The disclosure refers to the field of cleaning of compressors, especially compressors of exhaust gas turbochargers for internal combustion engines.
It is known that with compressors of exhaust gas turbochargers for internal combustion engines the inducting of polluted air can lead to contaminants, especially on the rotor blades and on the hub of the rapidly rotating impeller. The contaminants cause rough surfaces which within a short time can substantially impair the output of the compressor.
In order to avoid the effects which are mentioned in the introduction, compressors are regularly cleaned. The cleaning is carried out under full load or partial load, depending upon design of the compressor. The impeller is correspondingly rotated at full rotational speed or at reduced rotational speed, and a cleaning fluid is fed to the flow upstream of the impeller.
If these regions, which cannot be reached in the case of the rapidly rotating impeller, are to be effectively cleaned, the internal combustion engine has to be throttled in order to lower the rotational speed of the impeller and consequently to lower the speed of the compressor rotor blades.
Cleaning with conventional cleaning devices, therefore, does not always lead to satisfactory results.
DE 299 09 629 U1 discloses a compressor with a device for introducing a solution for preventing deposits in the compressor. The solution in this case is atomized via a nozzle just upstream of the compressor or in the compressor. Engine oil, which is extracted from the lubricating oil circuit of the internal combustion engine, is provided as solution.
A compressor with an improved cleaning device is disclosed, by which the compressor can be effectively freed of contaminants even with a rapidly rotating impeller.
A compressor is disclosed, comprising an impeller which is rotatable around an axis, and also a cleaning device for cleaning the impeller, with a feed line for a cleaning fluid, wherein the feed line for the cleaning fluid comprises a feed nozzle which is arranged on the axis and oriented in the direction of the axis in such a way that the cleaning fluid can be directed through the feed nozzle as a bunched feed jet along the axis towards the impeller.
An impeller is disclosed, comprising a hub and rotor blades which are arranged on the hub, wherein means for receiving and transmitting a cleaning fluid which is guided as a bunched feed jet along the axis onto the impeller, are let into the hub.
A cylindrical impeller cleaning attachment is disclosed, comprising a central opening into which a cleaning fluid, which is guided as a bunched feed jet along the axis onto the impeller cleaning attachment, can be guided, and which in its radially outer region leads into radially outwards oriented cleaning nozzles, via which the fluid which is directed into the central opening can be directed radially from the cleaning attachment.
The compressor according to the disclosure with a cleaning device is subsequently explained in more detail with reference to drawings. In the drawings in this case
According to the disclosure, rotor blades and hub of the impeller are cleaned by means of a cleaning fluid jet which is directed along the rotational axis of the impeller onto the impeller. The cleaning fluid jet in this case is directed or sprayed towards the impeller from a feed nozzle which is arranged upon the axis and oriented in the direction of the impeller along the axis. The feed jet in this case follows the axis and consequently strikes the hub of the impeller in the rotational center of the impeller.
This achieves the effect of the cleaning fluid striking the impeller in the radially innermost point, that is in the rotational center, of the impeller. Even if the cleaning fluid is then gathered by the strong flow and is carried radially outwards, it is ensured that the cleaning fluid at least partially flows along the hub surface and the desired cleaning of the surface occurs in the process.
By a jet divider in the rotational center of the impeller the feed jet can be uniformly divided and deflected in the radial direction. The jet divider has a tip and advantageously has inclined flanks which are curved radially outwards. As a result, the feed jet can be smoothly deflected so that it does not spray back from the hub surface.
The feed jet can additionally be collected by a central bore in the rotational center of the impeller. Especially in combination with the jet divider, an optimum intermediate storage for the cleaning fluid is created in this way. In the central bore, the cleaning fluid is carried radially outwards and accelerated in the circumferential direction. In the radial extension of the central bore, a ring of cleaning fluid is formed, which co-rotates with the impeller. The cleaning fluid is consequently uniformly distributed along the circumference of the central bore, so that the cleaning fluid which issues from the central bore can also uniformly clean the impeller along the circumference.
For specific orientation of the cleaning fluid onto the rotor blades of the impeller, or onto hub regions which lie between the rotor blades, radially outwards oriented cleaning nozzles can be let into the hub of the impeller. The cleaning nozzles are especially advantageously arranged in the radially outer region of the central bore so that the cleaning fluid can be forced from the central bore through the cleaning nozzles as a result of the centrifugal acceleration and directed onto the regions of the impeller which are to be cleaned.
Depending upon requirement, the cleaning nozzles are oriented so that the jet which is produced issues from the nozzle in a bunched or diverging manner. A diverging jet is advantageous if a distribution of cleaning fluid over a large area is aimed for, while the bunched jet is typically directed onto surface points with persistent contamination.
The jet divider, the central bore and the cleaning nozzles can be integrated individually or in any combination in a cleaning attachment which can be fitted onto the hub tip of the impeller and fastened thereupon. As a result, existing impellers can be retrofitted with the cleaning device according to the disclosure in the conceivably simplest way.
