EP2209997A1 - Noise attenuation device for a centrifugal compressor discharge or suction nozzle - Google Patents

Noise attenuation device for a centrifugal compressor discharge or suction nozzle

Info

Publication number
EP2209997A1
EP2209997A1 EP08851643A EP08851643A EP2209997A1 EP 2209997 A1 EP2209997 A1 EP 2209997A1 EP 08851643 A EP08851643 A EP 08851643A EP 08851643 A EP08851643 A EP 08851643A EP 2209997 A1 EP2209997 A1 EP 2209997A1
Authority
EP
European Patent Office
Prior art keywords
centrifugal compressor
suction nozzle
side resonator
resonator
compressor discharge
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
EP08851643A
Other languages
German (de)
French (fr)
Inventor
Chiel Schoeman
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Siemens AG
Original Assignee
Siemens AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siemens AG filed Critical Siemens AG
Priority to EP08851643A priority Critical patent/EP2209997A1/en
Publication of EP2209997A1 publication Critical patent/EP2209997A1/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/663Sound attenuation
    • F04D29/665Sound attenuation by means of resonance chambers or interference

Definitions

  • the invention relates to a centrifugal compressor discharge or suction nozzle, a centrifugal compressor discharge or suction nozzle formed as a pipe section piece adapted to be mounted on a centrifugal compressor nozzle, a centrifugal compressor comprising the centrifugal compressor discharge or suction nozzle, and a centrifugal compressor arrangement respectively comprising at least one side resonator integrally formed in the centrifugal compressor discharge or suction nozzle, wherein the side resonator (s) act(s) like an acoustic mirror.
  • centrifugal compressor In chemical and petrochemical plants a centrifugal compressor is commonly used for pressurising process gas.
  • the centrifugal compressor comprises at least one suction nozzle and at least one discharge nozzle, wherein said nozzles are connected to plant piping. Through the suction nozzle process gas flows into the centrifugal compressor to be compressed therein. The compressed process gas exits the centrifugal compressor through the discharge nozzle to be delivered to downstream plant components.
  • the centrifugal compressor comprises at least one rotor with at least one impeller. Downstream of the impeller the centrifugal compressor comprises a diffuser. The impeller and the diffuser are aerodynamically effective to compress the process gas. During operation of the compressor the rotor rotates thereby generating noise.
  • the noise is a combination of discrete frequency noise (tonal noise) related to the so- called blade passing frequency and its higher harmonics. The noise generates a high noise exposure of the environment and can cause structural failures of the centrifugal compressor and the piping due to vibration cracking.
  • a remedy to reduce the noise intensity level of the centrifugal compressor is to cover the centrifugal compressor with a noise hood.
  • the noise hood is able to reduce the noise exposure of the environment.
  • the noise-hood is cost- intensive and needs to be taken into consideration with respect to space requirement being problematic in a plant with limited space.
  • Another remedy to reduce the noise intensity level of the centrifugal compressor is to provide the downstream piping of the centrifugal compressor with a piping silencer.
  • the piping silencer is flown through by the process gas and therefore induces a high flow resistance resulting in an adverse pressure loss.
  • the piping silencer is costly in construction and large in geometrical dimensions. Such a silencer is shown in DE 1814146Al .
  • the centrifugal compressor discharge or suction nozzle comprises at least one side resonator integrally formed in the centrifugal compressor discharge or suction nozzle.
  • the centrifugal compressor discharge or suction nozzle is formed as a pipe section piece adapted to be mounted on a centrifugal compressor nozzle, comprising at least one side resonator integrated into the pipe section piece.
  • various stacked rings can be installed forming one or more side resonator (s) .
  • the centrifugal compressor comprises the centrifugal compressor discharge or suction nozzle.
  • the centrifugal compressor arrangement comprises the centrifugal compressor.
  • the process gas discharging the centrifugal compressor is interfered by tonal noise generated within the centrifugal compressor during its operation at a specific frequency band.
