CN108443112A - A kind of exhaust system for reciprocating compressor - Google Patents

A kind of exhaust system for reciprocating compressor Download PDF

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Publication number
CN108443112A
CN108443112A CN201810272845.4A CN201810272845A CN108443112A CN 108443112 A CN108443112 A CN 108443112A CN 201810272845 A CN201810272845 A CN 201810272845A CN 108443112 A CN108443112 A CN 108443112A
Authority
CN
China
Prior art keywords
air cavity
row air
discharge chamber
cylinder head
crankcase
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.)
Pending
Application number
CN201810272845.4A
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Chinese (zh)
Inventor
储呈国
郑佳欢
吴斌
陆龙泉
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.)
Jiaxipera Compressor Co Ltd
Original Assignee
Jiaxipera Compressor Co Ltd
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 Jiaxipera Compressor Co Ltd filed Critical Jiaxipera Compressor Co Ltd
Priority to CN201810272845.4A priority Critical patent/CN108443112A/en
Publication of CN108443112A publication Critical patent/CN108443112A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/0027Pulsation and noise damping means
    • F04B39/0055Pulsation and noise damping means with a special shape of fluid passage, e.g. bends, throttles, diameter changes, pipes

Abstract

The invention discloses a kind of exhaust systems for reciprocating compressor, including crankcase, cylinder, cylinder head and interior comb, high pressure chest is equipped in cylinder head, crankcase is equipped with first row air cavity, second row air cavity, third discharge chamber and the first cushion chamber, it is respectively equipped with through-hole between high pressure chest in cylinder head and first row air cavity, between first row air cavity and second row air cavity, between third discharge chamber and the first cushion chamber, it is connected to by connecting tube between second row air cavity and third discharge chamber, interior comb is connected with third discharge chamber.The present invention has given full play to the effect of four exhaust cavitys on crankcase, and the exhaust gas pulses of compressor are minimized.Meanwhile without increasing too many part when implementation, pass through the setting of the order of connection and throttle orifice of cavity of arranging, you can reduce exhaust gas pulses, application cost is relatively low.

