The present invention relates to an electric gear pump. In particular, the present invention relates to a gerotor electric gear pump.
The present invention also relates to a pump assembly comprising, in series:
The use of systems for supplying fuel, in particular diesel, to an internal combustion engine, which comprise a high-pressure pump for supplying the internal combustion engine, and a low-pressure pump for supplying fuel to the high-pressure pump, is already known. The high-pressure pump comprises at least one pumping piston moved by a shaft and housed in a cylinder supplied with fuel at low pressure. At least two different types of low-pressure pump for such systems currently exist.
The first type comprises a gear pump which is driven by the same shaft as drives the pistons of the high-pressure pump. In particular, this gear pump may be a “gerotor” pump. As is known, the gerotor pump comprises an external spur rotor rotated by the shaft and housed inside an internal spur rotor. During rotation, the spurs of the external spur rotor engage with the spurs of the internal spur rotor, which has one more spur than the external spur rotor. The two rotors, rotating either absolutely or relatively, or relative to one another, pump fuel from an inlet, connected to the tank, to an outlet, connected to the high-pressure pump.
The second type of gear pump comprises gear pumps not driven by the shaft for driving the pumping pistons, but pumps driven electrically or electromagnetically. With this type of pump, in current gerotor pumps, at least one out of the internal spur rotor and the external spur rotor has magnetic or ferromagnetic modules, such as bundles of little plaques made of iron, which engage electromagnetically with a stator which is arranged outside of the internal spur rotor and comprises electrical windings. In particular, it is currently common to house the magnetic modules, which usually have a parallelepiped structure, embedded directly in the internal spur rotor near the external surface thereof, or near the windings of the stator placed outside the internal spur rotor.
By supplying current to said windings, electromagnetic conditions are created such that the gerotor starts to rotate, pumping the fuel between the tank and the high-pressure pump.
In this type of gerotor electric gear pump, the stator with electrical windings, which may also be defined as an “electric motor” since it causes the gerotor to move, is placed at the same level as said gerotor so as to increase the electromagnetic interaction. This concentric arrangement of gerotor and stator currently requires the presence of a bearing placed between the external wall of the internal spur rotor of the gerotor and the stator. A high degree of precision in terms of mechanical machining regarding the geometric circularity of the external surface of the internal spur rotor coupled to said bearing is thus necessary.
Although gerotor electric gear pumps are widely used, the current versions of these pumps have a number of drawbacks.
In particular, placing the magnets inside the internal spur rotor as described above is a difficult, expensive process.
In light of the known prior art, it is an aim of the present invention to produce an alternative gear pump, preferably an alternative gerotor electric gear pump.
In particular, it is an aim of the present invention to produce a gerotor electric gear pump which makes it possible to improve the corresponding prior art pumps described above, simply and economically, both from the functional viewpoint and from the structural viewpoint.
In accordance with these aims, the present invention relates to an electric gear pump comprising:
Advantageously, in this way, the magnetic structure, which may take the form of one or more magnets or one or more ferromagnetic structures, is not embedded in the internal spur rotor but is rigidly secured thereto by being positioned between the external surface of the rotor and the covering thereof. As will be seen below, the magnetic structure may be held firmly in this position by providing direct connections between the magnetic structure and the covering and/or the rotor and it is even possible to provide for simply forcing the magnetic structure into position by compressing or clamping in seats.
According to a first embodiment of the invention, the magnetic structure is connected both to the covering and to the internal spur rotor. Preferably, according to this embodiment, both the covering and the magnetic structure are made in the form of cylindrical sleeves having the same height, along the axis of rotation A, as the external surface of the internal spur rotor. In this embodiment use is made of adhesive, both between the magnetic cylindrical sleeve and the covering and between the magnetic cylindrical sleeve and the internal spur rotor. According to this embodiment of the invention, the magnetic structure is therefore rigidly secured to the rotor by the connection provided by the adhesive, while the covering is connected to the rotor indirectly by means of the adhesive bonding to the magnetic structure which is in turn adhesively bonded to the rotor.
Advantageously, according to this embodiment, no particular machining of the surfaces of either the rotor or the covering is required.
According to another embodiment of the invention, the magnetic structure is connected to the covering or to the internal spur rotor. Preferably, the magnetic structure is connected to the covering or to the internal spur rotor by adhesive, while the covering is connected to the internal spur rotor by screws which are engaged in threaded holes made radially in the internal spur rotor. According to two different variants of this embodiment of the invention, the covering and the magnetic structure are made in the form of cylindrical sleeves provided with aligned holes, or the covering is made in the form of a cylindrical sleeve with holes and the magnetic structure is made in the form of magnetic sectors spaced apart in line with the holes in the covering. In this latter variant, lateral shoulders may be provided to facilitate positioning of the magnetic segments. According to this latter variant embodiment of the invention, the magnetic structure is rigidly secured to the rotor by virtue of the fact that it is connected to the covering, which is in turn connected to the rotor. Preferably, the screws used in the embodiments of the invention just described do not project outside the covering.
Advantageously, in this way, the screws do not have a negative impact on the rotary coupling between the covering and the bearing of the stator.
According to another embodiment of the invention, adhesive is not used and the magnetic structure is simply clamped in position by tightening the covering against the rotor. Preferably, according to a variant of this embodiment, the internal spur rotor comprises an external surface with at least one circumferential seat and the magnetic structure is made in the form of a ring clamped in the seat by the covering. Preferably, the covering of the rotor is made of metal, for example steel, so as to provide a functional surface for sliding on the bearing of the stator, which is usually made of plastic, for example PEEK.
Naturally, the present invention can be used both for a pump assembly for supplying fuel from a tank to an internal combustion engine which comprises, in series, an electric gear pump as described above and a high-pressure pump, and for just the internal spur rotor with the associated covering as a possible spare part that may be used to improve the pumps currently used.
Further features and advantages of the present invention will become clearer from the description below of two non-limiting embodiments thereof, with reference to the figures in the attached drawings, in which:
In this example, the internal combustion engine 3 is shown only schematically and comprises a common manifold 17 fed by the high-pressure delivery pipes 8 and a plurality of injectors 18 (not shown) designed to spray and inject the fuel at high pressure into the cylinders of the internal combustion engine 3. In
As can be seen in
Lastly, it is clear that amendments and variations may be made to the invention described herein without exceeding the scope of the attached claims.
Number | Date | Country | Kind |
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102016000129613 | Dec 2016 | IT | national |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2017/082846 | 12/14/2017 | WO | 00 |