  • the tonal noise is related to the so-called blade passing frequency and its higher harmonics.
  • the discharge or suction nozzle of the centrifugal compressor comprises the side resonator (s) , whereby the side resonator (s) is (are) in direct cooperation with the discharge or inlet process gas. Since the side resonator (s) is (are) appropriate to reduce the tonal noise by the effects of acoustic impedance, the side resonator (s) act(s) like an acoustic mirror at the specific frequency band of the tonal noise.
  • the geometrical dimensions of the side resonator (s) determine the frequency band in which the resonator (s) is (are) active. Therefore, it is possible to attenuate the frequency band in which the blade passing frequency is active. As a consequence of this, during operation of the centrifugal compressor, its noise emission level is lower.
  • the process gas passes the side resonator without disturbing the process gas flow in the discharge or suction nozzle. Therefore, the side resonator includes very low or even less flow resistance to the process gas discharge or suction flow. Hence, a side resonator does not cause any significant pressure loss in the process gas discharge or suction flow.
  • the process gas discharge or suction flow is noise attenuated by the side resonator (s) . Consequently, the centrifugal compressor comprising the side resonator has a high energy efficiency.
  • the side resonator (s) is (are) integrated in the pipe section piece, such that advantageously the centrifugal compressor can be equipped with the side resonator (s) subsequent to its assembly.
  • different types of side resonators can be provided for the centrifugal compressor in replacing the pipe section piece provided with different side resonators, and the pipe section piece can be designed as an universal section which can be mounted on any centrifugal compressor.
  • various rings can be stacked in between the nozzle piping connection forming one or more resonators that can be fitted to any compressor.
  • the centrifugal compressor Since the side resonator is in the pipe section piece, , the centrifugal compressor has a compact design, which is easy and cost saving to be manufactured.
  • the compressor discharge or suction nozzle comprises a plurality of side resonators located after each other. This enlarges the frequency band in which the noise is attenuated and makes the solution most robust.
  • Each side resonator is capable to reduce a specific frequency. Therefore, by providing a plurality of side resonators after each other, wherein each side resonator can be adapted to reduce another specific frequency, the frequency band in which the plurality of side resonators is effective to reduce the tonal noise, is broadened. This is the reason why the inventive centrifugal compressor is silenced in an effective way by means of the plurality of side resonators.
  • the pipe section piece comprises a plurality of ring elements having different inner diameters and concentrically adjoining each other, and at least one flange element facing the plurality of ring elements, wherein the plurality of ring elements form the side resonator (s) .
  • the ring elements preferably can be formed by universal rings. Further, preferably standard flange elements can be used, such that manufacturing costs of the pipe section piece are low.
  • the centrifugal compressor arrangement comprises the centrifugal compressor, wherein the side resonator comprises a liquid injection device for liquid injection into the side resonator for cleaning thereof.
  • the centrifugal compressor arrangement comprises a gas scrubber provided upstream of the centrifugal compressor and a bypass line from the side resonator to the gas scrubber for bypassing the process gas or the liquid from the side resonator to the gas scrubber.
  • the bypass line comprises a bypass valve.
  • Fig. 4 is a longitudinal section of a third embodiment of a centrifugal compressor nozzle according to the invention.
  • Fig. 18 is a longitudinal section of a ninth embodiment of a centrifugal compressor nozzle according to the invention.
  • Fig. 19 is a longitudinal section of a tenth embodiment of a centrifugal compressor nozzle according to the invention.
  • Fig. 21 is a schematic view of a centrifugal compressor arrangement according to the invention.
  • the side resonator according to Fig. 4 comprises a circular resonator 4.