Description

A kind of exhaust system for reciprocating compressor
Technical field
The present invention relates to technical field of refrigeration compressors, specifically a kind of for arranging refrigerant on reciprocating compressor Go out the exhaust system of shell.
Background technology
The movement of compressor piston makes inner pressure of air cylinder change, so as to cause the opening and closing of suction valve chip. When piston is moved to cylinder head, the pressure in cylinder can increase;When the pressure in cylinder is more than the pressure in shell, inhale Air valve is closed;When the pressure in cylinder continues growing and is more than the pressure in discharge chamber, air bleeding valve is opened, and refrigerant enters gas High pressure chest in cylinder cap enters back into interior comb subsequently into the discharge chamber on crankcase, finally enters the exhaust pipe row of compressor Go out except compressor housing.High pressure chest of the refrigerant of high temperature and pressure out of cylinder head, into the discharge chamber on crankcase this The operating path of section gas has prodigious relationship with compressor air-discharging pulsation.In addition the position of throttle orifice is also to compressor Exhaust gas pulses have prodigious relationship.Since the structure of the exhaust system of existing crankcase is more complicated, crankcase casting cost ratio It is higher, while because that can not arrange throttle orifice in the grate flow channel of existing crankcase, thus exhaust gas pulses are bigger.
Invention content
Technical problem to be solved by the present invention lies in a kind of exhaust gas pulses that can effectively reduce compressor are proposed, it is implemented as This lower exhaust system for reciprocating compressor.
In order to solve the above technical problems, a kind of exhaust system for reciprocating compressor of the invention include crankcase, cylinder, Cylinder head and interior comb, are equipped with high pressure chest in the cylinder head, the crankcase be equipped with first row air cavity, second row air cavity, Third discharge chamber and the first cushion chamber, between the high pressure chest and the first row air cavity in the cylinder head, described first It is respectively equipped with through-hole between discharge chamber and the second row air cavity, between the third discharge chamber and first cushion chamber, institute It states and is connected to by connecting tube between second row air cavity and the third discharge chamber, the interior comb and the third discharge chamber phase Even.
Above-mentioned a kind of exhaust system for reciprocating compressor, between the first row air cavity and the second row air cavity The through-hole is throttle orifice.
For the present invention as a result of above-mentioned technical pattern, it has given full play to the effect of four exhaust cavitys on crankcase, The exhaust gas pulses of compressor are minimized.Meanwhile without increasing too many part when implementation, the connection by cavity of arranging is suitable The setting of sequence and throttle orifice, you can reduce exhaust gas pulses, application cost is relatively low.
Description of the drawings
Fig. 1 is the structural schematic diagram of exhaust system embodiment one of the present invention;
Fig. 2 is the structural schematic diagram of exhaust system embodiment two of the present invention;
Fig. 3 is the structural schematic diagram of exhaust system embodiment three of the present invention;
Fig. 4 is the structural schematic diagram of exhaust system embodiment four of the present invention;
Fig. 5 is the structural schematic diagram of exhaust system embodiment five of the present invention;
Fig. 6 is the dimensional structure diagram of crankcase used in scheme shown in Fig. 2;
Fig. 7 is the dimensional structure diagram of scheme exhaust system shown in Fig. 2;
Fig. 8 is the pressure fluctuation situation schematic diagram of interior comb outlet under the conditions of each scheme.
Specific implementation mode
In order to obtain preferable exhaust system, the present invention devises five kinds of exhaust system schemes, lists possible exhaust line The location arrangements of diameter and throttle orifice carry out analogue simulation and experiment test, with the preferable exhaust system scheme of determination so that Exhaust gas pulses are minimum.
Such as Fig. 1, exhaust system scheme one includes cylinder 1k, cylinder head 3, first row air cavity 1a, second row air cavity 1b, connection Pipe 4, third discharge chamber 1c, the first cushion chamber 1d and interior comb 5.The high temperature and high pressure gas through overcompression initially enters in cylinder 1k High pressure chest 3a in cylinder head 3, then by being connected to the through-hole 1e of first row air cavity 1a, into first row air cavity 1a;Then lead to The through-hole 1g for crossing connection second row air cavity 1b, into second row air cavity 1b;Then by connecting tube 4, into third discharge chamber 1c, Part of refrigerant enters interior comb 5, and part of refrigerant enters the through-hole 1h of the first cushion chamber 1d of connection, finally returns the Three discharge chamber 1c, enter back into interior comb 5.
As shown in Fig. 2, exhaust system scheme two includes cylinder 1k, cylinder head 3, high pressure chest 3a, connection first row air cavity 1a Through-hole 1e, first row air cavity 1a, the through-hole 1g of connection second row air cavity 1b, second row air cavity 1b, connecting tube 4, third exhaust Chamber 1c, through-hole 1h, the first cushion chamber 1d and the interior comb 5 for being connected to the first cushion chamber 1d, the high temperature through overcompression is high in cylinder 1k Body of calming the anger initially enters the high pressure chest 3a in cylinder head 3, then by being connected to the through-hole 1e of first row air cavity 1a, into first row Air cavity 1a;Then by being connected to the through-hole 1g of second row air cavity 1b, into second row air cavity 1b(Through-hole 1g is throttle orifice, is passed through Throttling action is played in reduced bore, reduces exhaust gas pulses);Then by connecting tube 4, into third discharge chamber 1c, part system Cryogen enters interior comb 5, and part of refrigerant enters the through-hole 1h of the first cushion chamber 1d of connection, finally returns third discharge chamber 1c enters back into interior comb 5.
As shown in figure 3, in exhaust system scheme three of the present invention, in cylinder 1k the high temperature and high pressure gas through overcompression first into Enter the high pressure chest 3a in cylinder head 3, then by being connected to the through-hole 1e of first row air cavity 1a, into first row air cavity 1a;Then By being connected to the through-hole 1g of second row air cavity 1b, into second row air cavity 1b;Then by connecting tube 4, into discharge chamber 1d, then Into discharge chamber 1c, interior comb 5 is finally entered back into.
As shown in figure 4, in exhaust system scheme four of the present invention, in cylinder 1k the high temperature and high pressure gas through overcompression first into Enter the high pressure chest 3a in cylinder head 3, then by being connected to the through-hole 1e of first row air cavity 1a, into first row air cavity 1a;Then By being connected to the through-hole 1g of second row air cavity 1b, in through-hole 1g setting throttlings, into second row air cavity 1b;Then pass through connecting tube 4, into discharge chamber 1d, discharge chamber 1c is entered back into, finally enters interior comb 5.
As shown in figure 5, in exhaust system scheme five of the present invention, in cylinder 1k the high temperature and high pressure gas through overcompression first into Enter the high pressure chest 3a in cylinder head 3, part of refrigerant is directly entered discharge chamber 1d(The chamber is same knot with aforementioned cushion chamber Structure, only because the sequence that gas flows through is different, role is also different), into discharge chamber 1c, finally enter interior comb 5;It is another Some refrigerant is introduced into cushion chamber 1a(Similarly, the cavity and aforementioned discharge chamber are same structure, only because gas flows through Sequence is different, and role is also different), by through-hole 1g, throttling is set at through-hole 1g, enters back into cushion chamber 1b, then again Cushion chamber 1a is returned to, high pressure chest 3a is returned to, into discharge chamber 1d, discharge chamber 1c is entered back into, finally enters interior comb 5.
As shown in figure 8, by simulation calculation and experiment, exhaust gas pulses minimum is scheme two shown in Fig. 2.When implementation, As shown in Figure 6 and Figure 7, simultaneously provided with first row air cavity 1a, second row air cavity 1b, third discharge chamber 1c and the on crankcase 1 One cushion chamber 1d is also equipped with connection first row air cavity 1a and the through-hole 1e of high pressure chest 3a on crankcase 1, is connected to third discharge chamber 1c With the through-hole 1h of the first cushion chamber 1d, the logical of connection first row air cavity 1a and second row air cavity 1b is provided on crankcase 1 simultaneously Hole 1g, the through-hole play throttling action by reduced bore, reduce exhaust gas pulses.

