CN1003385B - Cooling apparatus for multi-stage compression - Google Patents

Cooling apparatus for multi-stage compression Download PDF

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Publication number
CN1003385B
CN1003385B CN85105288.6A CN85105288A CN1003385B CN 1003385 B CN1003385 B CN 1003385B CN 85105288 A CN85105288 A CN 85105288A CN 1003385 B CN1003385 B CN 1003385B
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CN
China
Prior art keywords
cooling
housing
cavity
unit according
cooling unit
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Expired
Application number
CN85105288.6A
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Chinese (zh)
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CN85105288A (en
Inventor
沃尔特·科勒
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Vodafone GmbH
Original Assignee
Mannesmann 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
Priority claimed from DE3513936A external-priority patent/DE3513936C2/en
Application filed by Mannesmann AG filed Critical Mannesmann AG
Publication of CN85105288A publication Critical patent/CN85105288A/en
Publication of CN1003385B publication Critical patent/CN1003385B/en
Expired legal-status Critical Current

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Abstract

The invention relates to a cooling device for a multi-stage compressor in which two coolers are placed in a common housing. The two coolers cool the medium of the preceiding stage of the multi-stage compressor heated by the input compressor work. The common housing has chambers that are divided into different pressure stages, are connected to the multi-stage compressor by inlet tubes and outlet tubes, and contain water separators with condensate removal pipes associates with them. To be able to conduct the medium to be cooled with a minimum of pressure drops, dividing walls (13,23) are provided at a distance from the top and bottom end, respectively, of the cooling housing (50). Each dividing wall forms a cylindrical space (24,14) with the housing wall (51) and the respective end walls (57,56) of the cooling housing (50) for the installation of the water separators (15,25).