  • the circular resonator 4 is a discshaped cavity encompassing the centrifugal compressor nozzle 1.
  • the side resonator any shape is possible provided its effective length is such that the desired noise attenuation is possible. Therefore, the side resonator do not need to be rotation symmetric but can comprise an eccentrically formed cylindrical resonator 6. Examples of the eccentrically formed
  • Fig. 18 to 20 show a pipe section piece 10.
  • the pipe section piece 10 is adapted to be mounted on a centrifugal compressor nozzle. Therefore, when the pipe section piece is mounted on the centrifugal compressor nozzle, process gas entering or discharging the centrifugal compressor passes through the pipe section piece 10.
  • Fig. 18 to 20 show one of many possible variants of the pipe section piece 10.
  • the pipe piece section 10 according to Fig. 18 and 20 is integrally formed and comprises a pipe 11 and two flanges 12 provided on the longitudinal ends of the pipe 11.
  • the flanges 12 are adapted to be fitted to the centrifugal compressor nozzle.
  • the pipe 11 has an inner diameter 15.
  • each circular resonator 4 to 4'' has an inner diameter 13 to 13' ' , respectively, being greater than the inner diameter 15 of the pipe 11, wherein the inner diameter 13 is smaller than the inner diameter 13', and the inner diameter 13' is smaller than the inner diameter 13' ' .
  • the circular resonators 4 to 4'' are arranged side by side such that the pipe piece section is acoustically effective for a broad frequency band.
  • the number and shape of the resonators 4 to 4'' can be varied depending on the desired acoustic characteristic of the pipe section piece 10.
  • i designates the number of resonators
  • 0 designates the diameter of the resonator i
  • t x designates the width of the resonator i
  • L 1 designates the distance between the resonator i and the resonator i+1.
  • the pipe piece section 10 according to Fig. 19 is similar to the pipe piece section 10 according to Fig. 18 and 20, but comprises seven individual ring elements 14, 14', 14'', 14'", 14 IV , 14 V , 14 VI .
  • the inner diameter of the ring elements 14, 14'' 14 IV , 14 VI equals the inner diameter 15 of the pipe 11.
  • the ring elements 14', 14''', 14 V have different inner diameters 13 to 13'' and are concentrically adjoined together.
  • the pipe piece section 10 according to Fig. 19 comprises two flange elements 12 facing the ring elements 14, 14', 14", 14'", 14 IV , 14 V , 14 VI for being adapted to be mountable to a centrifugal compressor nozzle.
  • the seven ring elements 14, 14', 14", 14'", 14 IV , 14 V , 14 VI are stacked and form the circular resonators 4, 4', 4''. Any other number of ring elements 14, 14', 14'', 14''', 14 IV , 14 V , 14 VI is possible.
  • Fig. 20 shows a centrifugal compressor arrangement comprising a centrifugal compressor 21 comprising the centrifugal compressor nozzle 1.
  • the centrifugal compressor nozzle 1 comprises the circular resonators 4 and 4'.
  • the centrifugal compressor nozzle 1 comprises a wash water injection device 28 for wash water injection into the side resonators 4 and 4' for cleaning thereof.
  • the centrifugal compressor arrangement 20 comprises a gas scrubber 24 provided upstream of the centrifugal compressor 21 and a bypass line 29 from the centrifugal compressor nozzle 1 to the gas scrubber 24.
  • the bypass line 29 comprises a bypass valve 30 for controlling the bypassed gas flow. Additionally, wash water is fed back to the scrubber 24 via the bypass line 29.
  • Fig.22, 23 show views of the first embodiment according to Fig. 1, 2 having self cleaning properties.
  • the single tube resonator 2 is thread-like arranged on the compressor nozzle 1. Therefore, a part of the process gas flows through the cavity.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A centrifugal compressor discharge or suction nozzle comprises at least one side resonator integrally formed in the centrifugal compressor discharge or suction nozzle. Further, a centrifugal compressor discharge or suction nozzle formed as a pipe section piece adapted to be mounted on a centrifugal compressor, comprises at least one side resonator integrated into the pipe section piece. Furthermore, a centrifugal compressor comprises the centrifugal compressor discharge or suction nozzle and/or the pipe section piece. Additionally, a centrifugal compressor arrangement comprises the centrifugal compressor.