Claims (2)

1. a kind of exhaust system for reciprocating compressor, including crankcase, cylinder, cylinder head and interior comb, the cylinder head It is interior to be equipped with high pressure chest, which is characterized in that the crankcase is equipped with first row air cavity, second row air cavity, third discharge chamber and the One cushion chamber, between the high pressure chest and the first row air cavity in the cylinder head, the first row air cavity and described the Between two discharge chambers, be respectively equipped with through-hole between the third discharge chamber and first cushion chamber, the second row air cavity and It is connected to by connecting tube between the third discharge chamber, the interior comb is connected with the third discharge chamber.
2. a kind of exhaust system for reciprocating compressor as described in claim 1, which is characterized in that the first row air cavity The through-hole between the second row air cavity is throttle orifice.
CN201810272845.4A 2018-03-29 2018-03-29 A kind of exhaust system for reciprocating compressor Pending CN108443112A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810272845.4A CN108443112A (en) 2018-03-29 2018-03-29 A kind of exhaust system for reciprocating compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810272845.4A CN108443112A (en) 2018-03-29 2018-03-29 A kind of exhaust system for reciprocating compressor

Publications (1)

Publication Number Publication Date
CN108443112A true CN108443112A (en) 2018-08-24

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CN201810272845.4A Pending CN108443112A (en) 2018-03-29 2018-03-29 A kind of exhaust system for reciprocating compressor

Country Status (1)

Country Link
CN (1) CN108443112A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112177878A (en) * 2020-08-21 2021-01-05 珠海格力节能环保制冷技术研究中心有限公司 Gas circuit structure, compressor and refrigerator

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1364980A (en) * 2001-01-19 2002-08-21 三星光州电子株式会社 Reciprocating compressor with exhaust pulse lowering structure
CN101446284A (en) * 2008-12-31 2009-06-03 广州冷机股份有限公司 Reciprocating sealed compressor
CN202187882U (en) * 2011-07-02 2012-04-11 胡雪群 Compressor frame
CN105673449A (en) * 2016-03-25 2016-06-15 芜湖欧宝机电有限公司 Noise reduction and energy conservation piston type compressor
CN208236599U (en) * 2018-03-29 2018-12-14 加西贝拉压缩机有限公司 A kind of exhaust system for reciprocating compressor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1364980A (en) * 2001-01-19 2002-08-21 三星光州电子株式会社 Reciprocating compressor with exhaust pulse lowering structure
CN101446284A (en) * 2008-12-31 2009-06-03 广州冷机股份有限公司 Reciprocating sealed compressor
CN202187882U (en) * 2011-07-02 2012-04-11 胡雪群 Compressor frame
CN105673449A (en) * 2016-03-25 2016-06-15 芜湖欧宝机电有限公司 Noise reduction and energy conservation piston type compressor
CN208236599U (en) * 2018-03-29 2018-12-14 加西贝拉压缩机有限公司 A kind of exhaust system for reciprocating compressor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112177878A (en) * 2020-08-21 2021-01-05 珠海格力节能环保制冷技术研究中心有限公司 Gas circuit structure, compressor and refrigerator

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