JP2005163691A - Compressor for supercharging equipped with surge suppressing means - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To improve a compressor for supercharging so as to present higher operation efficiency while suppressing surge over all speed ranges from a low speed range to a high speed range. <P>SOLUTION: This compressor for supercharging is provided with a compressor rotor, an annular diffuser row arranged on the peripheral edge of the compressor rotor, and a cochleate housing surrounding the annular diffuser row, and the annular diffuser row is constituted of a tiltable row of vanes. Opening/closing of a recirculation passage leading to the upstream side from an outlet region of the diffuser row is controlled in connection with tilting of the vanes. <P>COPYRIGHT: (C)2005,JPO&NCIPI

Description

  The present invention relates to a turbocharger compressor, and more particularly, to an improvement in surge suppression means of a turbocharger compressor,

  It is known as supercharging to pressurize intake air in order to increase the output performance of an internal combustion engine, and a means for this is known as a supercharging compressor. The supercharging compressor is usually driven by an exhaust turbine driven by the exhaust of the internal combustion engine, and contributes to the recovery of energy from the exhaust of the internal combustion engine to increase the thermal efficiency of the internal combustion engine.

When the supercharging compressor is driven by an exhaust turbine, particularly when the internal combustion engine is an internal combustion engine of a vehicle, the rotational speed thereof changes greatly from a low speed range to a high speed range. In this case, when the supercharging compressor has a structure having a compressor rotor, an annular diffuser row disposed on the periphery thereof, and a cochlear housing surrounding the annular diffuser row, the medium flow rate to the large flow rate are provided. If a compressor is designed so that a certain amount of supercharging can be obtained even in the region, there is a problem that surges are likely to occur in the low flow rate region. In response to such a problem, a row of tiltable vanes capable of variably adjusting a tilt angle with respect to a radiation extending radially from the central axis when the annular diffuser row is viewed in a virtual cross section perpendicular to the central axis of the compressor rotor. Patent Document 1 below describes that the vane tilt angle is changed in accordance with the rotational speed of the compressor rotor. Further, in this type of supercharging compressor, an open / close control valve is provided in the middle, and a reflux passage is provided that communicates the downstream side of the compressor rotor to the upstream side, and the reflux passage is appropriately opened and pressurized by the compressor. Patent Document 2 below describes that surge is suppressed by returning a part of air to the suction side of the compressor.
JP-A 64-66419 JP 112002-182257

  The present invention relates to a supercharging compressor having a compressor rotor, an annular diffuser row disposed on the periphery thereof, and a cochlear housing surrounding the annular diffuser row, wherein the annular diffuser row is a compressor rotor. When constituted by a row of vanes inclined with respect to the radiation extending radially from the central axis when viewed in a virtual section perpendicular to the central axis, the occurrence of surge is caused by the dynamic pressure of the air flow accelerated by the compressor rotor. In view of this, it is governed by the relationship between the increase in static pressure across the diffuser row obtained by converting to static pressure by the row and the inclination angle of the vane that regulates the flow of air flow across the diffuser row. Pay attention and operate at higher operating efficiency while better suppressing surges over the entire speed range from low speed to high speed It has an object to provide a supercharging compressor which is improved so.

  In order to solve the above-mentioned problems, the present invention includes a compressor rotor, an annular diffuser row disposed on the periphery thereof, and a cochlear housing surrounding the annular diffuser row, and the annular diffuser row is A supercharger composed of a row of vanes provided so as to be tiltable so that a tilt angle with respect to a radiation extending radially from the central axis can be variably adjusted when viewed in a virtual section perpendicular to the central axis of the compressor rotor. The compressor has a reflux passage that is controlled to open and close in response to the tilt of the vane, and that opens the outlet region of the diffuser row to the upstream side of the diffuser row when the tilt angle of the vane is equal to or greater than a predetermined value. The present invention proposes a supercharging compressor characterized by the above.

  In this case, the outlet of the return passage may be at an arbitrary position upstream of the diffuser row, but may be particularly between the compressor rotor and the diffuser row or upstream of the compressor rotor.

  Further, when the tilt angle of the vane is equal to or greater than the predetermined value, the reflux passage may be opened more widely as the tilt angle increases within a predetermined range.

  The inlet of the return passage may be a port that opens opposite to the end face of the vane, and the opening area of the port may be controlled to be opened and closed by the vane end face.