Description

The cooling unit that is used for multistage compressor
This invention relates to a kind of cooling unit that is used for multistage compressor, this device has been installed two coolers in a total housing, these two cooler coolings are compressed the prime medium of merit heating, this housing also has the chamber of several different pressures simultaneously, above-mentioned chamber links to each other with compressor with steam outlet pipe by air inlet, in the chamber in addition with the separator of condensate discharge pipe.
As cooler, often manufacturing the bottom surface when with water cooling is circular obround vessel, loads onto the cooling element of parallel to an axis in this container.Cooling water flow supercooling element, the parallel installation of separator with cooling element, medium to be cooled is by guide vane guiding (US-PS3,835918).
The most essential shortcoming of this known cooler be particularly when the installation of separator is parallel to cooling element medium to be cooled in cooler, turn to often.
Task of the present invention provides a kind of cooling unit identical with the above-mentioned type, make pressure medium loss to be cooled minimum, and cooling effect is identical.
Technical solution of the present invention is: the dividing plate perpendicular to housing shaft is installed in the front end of shrinking away from theshell body or a distance, rear end, the end wall of these dividing plates and shell body wall and housing has constituted the cylindrical cavity that can hold separator, dividing plate all has a breach, gas is flowed out by cooling element, enters in the cylindrical cavity by this breach.
In further technical solution of the present invention:
At the upper area of shell body wall, steam outlet pipe is installed in the cylindrical cavity.
Separator flatly is installed in the cylindrical cavity.
The dividing plate that a end respect to one another with shell body wall and vertical partition plate joins has been installed, this dividing plate basically with the central axes of housing.
It is directly plane that parallel baffle is in the cooling element zone, and the zone beyond this has at least an end to be spiral form.
The spiral form part of parallel baffle is made up of three straight planes at least.
Independent cavity forms the part that this cavity is positioned at the cooling element first half by the surface of the spiral form of dividing plate part, vertical partition plate and cooling element and constantly dwindles towards the direction of the cylindrical cavity that pressure is arranged.
Major part in the shell body wall upper cavity is equipped with suction tude.
Coolant intake pipe and coolant outlet hose are installed on cooling element.The axis of these pipes and the central axes of housing, and by cavity with pass end wall.
Also can make the cavity of the cooler of one cooling water input and output pipe by its place in two cooling elements.
Dispose seal element between the outer wall of cooling element and vertical partition plate, the sealing element separates the pressure chamber with the cavity that cooling water input, output tube are housed.
Because separator is installed in the space that the cooling element chamber is separated, medium to be cooled so not only vertically passes through separator, and no longer vertically passes through cooling element through aforesaid turning to, and therefore medium to be cooled only turns to twice.
Some spaces that are used for separator can utilize the whole diameter of housing, therefore allow separator that suitable size is arranged, and so just can use the whole inner chamber of circular cylindrical cavity, and separator is installed one by one in circular cylindrical cavity.
Water-cooling tube extends by each stage pressure cavity and along separator.A kind of structure of preferential employing is to make whole cooling waters be carried into by a side of cooling unit, and the cavity of each cooler and the sealing of the cavity of another cooler separate, their pressure is also different, particularly cooling element is mounted in the time of can pushing or extract out, this structure can be changed element easily.
An embodiment of this invention as shown in drawings, wherein:
Fig. 1 is the schematic representation of compressor apparatus.
Fig. 2 is a kind of cooler axonometric drawing of two chambers, the figure shows the internal structure of cooler.
Fig. 3 is the sketch of cooler.
Fig. 4 is the A-A cross section of Fig. 3.
Fig. 5 is the B-B cross section of Fig. 3.
Fig. 6 is the C-C cross section of Fig. 2.
Fig. 1 has represented the level Four band reduction gear-turbocompressor general flow chart and the cooling water sketch that have the secondary cooling.Compressor 60 has four compression stages 61 and 62,63 and 64, and they are arranged at the both sides of reduction gear box.Compression stage 61 and 62 links to each other with cooler casing 50 by connecting tube 17,18,27; Compression stage 63 and 64 joins by connecting tube 37,38,47 and another cooler casing 55, and joins by connecting tube 28 and housing 50.Cooler 10 and 20 are installed in housing 50, and cooler 30 and 40 are installed in housing 55.The pipeline that plays interconnect function between each compression stage and cooler casing can be divided into suction tude 17,27,37,47 and steam outlet pipe 18,28,38,48.Coolant intake pipe 71 and 74 leads to the cooling element 22 and 12 in the cooler casing 50, and these cooling elements always join with coolant outlet hose 72 and 75 again simultaneously.Cooling water input and output pipe correspondingly is installed on the cooling element 32 and 42 of 55 li of cooler casings too.Each cooler element all is equipped with separator 15,25,35 and 45 respectively.The coagulant that forms in the separator gathers pipe 73 derivation by condensate line 19,29,39,49 and by condensed water.
Fig. 2 shows the axonometric drawing of the housing 50 that cooler 10 and 20 are installed, and a back cooler is owing to the covering of other parts be can't see.Inside cylindrical housings (50) is cooling element 12 and 22, and their axis is parallel to each other.Between cooling element 12 and 22 is dividing plate 52, and the part that this dividing plate is positioned at cooling element 12 and 22 tops is the scroll external form and has formed independent cavity 53 and 58 with shell body wall above cooling element 12 and 22.Suction tude 17 is installed in the big zone of independent cavity 53 in the housing 51.The arrow of Fig. 2 has been pointed out the flow direction of medium to be cooled.This medium vertical current supercooling element.Front end or a distance, rear end at shrinking away from theshell body 50 are provided with dividing plate 13 and 23, and the central shaft of they and housing 50 meets at right angles.These dividing plates and shell body wall 51 and end wall 57 and 56 have respectively formed a columniform cavity 14 and 24 at each end, and dividing plate 13 has a breach 26 below cooling element 12.After medium to be cooled flows out cooling element 22, flow to cylindrical cavity 24 through breach 26, separator 25 flatly has been installed in this cavity.Come from the reason that equipment is installed, separator 25 has been separated along the Vertical direction of central shaft.With the central shaft parallel to an axis of cylindrical cavity 24 be the supplying tube 71 and 74 of cooling water, and coolant outlet hose 72 and 75.At the upper area of cylindrical cavity 24 steam outlet pipe 28 has been installed, suction tude 27 is installed in the big zone of independent cavity 58 in the housing 51.Steam outlet pipe 18 has been installed above cylindrical cavity 14.14 li separator 15 has been installed flatly at cylindrical cavity.Medium to be cooled from cooling element 12 flows out from the breach 16 on the dividing plate 23, passes above-mentioned separator again and flows to outer pipe 18, is discharged from cavity 14 or 24 by means of condensate line 19 and 29 by the water that separator is separated.
Fig. 3 has provided with sketch has different pressures grade P 1And P 2Housing 50, these pressure ratings are separated from each other by dividing plate 52 and dividing plate 13 and 23.Cooling element 12 and 22 is installed with parallel to each other.The top of dividing plate 52 is spiral, and this scroll is made up of three straight planes at least.Suction tude 17 and 27 is installed in the top of housing 50.
Get terribly because the spiral shape of dividing plate 52 is crooked, thereby can in sizable scope, change the link position of supplying tube according to the needs of operation.Steam outlet pipe 18 or 28 is installed in the top of housing equally, equally also can adapt to the actual conditions of operation by the position that changes joint.Cooling water input and output pipe 71,72 or 74,75 is by cylindrical cavity 24.
The A-A cross section of Fig. 4 presentation graphs 3.Dividing plate 13 is with cooling element 12 sealings and a breach 26 that leads to cooling element 22 is arranged.Flatly be installed with at 24 li separators 25 of cylindrical cavity, coagulant is derived by condensate line 29.Medium to be cooled vertically passes through separator, and flows out housing 50 by steam outlet pipe 28.
Fig. 5 shows the B-B cross section of Fig. 3.Enter in the housing 50 by suction tude 27 media to be cooled, and it is mobile towards cooling element 22 to pass dividing plate 52.According to the degree of crook of dividing plate 52 spiral parts, can in the quite wide scope in the top of housing 50, be installed into tracheae 27.
Fig. 6 has provided C-C cross section, Fig. 2 cavity 24 position.Coolant intake pipe 74 and coolant outlet hose 75 communicate with cooling element 12 in being in chamber 11 at the end face of cooling element 12.Pair of pipes 74 and 75 is passed the end wall 57 of cavity 24, and the mounting hole that can seal 59 is arranged on end wall 57, and cooling element 12 can be extracted out from this hole.Between the outer wall of cooling element 12 and dividing plate 13 seal element 80 has been installed, the sealing element is divided into different pressure to chamber 11 with cylindrical chamber 24.21(does not express in the drawings by chamber) after effluent air passes cavity 24,, discharge cavity 24 again by steam outlet pipe 28.Separator (25) is mounted to and crosses gas flow direction, and the condensation product that is separated will be discharged by condensate line 29.