As already mentioned in the introduction,
Unlike the conventional cleaning device, in the case of the compressor cleaning according to the disclosure the feed line 5′″ for the cleaning fluid is centrally arranged. As shown in
Seen from the fluidic point of view, the feed jet 71 in the case of a radial compressor lies upon a flow line which is directed along the axis. As a result, even during full load operation of the compressor and with correspondingly stronger flow, the cleaning fluid can be injected in a manner in which it is directed with greater precision onto the impeller. Although the feed jet 71 of cleaning fluid occurs in the center of the impeller, the cleaning fluid is carried along the hub surface and the rotor blade roots as a result of the large centrifugal forces into the outer regions of the impeller, especially of the rotor blades 11, so that a complete wetting of the impeller is carried out.
The feed jet strikes the nose of the hub 10 of the impeller 1 and is deflected there from the axial direction into the radial direction. In order to assist the deflection and to ensure the uniform distribution of cleaning fluid, in the first exemplary embodiment of the compressor cleaning according to the disclosure in accordance with
In order to direct the cleaning fluid flow, which is deflected in the radial direction, specifically onto individual regions of the surfaces which are to be cleaned, cleaning nozzles 12 in the form of holes or slot-shaped recesses can be let into the surface of the hub radially outside the center of the hub. A constant cleaning nozzle jet 72 can be directed through the cleaning nozzles onto the same point of the impeller, since the nozzles of course do not move relative to the points which are to be cleaned.
A washing nozzle per rotor blade is advantageously arranged, as is also schematically indicated in the sectional diagram in accordance with
It is also conceivable that cleaning nozzles are arranged in a differently oriented manner along the circumference, so that for example one row of first nozzles is directed onto the rotor blades, and second nozzles, which are arranged between the nozzles of the first row in each case, are oriented onto the regions of the surface of the hub which are to cleaned.
So that the cleaning fluid film which is formed on the surface of the nose of the hub penetrates into the nozzles, no projections, which block the flow of cleaning fluid in the radial direction, can be attached radially outside the nozzles. Alternatively, an encompassing annular projection can be provided, which accumulates the cleaning fluid all around.
In order to be able to even better gather the cleaning fluid during the radial deflection of the feed jet 71, a central opening 15 is let into the nose of the hub 10 according to the second exemplary embodiment of the compressor cleaning according to the disclosure in accordance with
In a third exemplary embodiment of the compressor cleaning according to the disclosure in accordance with
When the feed jet strikes the surface of the hub or of the cleaning attachment, and also during the deflection in the radial direction, the cleaning fluid is accelerated in the circumferential direction. In order to assist this acceleration, as shown in the section through the cleaning attachment in
In the section through the cleaning attachment 6, the cleaning nozzles 62 are also to be seen, which in the represented embodiment are not strictly radially outwards let into the wall of the cleaning attachment, but, corresponding to the rotational direction of the impeller, are let in a manner extending obliquely to the radial.
The cleaning nozzles can be correspondingly oriented to the region of the impeller which is to be cleaned. Depending upon whether all the rotor blades 11, or a defined section of the surface of the hub, which is subjected to especially heavy contamination, are to be cleaned, differently oriented and differently formed nozzles can be advisable. The cleaning nozzle jet 72 can ultimately be influenced by the development of the orifices of the cleaning nozzles. As shown in the last two figures, the jet can leave the nozzles in a bunched (
The amount of cleaning fluid which issues through the cleaning nozzles is advantageously added to the amount of cleaning fluid which is fed to the impeller by means of the feed jet through the feed nozzle. The added amount in this case should be slightly greater in order to compensate possible losses through sprays. In order to prevent such losses and to reduce the influence of the feed jet by the flow of the medium which is to be compressed, the feed nozzle 51 can reach up to a short distance of several mm to several cm, depending upon dimensions of the impeller, to the nose of the hub of the impeller. Alternatively, the feed nozzle, as schematically indicated in
As cleaning fluid, for example water, with or without special processing, purification or temperature conditioning, with or without cleaning additives, can be used.
The compressor cleaning according to the disclosure is especially suitable for cleaning radial compressors of exhaust gas turbochargers for internal combustion engines.
It will be appreciated by those skilled in the art that the present invention can be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The presently disclosed embodiments are therefore considered in all respects to be illustrative and not restricted. The scope of the invention is indicated by the appended claims rather than the foregoing description and all changes that come within the meaning and range and equivalence thereof are intended to be embraced therein.
Number | Date | Country | Kind |
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05405481.2 | Aug 2005 | EP | regional |
This application claims priority under 35 U.S.C. §119 to EP Application 05405481.2 filed in Europe on Aug. 17, 2005, and as a continuation application under 35 U.S.C. §120 to PCT/CH2006/000359 filed as an International Application on Jul. 7, 2006, designating the U.S., the entire contents of which are hereby incorporated by reference in their entireties.
Number | Date | Country | |
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Parent | PCT/CH2006/000359 | Jul 2006 | US |
Child | 12031149 | US |