  As described above, the compressor rotor, the annular diffuser row disposed on the periphery thereof, and the cochlear housing surrounding the annular diffuser row, the annular diffuser row is seen in a virtual cross section perpendicular to the central axis of the compressor rotor. In the supercharged compressor constituted by a row of vanes that can be tilted so as to be able to variably adjust the tilt angle with respect to the radiation extending radially from the central axis, the tilting of the vane is supported. If the return passage that opens the outlet region of the diffuser row to the upstream side of the diffuser row when the vane tilt angle is greater than or equal to a predetermined value is provided, the amount of air flowing into the compressor rotor can be reduced. Accordingly, in the process of increasing the tilt angle of the vane to match the flow of air discharged from the periphery of the compressor rotor, In accordance with the vane tilt angle corresponding to the velocity region in which the possibility of occurrence of the above occurs, a part of the air compressed from the outlet region of the diffuser row is returned to the upstream side through the reflux passage, thereby controlling the vane tilt angle. The effect of suppressing the surge and the effect of suppressing the surge by reducing the unstable region of the flow in the diffuser array by partially recirculating the air are optimally matched, and the minimum amount of air is returned according to the compressor rotor rotation speed. The turbocharging compressor can be operated with higher operating efficiency while reliably suppressing the surge with the flow rate. Return to the upstream side of the compressor rotor from the diffuser row outlet region to alleviate the unstable region of the diffuser flow related to the compressor surge does not go to the upstream side of the compressor rotor, but between the compressor rotor and the diffuser row Is also possible.

  When the tilt angle of the vane is greater than or equal to the predetermined value, if the return passage is opened more widely as the tilt angle increases within the predetermined range, surge suppression by controlling the vane tilt angle and crossing the diffuser row It becomes possible to make a mutual harmony with surge suppression by partial air recirculation more desirable.

  In addition, if the inlet of the return passage is a port that opens opposite to the end face of the vane, and the opening area of the port is controlled to be opened and closed by the vane end face, the vane is used directly as a port variable opening / closing valve means. The movable means for variable opening and closing of the port can be omitted, and the opening and closing of the reflux passage and the degree thereof can be controlled corresponding to the tilt of the vane.

  FIG. 1 attached herewith is a view corresponding to a longitudinal cross-sectional view illustrating only one of the essential portions of one embodiment of a supercharging compressor according to the present invention. However, in view of the fact that this type of device is generally composed of a combination of vertically split halves for the convenience of manufacture and assembly as a product, the figure shows only the front half of the housing having such a structure. Is shown as being removed.

  The illustrated supercharging compressor includes a compressor rotor 10 that is rotatably supported by a suitable bearing device not shown in the drawing to rotate about a central axis C, and a series of airfoils arranged at the periphery thereof. A supercharged air outlet communicated in a tangential direction with an annular diffuser row 14 made of vanes 12, a cochlear housing 16 surrounding the annular diffuser row, and a cochlear diffuser row outlet space 18 formed around the annular diffuser row 14 Port 20. In this case, each of the series of vanes 12 corresponds to a radiation (one of which is indicated by R) extending radially from the central axis when viewed in a virtual section perpendicular to the central axis C of the compressor rotor by the rotation shaft 22. The tilt angle α is supported so that the tilt angle α can be changed, and a diffuser tilt angle control mechanism (not shown in FIG. 1) that controls the tilt angles variably at the same time is used to expand the tilt angle and the associated diffuser passage. The variable diffuser is configured to change the degree according to the change in the rotational speed of the compressor rotor.

  FIG. 2 is a schematic view of one embodiment as viewed in the direction of the arrow when a part of the turbocharging compressor shown in FIG. 1 is cut along the central axis of the compressor rotor by a virtual cutting plane indicated by D in FIG. It is. Intake air is sucked from the suction port 24 as indicated by the arrow in the figure, and is centrifugally accelerated by the rotation of the compressor rotor 10 in the direction indicated by the arrow in FIG. 1, and its kinetic energy is converted into pressure energy by the annular diffuser row 14. However, it is collected in the cochlear diffuser row outlet space 18 and then flows out through the supercharged air outlet port 20.

  One end of a lever 26 is attached to the rotating shaft 22 of each vane 12, and the other end of each lever is driven all at once in the circumferential direction by vane tilt control means not shown in the drawing. The tilt angle of the vane 12 is changed at the same time.

