CN106122028A - Compressor - Google Patents

Compressor Download PDF

Info

Publication number
CN106122028A
CN106122028A CN201610605801.XA CN201610605801A CN106122028A CN 106122028 A CN106122028 A CN 106122028A CN 201610605801 A CN201610605801 A CN 201610605801A CN 106122028 A CN106122028 A CN 106122028A
Authority
CN
China
Prior art keywords
airway
compressor
heat
assembly
airways
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
CN201610605801.XA
Other languages
Chinese (zh)
Inventor
方智祥
康晓虎
高斌
达拉
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.)
Guangdong Midea Toshiba Compressor Corp
Guangdong Meizhi Compressor Co Ltd
Anhui Meizhi Precision Manufacturing Co Ltd
Original Assignee
Guangdong Meizhi Compressor Co Ltd
Anhui Meizhi Precision Manufacturing 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 Guangdong Meizhi Compressor Co Ltd, Anhui Meizhi Precision Manufacturing Co Ltd filed Critical Guangdong Meizhi Compressor Co Ltd
Priority to CN201610605801.XA priority Critical patent/CN106122028A/en
Publication of CN106122028A publication Critical patent/CN106122028A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/04Heating; Cooling; Heat insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/12Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet

Abstract

The invention discloses a kind of compressor, including: housing, airway assembly and suction nozzle, it is provided with compression mechanism in housing, compression mechanism has compression chamber;One end of airway assembly is connected with compression mechanism through housing and connects with compression chamber inside, airway assembly includes the inside and outside nested at least two airway arranged, heat-insulation chamber is limited between two airways the most adjacent at least two airway, the minimum thickness of heat-insulation chamber is that C, C meet: C >=0.2mm;Suction nozzle is connected with the other end of airway.Compressor according to the present invention, it is effectively improved effect of heat insulation and the reliability of heat-insulation chamber, reduce the conduction of heat between adjacent two airway, thus efficiently reduce the heating to the gas flowing through airway assembly, reduce suction superheat, and then improve the refrigerating capacity of compressor, and improve efficiency and the efficiency of compressor.Additionally, also reduce difficulty of processing, thus reduce processing cost.