Description

Description
Noise attenuation device for a centrifugal compressor discharge or suction nozzle
The invention relates to a centrifugal compressor discharge or suction nozzle, a centrifugal compressor discharge or suction nozzle formed as a pipe section piece adapted to be mounted on a centrifugal compressor nozzle, a centrifugal compressor comprising the centrifugal compressor discharge or suction nozzle, and a centrifugal compressor arrangement respectively comprising at least one side resonator integrally formed in the centrifugal compressor discharge or suction nozzle, wherein the side resonator (s) act(s) like an acoustic mirror. Description
In chemical and petrochemical plants a centrifugal compressor is commonly used for pressurising process gas. The centrifugal compressor comprises at least one suction nozzle and at least one discharge nozzle, wherein said nozzles are connected to plant piping. Through the suction nozzle process gas flows into the centrifugal compressor to be compressed therein. The compressed process gas exits the centrifugal compressor through the discharge nozzle to be delivered to downstream plant components.
The centrifugal compressor comprises at least one rotor with at least one impeller. Downstream of the impeller the centrifugal compressor comprises a diffuser. The impeller and the diffuser are aerodynamically effective to compress the process gas. During operation of the compressor the rotor rotates thereby generating noise. The noise is a combination of discrete frequency noise (tonal noise) related to the so- called blade passing frequency and its higher harmonics. The noise generates a high noise exposure of the environment and can cause structural failures of the centrifugal compressor and the piping due to vibration cracking.
It is desirable to reduce the noise intensity level of the emitted noise spectrum at the blade passing frequency and its higher harmonics. Attenuation of the noise level upstream and downstream of the suction and discharge piping, respectively, will reduce the exposure to the environment and can reduce cyclic stresses in the structures upstream and downstream of the nozzles .
A remedy to reduce the noise intensity level of the centrifugal compressor is to cover the centrifugal compressor with a noise hood. The noise hood is able to reduce the noise exposure of the environment. However, the noise-hood is cost- intensive and needs to be taken into consideration with respect to space requirement being problematic in a plant with limited space.
Another remedy to reduce the noise intensity level of the centrifugal compressor is to provide the downstream piping of the centrifugal compressor with a piping silencer. However, the piping silencer is flown through by the process gas and therefore induces a high flow resistance resulting in an adverse pressure loss. Further, the piping silencer is costly in construction and large in geometrical dimensions. Such a silencer is shown in DE 1814146Al .
Furthermore, another remedy to reduce the noise intensity level of the centrifugal compressor is to provide a Helmholtz array in the diffuser. The Helmholtz array is installed on the diffuser wall resulting in a complicated and cost- intensive centrifugal compressor construction. Such a construction is shown in US 6,575,696 Bl.
It is an object of the invention to provide a centrifugal compressor discharge or suction nozzle, a centrifugal compressor comprising the centrifugal compressor discharge or suction nozzle, and a centrifugal compressor arrangement comprising the centrifugal compressor, wherein the centrifugal compressor is effectively noise attenuated during operation and cost-effective in construction.
According to the invention, the centrifugal compressor discharge or suction nozzle comprises at least one side resonator integrally formed in the centrifugal compressor discharge or suction nozzle.
Alternatively, according to the invention, the centrifugal compressor discharge or suction nozzle is formed as a pipe section piece adapted to be mounted on a centrifugal compressor nozzle, comprising at least one side resonator integrated into the pipe section piece.
Further, according to the invention, between compressor nozzles and piping various stacked rings can be installed forming one or more side resonator (s) .
Furthermore, according to the invention, the centrifugal compressor comprises the centrifugal compressor discharge or suction nozzle.