  The wall surface 30 that the housing 16 is opposed to one end face 28 of each vane 12 is blocked by the end face of each vane when the tilt angle α of each vane is equal to or less than a first predetermined value. When the tilt angle α of the vane exceeds the first predetermined value, the vane begins to be exposed out of the overlap with the end face of each vane, and the vane tilt angle reaches a certain second predetermined value. As the tilt angle of the diffuser row increases, ports 32 are provided which are exposed to a greater extent than the overlap with the end faces of the vanes, and these ports are located in the diffuser row at the outlet region of the diffuser row 14. When it is opened and communicated with the reflux passage 34 leading to the upstream side, the opening degree of the reflux passage 34 is controlled according to the opening degree. In the embodiment shown in FIG. 2, the outlet of the reflux passage 34 is between the compressor rotor 10 and the diffuser row 14. In FIG. 1, the end face 28 of the vane that controls the opening degree facing each port 32 is a face that is visible to the front in the figure, and since each port 32 is not visible, it corresponds to the vane end face 28. Its position and outline are indicated by broken lines.

  FIG. 3 is a view similar to FIG. 2 showing another embodiment of the present invention. In FIG. 3, the same parts as those shown in FIG. 2 are denoted by the same reference numerals as in FIG. In this case, the outlet of the reflux passage 34 a that leads from the outlet region of the diffuser row 14 to the upstream side of the diffuser row is the upstream side of the compressor rotor 10. Reference numeral 36 denotes a porous packing for adjusting the flow of the reflux passage 34a. In addition, it may replace with this porous packing and the guide vane for flow volume adjustment may be provided.

  Thus, according to the present invention, when the annular diffuser row 14 is viewed in a virtual cross section perpendicular to the central axis C of the compressor rotor 10, the tilt angle α with respect to the radiation R extending radially from the central axis can be variably adjusted. It is composed of a row of tiltable vanes 12, and changes the vane tilt angle in accordance with the amount of air flowing into the compressor rotor to better adapt the shape of the diffuser to the rotational speed of the compressor rotor, thereby suppressing the occurrence of surges, and the diffuser row By appropriately opening the reflux passages 34 and 34a leading to the upstream side from the outlet region of the gas, and returning a part of the air pressurized through the diffuser row to the upstream side of the diffuser row, the unstable flow region is removed. By controlling the occurrence of surges in a related manner, these two surge suppression effects can be better harmonized, It is possible to operate the supercharger compressor at higher operating efficiency while better suppressing surge over the flow rate range in all operating regions leading to a high flow rate region.

  Although the present invention has been described in detail with reference to two embodiments, it will be apparent to those skilled in the art that various modifications can be made to these embodiments within the scope of the present invention.

The figure equivalent to the longitudinal section which shows one embodiment of one embodiment of the compressor for supercharging by this invention only about the principal part in illustration. In FIG. 1, a state where a part of the illustrated supercharging compressor is cut along the central axis of the compressor rotor by a virtual cutting surface indicated by D in FIG. 1 is viewed in the direction of the arrow in one embodiment of the present invention. Schematic. Schematic similar to FIG. 2 showing another embodiment of the present invention.

Explanation of symbols

  DESCRIPTION OF SYMBOLS 10 ... Compressor rotor, 12 ... Vane, 14 ... Annular diffuser row, 16 ... Cochlear housing, 18 ... Diffuser row outlet space, 20 ... Supercharged air outlet port, 22 ... Rotating shaft, 24 ... Suction port, 26 ... Lever, 28 ... One end face of vane, 30 ... Housing wall surface, 32 ... Port, 34, 34a ... Reflux passage, 36 ... Porous packing for resistance adjustment

Claims (5)

  A compressor rotor, an annular diffuser row disposed on the periphery of the compressor rotor, and a cochlear housing surrounding the annular diffuser row, the annular diffuser row being viewed in a virtual cross section perpendicular to the central axis of the compressor rotor. A supercharging compressor constituted by a row of vanes provided so as to be tiltable so as to be able to variably adjust a tilt angle with respect to a radiation extending radially from the central axis, and corresponding to the tilt of the vane. A supercharging compressor characterized by having a reflux passage that is controlled to open and close and opens an outlet region of the diffuser row to an upstream side of the diffuser row when a tilt angle of the vane is a predetermined value or more.   The supercharging compressor according to claim 1, wherein an outlet of the reflux passage is between the compressor rotor and the diffuser row.   The supercharging compressor according to claim 1, wherein an outlet of the reflux passage is upstream of the compressor rotor.   The supercharging according to any one of claims 1 to 3, wherein when the tilt angle of the vane is equal to or greater than the predetermined value, the return passage is opened more widely as the tilt angle increases in a predetermined range. Compressor. The inlet of the reflux passage is a port that opens opposite to the end surface of the vane, and the opening area of the port is controlled to be opened and closed by the vane end surface. A supercharging compressor according to any one of the above.

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