EP2572108A1 - Centrifugal compressor - Google Patents
Centrifugal compressorInfo
- Publication number
- EP2572108A1 EP2572108A1 EP11721272A EP11721272A EP2572108A1 EP 2572108 A1 EP2572108 A1 EP 2572108A1 EP 11721272 A EP11721272 A EP 11721272A EP 11721272 A EP11721272 A EP 11721272A EP 2572108 A1 EP2572108 A1 EP 2572108A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- shaft
- centrifugal compressor
- shaft end
- housing
- spiral
- 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.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/083—Sealings especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
- F04D17/122—Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
Definitions
- the invention relates to a centrifugal compressor having a shaft extending along a machine axis, wherein a drive on the side of a collecting spiral, the
- Machine module collects which drive on one of a
- Housing of the centrifugal compressor guided out shaft end is disposed, wherein at an opposite shaft end of the shaft axial suction is provided at an overhang stage of the centrifugal compressor.
- Such compressors are used in particular for compressing large volume flows (eg 600,000 m 3 per hour) to pressures of, for example, 8 bar.
- the axial suction here has the advantage that the suction is designed to be particularly large and at the same time the maximum diameter of the wheels remains moderate, so that the machine can be operated at higher speeds without overloading the materials of the rotating parts.
- Cooling unit Regularly, such a collecting spiral is a slightly helically executed annular chamber whose cross-sectional area is in the circumferential direction
- the invention has therefore taken on the task of improving the initially defined centrifugal compressor such that on the one hand the production cost is reduced and on the other hand no high pressure losses in the
- Circumference is undivided and is flanged to the housing of the centrifugal compressor.
- the tolerance chain between the wheels of the shaft and opposite inner surfaces of the housing is particularly short.
- Centrifugal compressor on one side final component as it formed a lid Accordingly, the number of components is reduced.
- the directional data axial, radial, circumferential direction always refer to the machine axis.
- the invention is based on a special
- Figure 1 is a schematic representation of a
- FIG. 1 shows a schematic longitudinal section through a compressor CO according to the invention.
- Essential components of the compressor CO are a housing C, a shaft SH, the wheels IM, of which only one is shown and carries an overhang stage ST, one to the housing C.
- the shaft SH extends along a machine axis AX, which is the axis of rotation of the drive D at the same time.
- Process fluid F is axially drawn in by the compressor CO and enters an overhang stage ST, is further compressed downstream by means of impellers IM, and enters a final stage LST to be subsequently collected in the collection coil CC for entry into the subsequent machine modules.
- the shaft SH is mounted in two radial bearings BEI, BE2.
- the shaft SH has a first shaft end SEI and a second shaft end SE2, wherein the first shaft end SEI is driven by the drive D and the second
- End of the shaft SE2 carries the overhang ST.
- Shaft end SEI, SE2 the invention means a portion of the shaft extending from the respective end of the shaft in the direction of the shaft center, wherein about one third of the
- the shaft end In the region of the first shaft end SEI, in addition to the torque-transmitting connection with the drive D, the collecting spiral CC, the second radial BE2 and a shaft seal SHS
- Machine axis AX has a parting line is the
- the collecting spiral CC carries the second radial bearing BE2 and the shaft seal SHS.
- Design of the collecting spiral which is designed as a casting, has the advantage that it does not have any paragraph otherwise caused by a parting line in the circumferential direction, which could cause flow losses.
- the attachment of the second radial bearing BE2 and the shaft seal SHS to the collecting spiral CC has the shortest possible tolerance chain between the radial bearing B2 and the shaft seal SHS result so that necessary for example thermal expansions radial clearances of the shaft SH in the shaft seal SHS can be minimal. In this way, a particularly good efficiency can be achieved.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102010020891 | 2010-05-18 | ||
PCT/EP2011/057660 WO2011144515A1 (en) | 2010-05-18 | 2011-05-12 | Centrifugal compressor |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2572108A1 true EP2572108A1 (en) | 2013-03-27 |
EP2572108B1 EP2572108B1 (en) | 2015-08-26 |
Family
ID=44312333
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11721272.0A Not-in-force EP2572108B1 (en) | 2010-05-18 | 2011-05-12 | Centrifugal compressor |
Country Status (4)
Country | Link |
---|---|
US (1) | US20130064659A1 (en) |
EP (1) | EP2572108B1 (en) |
CN (1) | CN102893033B (en) |
WO (1) | WO2011144515A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
TWI748546B (en) | 2011-12-06 | 2021-12-01 | 日商佳能股份有限公司 | Rotational force transmission unit |
US9689502B2 (en) | 2015-10-26 | 2017-06-27 | Rolls-Royce Corporation | Rotary exhaust valve system |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE503754C (en) * | 1928-04-11 | 1930-07-26 | Siemens Schuckertwerke Akt Ges | Centrifugal compressor with housing cooling |
US2476191A (en) * | 1945-06-15 | 1949-07-12 | Westinghouse Electric Corp | Multistage, axial flow, gas compressor |
US2578617A (en) * | 1946-11-15 | 1951-12-11 | Worthington Pump & Mach Corp | Multistage centrifugal compressor |
DE835341C (en) * | 1948-11-28 | 1952-03-31 | Diederich Storjohann | Saucepan handle |
CH676487A5 (en) * | 1988-10-19 | 1991-01-31 | Proizv Ob Nevsky Z Im V I | |
JP3799121B2 (en) * | 1997-03-19 | 2006-07-19 | 株式会社 日立インダストリイズ | 2-stage centrifugal compressor |
BR0008359A (en) * | 1999-01-25 | 2001-11-27 | Elliott Turbo | Housing for rotating machines, method for manufacturing a portion of housing and high pressure housing |
US6345503B1 (en) * | 2000-09-21 | 2002-02-12 | Caterpillar Inc. | Multi-stage compressor in a turbocharger and method of configuring same |
GB2400631B (en) * | 2003-04-16 | 2006-07-05 | Adrian Alexander Hubbard | Compound centrifugal and screw compressor |
EP2050968A1 (en) * | 2007-10-19 | 2009-04-22 | Siemens Aktiengesellschaft | Pressure container with a cover |
US8292576B2 (en) * | 2008-03-31 | 2012-10-23 | Honeywell International Inc. | Compressor scrolls for auxiliary power units |
DE102008057472B4 (en) * | 2008-11-14 | 2011-07-14 | Atlas Copco Energas GmbH, 50999 | Multi-stage radial turbocompressor |
-
2011
- 2011-05-12 CN CN201180024259.4A patent/CN102893033B/en not_active Expired - Fee Related
- 2011-05-12 US US13/698,317 patent/US20130064659A1/en not_active Abandoned
- 2011-05-12 EP EP11721272.0A patent/EP2572108B1/en not_active Not-in-force
- 2011-05-12 WO PCT/EP2011/057660 patent/WO2011144515A1/en active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of WO2011144515A1 * |
Also Published As
Publication number | Publication date |
---|---|
WO2011144515A1 (en) | 2011-11-24 |
US20130064659A1 (en) | 2013-03-14 |
EP2572108B1 (en) | 2015-08-26 |
CN102893033A (en) | 2013-01-23 |
CN102893033B (en) | 2015-06-03 |
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