Additionally, according to the invention, the centrifugal compressor arrangement comprises the centrifugal compressor.
The process gas discharging the centrifugal compressor is interfered by tonal noise generated within the centrifugal compressor during its operation at a specific frequency band. The tonal noise is related to the so-called blade passing frequency and its higher harmonics. The discharge or suction nozzle of the centrifugal compressor comprises the side resonator (s) , whereby the side resonator (s) is (are) in direct cooperation with the discharge or inlet process gas. Since the side resonator (s) is (are) appropriate to reduce the tonal noise by the effects of acoustic impedance, the side resonator (s) act(s) like an acoustic mirror at the specific frequency band of the tonal noise. The geometrical dimensions of the side resonator (s) determine the frequency band in which the resonator (s) is (are) active. Therefore, it is possible to attenuate the frequency band in which the blade passing frequency is active. As a consequence of this, during operation of the centrifugal compressor, its noise emission level is lower.
Further, when the process gas flows through the discharge or suction nozzle, the process gas passes the side resonator without disturbing the process gas flow in the discharge or suction nozzle. Therefore, the side resonator includes very low or even less flow resistance to the process gas discharge or suction flow. Hence, a side resonator does not cause any significant pressure loss in the process gas discharge or suction flow. The process gas discharge or suction flow is noise attenuated by the side resonator (s) . Consequently, the centrifugal compressor comprising the side resonator has a high energy efficiency.
As an alternative, the side resonator (s) is (are) integrated in the pipe section piece, such that advantageously the centrifugal compressor can be equipped with the side resonator (s) subsequent to its assembly. Further, different types of side resonators can be provided for the centrifugal compressor in replacing the pipe section piece provided with different side resonators, and the pipe section piece can be designed as an universal section which can be mounted on any centrifugal compressor.
As an alternative various rings can be stacked in between the nozzle piping connection forming one or more resonators that can be fitted to any compressor.
Since the side resonator is in the pipe section piece, , the centrifugal compressor has a compact design, which is easy and cost saving to be manufactured. Preferably, the compressor discharge or suction nozzle comprises a plurality of side resonators located after each other. This enlarges the frequency band in which the noise is attenuated and makes the solution most robust.
Each side resonator is capable to reduce a specific frequency. Therefore, by providing a plurality of side resonators after each other, wherein each side resonator can be adapted to reduce another specific frequency, the frequency band in which the plurality of side resonators is effective to reduce the tonal noise, is broadened. This is the reason why the inventive centrifugal compressor is silenced in an effective way by means of the plurality of side resonators.
It is preferred that the pipe section piece comprises a plurality of ring elements having different inner diameters and concentrically adjoining each other, and at least one flange element facing the plurality of ring elements, wherein the plurality of ring elements form the side resonator (s) .
The ring elements preferably can be formed by universal rings. Further, preferably standard flange elements can be used, such that manufacturing costs of the pipe section piece are low.
It is preferred that the centrifugal compressor arrangement comprises the centrifugal compressor, wherein the side resonator comprises a liquid injection device for liquid injection into the side resonator for cleaning thereof.
Preferably, the centrifugal compressor arrangement comprises a gas scrubber provided upstream of the centrifugal compressor and a bypass line from the side resonator to the gas scrubber for bypassing the process gas or the liquid from the side resonator to the gas scrubber. Further, it is preferred that the bypass line comprises a bypass valve.
In the following the invention is explained on the basis of preferred embodiments with reference to the drawings. In the drawings :
Fig. 4 is a longitudinal section of a third embodiment of a centrifugal compressor nozzle according to the invention,
