of coils 440 is distributed annularly in the first annular recesses 4113 while the second plurality of coils 450 is distributed annularly in the second annular recesses 4123.
Once the pump 400 is assembled, the rotation shaft 424 of the inner gear 421 is supported by bearings 4114 and 4124 present respectively on the first and second casings 411 and 412 while the first and second pluralities of coils 440 and 450 are present respectively on one side and on the other side of the outer ring gear 422 and facing the magnets along an axial direction DA.
In addition to the advantages of integration and of compactness already mentioned earlier for the pump 300, the electromagnetic pump 400 comprises two pluralities of coils which allow ensuring redundancy in case of breakdown or of failure of one plurality of coils, each plurality of coils having its own connections to the control system. The redundancy of the plurality of coils can also be used to double the power of the electromagnetic fields to which the permanent magnets are subjected. It will also be noted that, still with the purpose of optimizing the bulk of the pump, only the plurality of coils is redundant, this as close as possible to the permanent magnets.
The electromagnetic pump 500 also comprises a rotor 520 comprising an inner gear 521 and an outer ring gear 522, present around the inner gear 521 along a radial direction DR. The inner gear comprises outer teeth consisting here of six teeth 5210 while the outer ring gear 522 comprises inner teeth consisting here of 7 teeth 5220. The inner gear 521 includes a rotation shaft 524 intended to be supported by bearings 5114 and 5124 present respectively on the casing 511 and the flange 512.
The electromagnetic pump 500 also comprises a plurality of permanent magnets 530 held annularly in the inner gear 521 around the rotation shaft 524 and a plurality of coils 540 held in the annular recesses 5113 present in the casing 511.
Once all the elements constituting the pump 500 are assembled, the coils 540 are located facing the permanent magnets 530 along an axial direction DA. In known fashion, the control of the electromagnetic pump 500 (torque and speed of rotation) is accomplished by controlling the current circulating in the coils.
By fixing the permanent magnets direction 530 on the inner gear 321, a portion of the means for driving the pump is integrated directly within the moving elements, which allows obtaining a high level of integration of the driving means and therefore a reduced bulk for the pump.
In addition, by placing the plurality of magnets and the plurality of coils facing one another along the axial direction, the radial bulk of the pump is greatly optimized. A very compact pump is thus obtained which can be controlled independently relative to the engine speed of the turbomachine with which it is associated.
Just as for the pumps described previously, the electromagnetic pump 500 can be equipped with dual coils, namely comprise first and second pluralities of coils present respectively on one side and on the other side of the inner gear, the coils of the first and second pluralities facing the magnets along the axial direction.
According to an additional feature of the invention, the permanent magnets present on the outer ring of the impeller for the embodiments described earlier in relation to
The electromagnetic pump according to the invention can in particular be used to supply the turbomachine with fuel or lubricant.
Regarding the oil supply circuit of a turbomachine, the low and/or high pressure feed pumps can also be replaced partially or totally by electromagnetic pumps controlled independently of the engine speed. In this case, pumps of the gerotor type are used preferably but not exclusively.
Number | Date | Country | Kind |
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1911967 | Oct 2019 | FR | national |
This application is a National Stage Application of International Application PCT/FR2020/051855, filed on Oct. 16, 2020, now published as WO 2021/079048 A1, and which claims priority to French patent application FR1911967, filed on Oct. 25, 2019, which is incorporated by reference herein in its entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/FR2020/051855 | 10/16/2020 | WO |