Multi-stage radial compressor unit comprising gas removal during a compressor stage

Abstract

A radial compressor unit for compressing gas has several compressor stages. Each compressor stage includes an impeller having rotor blades, and a flow channel arranged downstream of the impeller, as viewed in the flow direction of the gas to be compressed, having a diffusor section, a deflection section, and a recirculation section having guide blades. The gas compressed in a compressor stage can be removed as cooling gas for cooling a component to be cooled, and can be conveyed in the direction of the component to be cooled. The cooling gas can be removed adjacent to an intermediate wall of the compressor stage from the deflection section and/or the recirculation section of the flow channel of the compressor stage.

Claims

1. A radial compressor unit for the compression of gas, comprising: a plurality of compressor stages (11, 12, 13), each compressor stage (11, 12, 13) having: an intermediate wall (32), an impeller (18) with rotor blades (23), a flow channel (24) arranged, with respect to a flow direction of the gas to be compressed, downstream of the impeller (18), the flow channel (24) having: a diffuser section (25) directly following, in the flow direction, the impeller (18), a deflection section (26) following, in the flow direction, the diffuser section (25), and a recirculation section (27) with multiple guide blades (28), the recirculation section (27) following, in the flow direction, the deflection section (26), wherein the diffuser section (25), the deflection section (26) and the recirculation section (27) are bounded on the inside by the intermediate wall (32), and a removal pipe (35) having a projecting section (37) projecting into the flow channel (24) and having, at an end of the projecting section (37) within a flow path of the flow channel (24), a removal opening (36) arranged in a region of the flow channel (24) proximate the deflection section (26) and adjacent to the intermediate wall (32), the removal pipe (35) and removal opening (36) being configured and arranged such that compressed gas, as cooling gas, is removed, by the removal pipe (35), from the flow channel (24), in a region of the flow channel (24) adjacent to the intermediate wall (32) so as to remove cooling gas from the region of the flow channel (24) at which the removal opening (36) is located.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Preferred further developments of the invention are obtained from the following description. Exemplary embodiments of the invention are explained in more detail with the help of the drawings without being restricted to this. In the drawings:

(2) FIG. 1: is a schematic cross section through a radial compressor unit for the compression of gas;

(3) FIG. 2: is a detail from a radial compressor unit according to the invention in the region of a compressor stage of the same according to a first version of the invention; and

(4) FIG. 3: is a detail from a radial compressor unit according to the invention in the region of a compressor stage of the same according to a second version of the invention.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(5) The present invention relates to a radial compressor unit for compressing gas, such as is employed, for example, for the extraction of natural gas in the offshore sector.

(6) FIG. 1 shows a schematic cross section through a radial compressor unit 10 for the compression of gas, wherein the radial compressor unit 10 has multiple compressor stages 11, and 13, which are driven by a drive 14 embodied as an electric motor, wherein of the drive 14 embodied as electric motor a stator 15 on the one hand and a rotor 16 on the other hand are shown.

(7) The drive 14 drives a shaft 17 of the radial compressor unit 10, wherein with the shaft 17 so-called impellers 18 of the compressor stages 11, 12 and 13 are coupled, so that the impellers 18 of the compressor stages 11, 12 and 13 are driven by the drive 14 of the radial compressor unit 10. The impellers 18 of the compressor stages 11, 12 and 13 are also called rotors.

(8) Seen in flow direction of the gas to be compressed downstream of the impeller 18 of the respective compressor stage 11, 12, 13, a flow channel 24 follows each respective compressor stage 11, 12, 13.

(9) In the illustrated exemplary embodiment, the radial compressor unit 10 of FIG. 1 exemplarily comprises compressor stages 11, and 13, wherein uncompressed gas is fed to compressor stages 11, 12 and 13 as per the arrow 19, and wherein compressed gas is discharged as per the arrow 20. The compressor stages 11, 12 and 13 are connected one behind the other and serve for the step-by-step compression of the gas, wherein the compressor stage 11 can also be described as low-pressure compressor stage, the compressor stage 12 also as medium pressure compressor stage and the compressor stage 13 also as high-pressure compressor stage.

(10) The compressor stages 11, 12 and 13 of the radial compressor unit 10 are received in a common housing 21 together with the drive 14 embodied as electric motor, wherein the shaft 17 is mounted in the housing 21 via bearings 22.