Fig. 18 is a longitudinal section of a ninth embodiment of a centrifugal compressor nozzle according to the invention,
Fig. 19 is a longitudinal section of a tenth embodiment of a centrifugal compressor nozzle according to the invention,
Fig. 21 is a schematic view of a centrifugal compressor arrangement according to the invention, and
Further, the side resonator according to Fig. 4 comprises a circular resonator 4. The circular resonator 4 is a discshaped cavity encompassing the centrifugal compressor nozzle 1.
For the side resonator any shape is possible provided its effective length is such that the desired noise attenuation is possible. Therefore, the side resonator do not need to be rotation symmetric but can comprise an eccentrically formed cylindrical resonator 6. Examples of the eccentrically formed
Fig. 18 to 20 show a pipe section piece 10. The pipe section piece 10 is adapted to be mounted on a centrifugal compressor nozzle. Therefore, when the pipe section piece is mounted on the centrifugal compressor nozzle, process gas entering or discharging the centrifugal compressor passes through the pipe section piece 10. Fig. 18 to 20 show one of many possible variants of the pipe section piece 10. The pipe piece section 10 according to Fig. 18 and 20 is integrally formed and comprises a pipe 11 and two flanges 12 provided on the longitudinal ends of the pipe 11. The flanges 12 are adapted to be fitted to the centrifugal compressor nozzle. The pipe 11 has an inner diameter 15.
Further, in the pipe 11 three circumferentially extending ring grooves are provided thereby forming three circular resonators 4 to 4" integrated into the pipe section piece 10, respectively. Each circular resonator 4 to 4'' has an inner diameter 13 to 13' ' , respectively, being greater than the inner diameter 15 of the pipe 11, wherein the inner diameter 13 is smaller than the inner diameter 13', and the inner diameter 13' is smaller than the inner diameter 13' ' . The circular resonators 4 to 4'' are arranged side by side such that the pipe piece section is acoustically effective for a broad frequency band.
The number and shape of the resonators 4 to 4'' can be varied depending on the desired acoustic characteristic of the pipe section piece 10. In Fig. 18 and 19 i designates the number of resonators, 0 designates the diameter of the resonator i, tx designates the width of the resonator i, and L1 designates the distance between the resonator i and the resonator i+1.
The pipe piece section 10 according to Fig. 19 is similar to the pipe piece section 10 according to Fig. 18 and 20, but comprises seven individual ring elements 14, 14', 14'', 14'", 14IV , 14V , 14VI. The inner diameter of the ring elements 14, 14'' 14IV , 14VI equals the inner diameter 15 of the pipe 11. The ring elements 14', 14''', 14V have different inner diameters 13 to 13'' and are concentrically adjoined together. Further, the pipe piece section 10 according to Fig. 19 comprises two flange elements 12 facing the ring elements 14, 14', 14", 14'", 14IV , 14V , 14VI for being adapted to be mountable to a centrifugal compressor nozzle. The seven ring elements 14, 14', 14", 14'", 14IV , 14V , 14VI are stacked and form the circular resonators 4, 4', 4''. Any other number of ring elements 14, 14', 14'', 14''', 14IV , 14V , 14VI is possible.
Fig. 20 shows a centrifugal compressor arrangement comprising a centrifugal compressor 21 comprising the centrifugal compressor nozzle 1. The centrifugal compressor nozzle 1 comprises the circular resonators 4 and 4'.
As a further option, the centrifugal compressor nozzle 1 comprises a wash water injection device 28 for wash water injection into the side resonators 4 and 4' for cleaning thereof. Further, the centrifugal compressor arrangement 20 comprises a gas scrubber 24 provided upstream of the centrifugal compressor 21 and a bypass line 29 from the centrifugal compressor nozzle 1 to the gas scrubber 24. By means of the bypass line 29 a gas flow can be forced through the pipe section piece 10 to the gas scrubber 24. Further, the bypass line 29 comprises a bypass valve 30 for controlling the bypassed gas flow. Additionally, wash water is fed back to the scrubber 24 via the bypass line 29.
Fig.22, 23 show views of the first embodiment according to Fig. 1, 2 having self cleaning properties. The single tube resonator 2 is thread-like arranged on the compressor nozzle 1. Therefore, a part of the process gas flows through the cavity.