Description

Compressor
Technical field
The present invention relates to Compressor Technology field, especially relate to a kind of compressor.
Background technology
In correlation technique, compressor such as high back pressure compressor, in running, is High Temperature High Pressure in compression case body There is the bigger temperature difference in the gas in gas, with airway assembly, the gas in airway assembly passes through inducing QI tube wall from housing Gas absorbs heat, increases air-breathing heat exchange amount.But, owing to the heat of the gas suction in airway assembly is not from cold But medium, occurs the air-breathing heat exchange in airway assembly to belong to invalid heat exchange, thus increases inspiratory volume, reduce compression The compression efficiency of machine.
In correlation technique, in order to solve the problem of above-mentioned invalid heat exchange, some producers use to be increased in airway assembly The instlated tubular of macromolecule heat-barrier material such as engineering plastics class reduces air-breathing heat exchange amount, but in welding process, engineering plastic Material pipe is heated and easily melts, and reliability is low and range is limited.Additionally, the heat conductivity of engineering plastics pipe is higher, heat insulation effect The most bad.
Summary of the invention
It is contemplated that at least solve one of technical problem present in prior art.To this end, one object of the present invention Being to propose a kind of compressor, the compression efficiency of this compressor is high.
According to the compressor of the present invention, including: housing, it is provided with compression mechanism in described housing, described compression mechanism has Compression chamber;Airway assembly, one end of described airway assembly is connected and with described through described housing with described compression mechanism The internal connection of compression chamber, described airway assembly includes the inside and outside nested at least two airway arranged, and described at least two is led Limiting heat-insulation chamber between two described airways the most adjacent in trachea, the minimum thickness of described heat-insulation chamber is C, and described C is full Foot: C >=0.2mm;Suction nozzle, described suction nozzle is connected with the other end of described airway assembly.
According to the compressor of the present invention, by arranging the inside and outside nested at least two inducing QI arranged in airway assembly Pipe, and between two the most adjacent airways, limit heat-insulation chamber, and the thickness C of heat-insulation chamber is met: C >=0.2mm, by This, be effectively improved effect of heat insulation and the reliability of heat-insulation chamber, reduces the conduction of heat between adjacent two airway, from And efficiently reduce the heating to the gas flowing through airway assembly, reduce suction superheat, and then improve compressor Refrigerating capacity, and improve efficiency and the efficiency of compressor.Additionally, also significantly reduce the difficulty of processing of airway assembly, Improve the production efficiency of airway assembly, thus reduce the processing cost of compressor.
It addition, can also have the technical characteristic added as follows according to the compressor of the present invention:
According to some embodiments of the present invention, at least one end of described at least two airway is tightly connected.
Alternatively, described at least one end welding of described at least two airway, bonding or interference fit.
According to some embodiments of the present invention, the length of fit of described at least one end of described at least two airway is B, Described B meets: 0.5mm≤B≤5mm.
According to some embodiments of the present invention, in the most adjacent said two airway in described at least two airway The wall thickness of outer layer airway be t1, described t1 meets: 0.3mm≤t1≤3mm.
According to some embodiments of the present invention, in the most adjacent said two airway in described at least two airway The wall thickness of internal layer airway be t2, described t2 meets: 0.3mm≤t2≤3mm.
According to some embodiments of the present invention, described heat-insulation chamber is vacuum cavity.
According to other embodiments of the present invention, described compressor farther includes: thermal insulation barriers, and described thermal insulation barriers is filled in In described heat-insulation chamber.
Alternatively, the heat conductivity of described thermal insulation barriers is less than the heat conductivity of described airway.
According to some embodiments of the present invention, described suction nozzle and described airway assembly are formed as Split type structure or one Structure.
The additional aspect of the present invention and advantage will part be given in the following description, and part will become from the following description Obtain substantially, or recognized by the practice of the present invention.
Accompanying drawing explanation
Above-mentioned and/or the additional aspect of the present invention and advantage are from combining the accompanying drawings below description to embodiment and will become Substantially with easy to understand, wherein:
Fig. 1 is the structural representation of compressor according to embodiments of the present invention;
Fig. 2 is the partial structurtes schematic diagram of compressor according to embodiments of the present invention;
Fig. 3 is the structural representation of the airway assembly shown in Fig. 2;
Fig. 4 is the structural representation of the airway assembly according to second embodiment of the invention;
Fig. 5 is the structural representation of the airway assembly according to third embodiment of the invention;
Fig. 6 is the structural representation of the airway assembly according to four embodiment of the invention;
Fig. 7 is the structural representation of the airway assembly according to fifth embodiment of the invention;
Fig. 8 is the structural representation of the airway assembly according to sixth embodiment of the invention;
Fig. 9 is the structural representation of the airway assembly according to seventh embodiment of the invention;
Figure 10 is the structural representation of airway assembly according to embodiments of the present invention and suction nozzle;
Figure 11 is the structural representation of airway assembly and suction nozzle in accordance with another embodiment of the present invention.
Reference:
Compressor 100,
Housing 1, installing hole 11, connecting tube 12,
Airway assembly 2, airway 21, heat-insulation chamber 22, stage portion 23, bending part 24, connection bump 25, flanging 26, mistake Cross portion 27,
Compression mechanism 3, base bearing 31, supplementary bearing 32, cylinder assembly 33, compression chamber 331, bent axle 34,
Rotor 4, reservoir 5, suction nozzle 6.
Detailed description of the invention
Embodiments of the invention are described below in detail, and the example of described embodiment is shown in the drawings, the most from start to finish Same or similar label represents same or similar element or has the element of same or like function.Below with reference to attached The embodiment that figure describes is exemplary, is only used for explaining the present invention, and is not considered as limiting the invention.