Claims (10)

1, a kind of cooling unit that is used for multistage compressor, it has installed two coolers (10 in a total housing (50), 20), a cooling element (12 is arranged in each cooler, 22), so that cooling is through the medium of prime compression, two dividing plates vertical with the housing central shaft (13 are equipped with in front end or a distance, rear end at shrinking away from theshell body (50), 23), aforementioned barriers and shell body wall (51) and housing two ends end wall (57,56) constituted and to have held separator (15,25) two cylindrical cavities (14,24), housing (50) has the chamber of two above different pressures, described chamber links to each other with compressor with steam outlet pipe by suction tude, it is characterized in that above-mentioned vertical partition plate (13,23) breach (26 is respectively arranged, 16), two-way gas is respectively from above-mentioned two cooling elements (22,12) flow out, through breach (26,16) enter cylindrical cavity (24,14) in, also has a dividing plate (52) parallel substantially in the housing (50) with the housing central shaft, it and shell body wall (51) and two vertical partition plates (13,23) intersect, thereby constituted the chamber of above-mentioned different pressures.
2, cooling unit according to claim 1 is characterized by: in cylindrical cavity (14,24), at the upper area of shell body wall 51 steam outlet pipe (18,28) is installed.
3, cooling unit according to claim 1 is characterized by: the separator (15,25) in the cylindrical cavity (14,24) is for flatly placing.
4, cooling unit according to claim 1 is characterized by: above-mentioned parallel baffle (52) presents directly plane in cooling element (12,22) zone, and the zone beyond this has at least an end to be spiral form.
5, cooling unit according to claim 4 is characterized by: the spiral form part of above-mentioned parallel baffle (52) is made up of three straight planes at least.
6, cooling unit according to claim 5, it is characterized by: by the independent cavity (53,58) that the surface of the spiral form of parallel baffle (52) part, two vertical partition plates (13,23) and two cooling elements (12,22) forms respectively, its part that is positioned at the cooling element first half diminishes gradually towards the direction of the cylindrical cavity that pressure is arranged (14,24).
7, cooling unit according to claim 6 is characterized by: the major part in shell body wall (51) upper cavity (53) is equipped with suction tude (17,27).
8, cooling unit according to claim 1, it is characterized by: on two cooling elements (12,22), be separately installed with coolant intake pipe (71,74) and coolant outlet hose (72,75), the central axes of the axis of these pipes and housing (50), and by cavity (14,24) with pass end wall (56,57).
9, cooling unit according to claim 1 is characterized by: the cooling water input and output pipe (71,72) of (12) in two cooling elements is by the cavity (24) of the cooler (20) at its place.
10, cooling unit according to claim 9 is characterized by: dispose seal element (80) between the outer wall of above-mentioned cooling element (12) and vertical partition plate (13): the sealing element separates pressure chamber (11) and cavity (24) that cooling water input, output tube be housed.
CN85105288.6A 1985-04-15 1985-07-10 Cooling apparatus for multi-stage compression Expired CN1003385B (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3513936A DE3513936C2 (en) 1984-08-17 1985-04-15 Cooling device for a multi-stage compressor
DEP3513936.6 1985-04-15

Publications (2)

Publication Number Publication Date
CN85105288A CN85105288A (en) 1987-01-07
CN1003385B true CN1003385B (en) 1989-02-22

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Application Number Title Priority Date Filing Date
CN85105288.6A Expired CN1003385B (en) 1985-04-15 1985-07-10 Cooling apparatus for multi-stage compression

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1091849C (en) * 1996-10-23 2002-10-02 阿尔斯通公司 Blade carrier for compressor

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1916410B (en) * 2005-08-19 2010-10-06 科拉克集团公开公司 Multi-stage oil-less gas compressor
CN103423130A (en) * 2013-09-10 2013-12-04 无锡市豫达换热器有限公司 Efficient air heat exchanger based on integrated technology

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1091849C (en) * 1996-10-23 2002-10-02 阿尔斯通公司 Blade carrier for compressor

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