Claims

Claims
1. Centrifugal compressor discharge or suction nozzle comprising at least one side resonator (2-9) integrally formed in the centrifugal compressor discharge or suction nozzle (1), wherein the side resonator (s) act(s) like an acoustic mirror, characterised in that the centrifugal compressor discharge or suction nozzle is formed as a pipe section piece (10) adapted to be mounted on a centrifugal compressor (21), comprising at least one side resonator (2-9) integrated into the pipe section piece (10), wherein the pipe section piece (10) comprises one or a plurality of ring elements (14-14VI) having different inner diameters (13-13'') and concentrically adjoining each other, and at least one flange element (12) facing the plurality of ring elements (14-14VI), wherein the plurality of ring elements (14-14VI) form the side resonator (4-4'').
2. Centrifugal compressor discharge or suction nozzle according to claim 1, wherein the side resonator (2-9) is integrally formed in the pipe section piece (10) .
3. Centrifugal compressor discharge or suction nozzle according to claim 1 or 2, wherein the compressor discharge or suction nozzle (1) comprises a plurality of side resonators (2-9) located after each other.
4. Centrifugal compressor discharge or suction nozzle according to claim 3, wherein the side resonator comprises an array of single tube resonators (3) circumferentially distributed.
5. Centrifugal compressor discharge or suction nozzle according to any of claims 3 to 4, wherein the side resonator comprises a circular resonator (4).
6. Centrifugal compressor discharge or suction nozzle according to any of claims 1 to 5, wherein the side resonator is a resonator adapted to have self cleaning properties.
7. Centrifugal compressor comprising a centrifugal compressor discharge or suction nozzle according to claim 1 to 6.
8. Centrifugal compressor arrangement comprising a centrifugal compressor (21) according to claim 7, wherein the side resonator (2-10) comprises liquid injection device (28) for liquid injection into the side resonator (2-10) for cleaning thereof.
9. Centrifugal compressor arrangement according to claim 8, wherein the centrifugal compressor arrangement (20) comprises a gas scrubber (24) provided upstream of the centrifugal compressor (21) and a bypass line (29) from the side resonator (2-10) to the gas scrubber (24) for bypassing the liquid from the side resonator (2-10) to the gas scrubber (24) .
10. Centrifugal compressor arrangement according to claim 9, wherein the bypass line (29) comprises a bypass valve (30) .
11. Centrifugal compressor arrangement according to claims 9 or 10, wherein the centrifugal compressor arrangement (20) comprises an additional gas scrubber (24) provided upstream of the centrifugal compressor (21).
EP08851643A 2007-11-20 2008-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle Withdrawn EP2209997A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP08851643A EP2209997A1 (en) 2007-11-20 2008-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP07022502A EP2063130A1 (en) 2007-11-20 2007-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle
EP08851643A EP2209997A1 (en) 2007-11-20 2008-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle
PCT/EP2008/065934 WO2009065904A1 (en) 2007-11-20 2008-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle

Publications (1)

Publication Number Publication Date
EP2209997A1 true EP2209997A1 (en) 2010-07-28

Family

ID=39186808

Family Applications (2)

Application Number Title Priority Date Filing Date
EP07022502A Withdrawn EP2063130A1 (en) 2007-11-20 2007-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle
EP08851643A Withdrawn EP2209997A1 (en) 2007-11-20 2008-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP07022502A Withdrawn EP2063130A1 (en) 2007-11-20 2007-11-20 Noise attenuation device for a centrifugal compressor discharge or suction nozzle

Country Status (3)

Country Link
US (1) US20100278635A1 (en)
EP (2) EP2063130A1 (en)
WO (1) WO2009065904A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE112011101909B4 (en) * 2010-06-04 2021-12-23 Borgwarner Inc. Compressor of an exhaust gas turbocharger
DE102011005025A1 (en) 2011-03-03 2012-09-06 Siemens Aktiengesellschaft Resonator silencer for a radial flow machine, in particular for a centrifugal compressor
US9169750B2 (en) * 2013-08-17 2015-10-27 ESI Energy Solutions, LLC. Fluid flow noise mitigation structure and method
GB2546538A (en) * 2016-01-21 2017-07-26 Gm Global Tech Operations Llc A compressor housing
FR3047599B1 (en) * 2016-02-05 2019-05-24 Universite De Bourgogne LOW THICK PERFORATED MILLE-SHEET ACOUSTIC RESONATOR FOR VERY LOW FREQUENCY ABSORPTION OR ACOUSTIC RADIATION
CN107035484B (en) * 2017-06-22 2023-04-25 广西壮族自治区环境保护科学研究院 Automobile exhaust purifying device