(11) During the operation of the radial compressor unit it is required to cool its components, in particular the drive 14, for the purpose of which compressed gas as cooling gas can be removed from a compressor stage of the radial compressor unit 10 and can be conveyed for cooling the assembly to be cooled, in particular of the drive 14 to be cooled, in the direction of the assembly to be cooled.

(12) It is important that the cooling gas is removed from a compressor stage such that the cooling gas, on the one hand, has few contaminations and, on the other hand, has an adequately high pressure in order, on the one hand, not to contaminate the assembly to be cooled through the cooling gas and, on the other hand, ensure as effective a cooling of the assembly to be cooled as possible.

(13) FIGS. 2 to 3 each show details of a radial compressor 10 according to the invention in the region of one of the compressor stages, namely of the compressor stage 11. In FIGS. 2 to 3, on the one hand, the impeller 18 of the respective compressor stage 11 is shown, which comprises rotor blades 23, and the flow channel 24 that follows, seen in flow direction of the gas to be compressed downstream of the impeller 18, is shown, wherein the flow channel 24 comprises multiple sections, namely a diffuser section 25 directly following the impeller 18, a deflection section 26 following the diffuser section 25 and a recirculation section 27 following the deflection section 26. In the recirculation section 27, fixed guide blades 28 are positioned, of which on, the one hand an inlet edge 29, and, on the other hand, an outlet edge 30 are schematically shown. The flow direction through the compressor stage 11 is visualised by arrows 31. The diffuser section 25, the deflection section 26 and the recirculation section 27 of the flow channel 24 of the compressor stage 11 are radially bounded on the inside at least in sections by an intermediate wall 32 on the stator side, hub-side.

(14) In order to now remove as pure as possible a cooling gas with an adequately high pressure from the compressor stage 11, it is proposed, according to the invention, to remove the cooling gas adjacent to the intermediate wall 32 of the compressor stage 11 from the deflection section 26 and/or the recirculation section 27 of the flow channel 24 of the compressor stage 11 and feed it to the assembly to be cooled.

(15) FIG. 2 shows a first version of the invention, in which the cooling gas is removed from the flow channel 24 of the compressor stage 11, namely via at least one removal pipe 35 projecting into the flow channel 24 in the region of the flow channel 24 located at a portion of the deflection section 26 leading to the recirculation section 27, the removal pipe 35 having a removal opening 36 positioned adjacent to the intermediate wall 32. The removal opening 36 of the removal pipe 35 via which the cooling gas is removed from the compressor stage 11 in the region of the intermediate wall 32, is positioned in this case in a region of the deflection section 26 leading to the recirculation section 27 so that the cooling gas is removed from the flow channel 24 in this region.

(16) The, or each, removal pipe 35 projecting into the flow channel 24 comprises a profiled, flow-guiding outer wall at least on the section 37, which projects into the flow channel 24 in order to exclude impairment of the flow through the removal pipe 35 projecting into the flow channel.

(17) A further version of the invention is shown by FIG. 3. In FIG. 3 the cooling gas is removed from the recirculation section 27 of the flow channel 24 of the compressor stage 11, namely via at least one removal channel 38, whose removal opening 39 is introduced into a front edge 29 of a guide blade 28. Here, as is evident from FIG. 3, this removal opening 39 for the removal channel 38 introduced into the front edge of the guide blade 28 is introduced into the front edge 29 of the guide blade 28 adjacent to the intermediate wall 32.

(18) With all versions according to the invention, cooling gas can be removed from a compressor stage 11 in such a manner that the cooling gas comprises few contaminations and an adequately high pressure. Because of this, effective cooling of an assembly of the radial compressor unit 10 to be cooled is possible on the one hand and on the other hand there is no risk that the assembly to be cooled is contaminated by the cooling gas.

(19) Thus, while there have been shown and described and pointed out fundamental novel features of the invention as applied to a preferred embodiment thereof, it will be understood that various omissions and substitutions and changes in the form and details of the devices illustrated, and in their operation, may be made by those skilled in the art without departing from the spirit of the invention. For example, it is expressly intended that all combinations of those elements and/or method steps which perform substantially the same function in substantially the same way to achieve the same results are within the scope of the invention. Moreover, it should be recognized that structures and/or elements and/or method steps shown and/or described in connection with any disclosed form or embodiment of the invention may be incorporated in any other disclosed or described or suggested form or embodiment as a general matter of design choice. It is the intention, therefore, to be limited only as indicated by the scope of the claims appended hereto.