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB489114A (en) * 1937-01-22 1938-07-20 Francois Cementation Co Ltd Improvements in or relating to silencers for flowing gases
US2514998A (en) * 1948-02-16 1950-07-11 Fundom Earl Henry Silencer
US3472001A (en) * 1967-11-01 1969-10-14 American Air Filter Co Gas intake device
SE326279B (en) * 1967-12-13 1970-07-20 T Abrahamsson
US5088886A (en) * 1990-08-28 1992-02-18 Sinko Kogyo Co., Ltd. Inlet air flow conditioning for centrifugal fans
AU635867B2 (en) * 1990-10-22 1993-04-01 Hitachi Automotive Engineering Co., Ltd. Centrifugal fan with noise suppressing arrangement
IT1256414B (en) * 1991-09-06 1995-12-05 Bosch Gmbh Robert BLOWER SILENCER
DE4219249C2 (en) * 1992-06-12 1994-03-31 Kuehnle Kopp Kausch Ag Radial compressor, especially a turbocharger
US6039532A (en) * 1996-07-18 2000-03-21 Iowa State University Research Foundation, Inc. Blower fan blade passage rate noise control scheme
DE29715710U1 (en) * 1997-09-02 1997-10-23 Intensiv-Filter Gmbh & Co Kg, 42555 Velbert Cleaning device for an industrial silencer
FR2780454B1 (en) * 1998-06-29 2001-01-26 Valeo Climatisation NOISE ABSORPTION DEVICE FOR CENTRIFUGAL MOTOR-FAN GROUP
DE19956172C5 (en) * 1999-11-23 2010-09-23 Umfotec Gmbh Double chamber damper
US6575696B1 (en) 2000-09-21 2003-06-10 Fasco Industries, Inc. Method of sound attenuation in centrifugal blowers
US7263995B2 (en) * 2001-02-28 2007-09-04 Hyperbaric Technology, Inc. Hyperbaric oxygen therapy system controls
GB2389150B (en) * 2001-09-07 2004-08-25 Avon Polymer Prod Ltd Noise and vibration suppressors
ITVI20020145A1 (en) * 2002-07-02 2004-01-02 Comefri Spa ANTI-NOISE AND ANTI-VORTE DIVIDER
US8272834B2 (en) * 2004-06-15 2012-09-25 Honeywell International Inc. Acoustic damper integrated to a compressor housing
DE102004057413A1 (en) * 2004-11-26 2006-06-29 Mahle Filtersysteme Gmbh Muffler for internal combustion engine, has housing arranged at airborne sound conveying pipe during operation of internal combustion engine and including damper body with set of hollow bodies that are connected with each other
US7883312B2 (en) * 2005-03-31 2011-02-08 Mitsubishi Heavy Industries, Ltd. Centrifugal blower

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2009065904A1 *

Also Published As

Publication number Publication date
EP2063130A1 (en) 2009-05-27
WO2009065904A1 (en) 2009-05-28
US20100278635A1 (en) 2010-11-04

Similar Documents

Publication Publication Date Title
US6550574B2 (en) Acoustic liner and a fluid pressurizing device and method utilizing same
US8197188B2 (en) Compressor
US20100278635A1 (en) Noise attenuation device for a centrifugal compressor discharge or suction nozzle
US6736238B2 (en) Air intake silencer
TWI548808B (en) Multi-stage low pressure drop muffler
JP4976046B2 (en) A silencer configured and intended for compressors
JP4532247B2 (en) Fluid flow engine
US4325459A (en) Muffler diffuser
US7854297B2 (en) Muffler and related systems
US5340275A (en) Rotary throat cutoff device and method for reducing centrifugal fan noise
WO2005119031A1 (en) Absorber silencer for compressors
JP2009264205A (en) Centrifugal compressor
JP2005069228A (en) Muffler
EP3667101B1 (en) Turbocharger system including acoustic damper for attenuating aerodynamically generated noise from compressor
CN104533843A (en) Impedance type composite muffler for turbocharger
JP6279524B2 (en) Centrifugal compressor, turbocharger
US10465687B2 (en) Device for conditioning flow of working fluids
RU2776170C1 (en) Pulsation dampener - silencer for positive displacement compressors
JP7258893B2 (en) Filter silencer for exhaust gas turbochargers of internal combustion engines
CN108591017B (en) Broadband pulsation attenuator
CN116335938A (en) Screw compressor
EP4053393A1 (en) Acoustic damper with barrier member configured to dampen acoustic energy propogating upstream in gas flow
CN117267135A (en) Exhaust bearing seat with built-in silencing structure and screw compressor
KR20120056792A (en) Blower arrangement

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20100422

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MT NL NO PL PT RO SE SI SK TR

AX Request for extension of the european patent

Extension state: AL BA MK RS

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20100810