In describing the invention, it is to be understood that term " " center ", " thickness ", " on ", D score, "left", "right", The orientation of the instruction such as " vertically ", " level ", " top ", " end ", " interior ", " outward ", " axially ", " radially ", " circumferential " or position relationship For based on orientation shown in the drawings or position relationship, be for only for ease of the description present invention and simplifying describe rather than instruction or Hint indication device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that Limitation of the present invention.Additionally, term " first ", " second " are only used for describing purpose, and it is not intended that instruction or hint phase To importance or the implicit quantity indicating indicated technical characteristic.Thus, define " first ", " second " feature permissible Express or implicitly include one or more this feature.In describing the invention, except as otherwise noted, " multiple " It is meant that two or more.
In describing the invention, it should be noted that unless otherwise clearly defined and limited, term " is installed ", " phase Even ", " connection " should be interpreted broadly, for example, it may be fixing connection, it is also possible to be to removably connect, or be integrally connected;Can To be mechanical connection, it is also possible to be electrical connection;Can be to be joined directly together, it is also possible to be indirectly connected to by intermediary, Ke Yishi The connection of two element internals.For the ordinary skill in the art, can understand that above-mentioned term is at this with concrete condition Concrete meaning in invention.
Below with reference to Fig. 1-Figure 11, compressor 100 according to embodiments of the present invention is described.Wherein, compressor 100 can be Rotary compressor, but it is not limited to this.
Alternatively, compressor 100 can be vertical compressor.Certainly, those skilled in the art are appreciated that compression Machine 100 can also be horizontal compressor (not shown).Here, it should be noted that " vertical compressor " can be understood as pressure The central axis upright of the cylinder of the compression mechanism 3 of contracting machine 100 is in the compressor 100 of the installed surface of compressor 100, such as, as Shown in Fig. 1, the central axis of cylinder vertically extends.Correspondingly, " horizontal compressor " can be understood as the center of cylinder Axis is parallel to the compressor 100 of the installed surface of compressor 100.In the application explained below, with compressor 100 for vertical Illustrate as a example by compressor.
As depicted in figs. 1 and 2, compressor 100 according to embodiments of the present invention, including: housing 1, airway assembly 2 and suction Trachea 6.
Specifically, being provided with compression mechanism 3 in housing 1, compression mechanism 3 has compression chamber 331.With reference to Fig. 1, compress mechanism 3 Can include bent axle 34, base bearing 31, supplementary bearing 32 and be located at base bearing 31 and and supplementary bearing 32 between cylinder assembly 33.Pressure Contracting chamber 331 can be formed on cylinder assembly 33.Base bearing 31 and supplementary bearing 32 are respectively provided at the axial two ends of cylinder assembly 33, Such as, in the example of fig. 1, base bearing 31 is positioned at the upper end of cylinder assembly 33, and supplementary bearing 32 is positioned at the lower end of cylinder assembly 33. Base bearing 31, cylinder assembly 33 and supplementary bearing 32 are run through in one end (such as, the lower end in Fig. 1) of bent axle 34, another of bent axle 34 End (such as, the upper end in Fig. 1) is connected with the rotor 4 of compressor 100 motor.After the electrical power of compressor 100, rotor 4 carries The bent axle 34 of dynamic pressure contracting mechanism 3 rotates, and makes compression mechanism 3 constantly suck low-temp low-pressure coolant, compression eventually through exhauster It is internal that High Temperature High Pressure coolant is expelled to housing 1 by structure, it is achieved the continuous work of compressor 100.
One end (such as, the left end in Fig. 1) of airway assembly 2 is connected and and compression chamber through housing 1 with compression mechanism 3 331 internal connections.Airway assembly 2 is used for deriving coolant and being imported by coolant in compression chamber 331 so that coolant is in compression mechanism Compress in 3.Specifically, seeing figures.1.and.2, housing 1 can be provided with installing hole 11, above-mentioned one end of airway assembly 2 is permissible It is connected through installing hole 11 with compression mechanism 3 and connects with the inside of compression chamber 331.
Further, can be provided with connecting tube 12 at installing hole 11, connecting tube 12 is stretched in above-mentioned one end of airway assembly 2 In connect with compression chamber 331.Airway assembly 2 can coordinate with connecting tube 12, to be fixed on housing 1 by airway assembly 2. Alternatively, the outer surface of airway assembly 2 can be tightly connected with connecting tube 12, and such as airway assembly 2 can weld or viscous It is connected in connecting tube 12.Thus, the position that can make airway assembly 2 is stable, and technique is simple, easy to process.
Alternatively, compressor 100 also includes reservoir 5.Reservoir 5 can pass through airway assembly 2 and compressor 100 phase Even, to provide coolant to compressor 100, but it is not limited to this.Such as, compressor 100 can also be introduced by other pipe-line systems Coolant, this is not especially limited by the present invention.
One end (such as, the upper end in Fig. 1) of suction nozzle 6 can be connected with reservoir 5, the other end (example of suction nozzle 6 As, the left end in Fig. 1) can be connected with the other end (such as, the right-hand member in Fig. 1) of airway assembly 2.Suction nozzle 6 can be used In the coolant in reservoir 5 is introduced airway assembly 2, and by airway assembly 2, coolant is imported in compression chamber 331.
Airway assembly 2 includes the inside and outside nested at least two airway 21 arranged, every phase at least two airway 21 Heat-insulation chamber 22 is limited between two adjacent airways 21.It is to say, airway 21 can be two or more such as Three, four etc..For example, referring to Fig. 3-Fig. 9, airway assembly 2 includes inside and outside nested two airways 21 arranged.
Wherein, the airway 21 of the central axis of the most adjacent close airway assembly 2 in two airways 21 is permissible For internal layer airway, the airway 21 away from airway 21 central axis can be outer layer airway, outer layer airway and internal layer Heat-insulation chamber 22 is limited between airway.Thus, it is possible to effectively reduce adjacent two airway 21 (i.e. outer layer airway and Internal layer airway) between conduction of heat, such that it is able to effectively reduce the heating to the gas flowing through airway assembly 2, reduce Suction superheat, and then the refrigerating capacity of compressor 100 can be improved, it is possible to improve efficiency and the efficiency of compressor 100.
Specifically, the minimum thickness of heat-insulation chamber 22 is that C, C meet: C >=0.2mm, its concrete numerical value can be according to actual need Seeking adjusted design, such as, the thickness C of heat-insulation chamber 22 can meet further: 1mm≤C≤2mm etc..Thus, it is possible to improve heat insulation The effect of heat insulation in chamber 22 and reliability.Additionally, also significantly reduce the difficulty of processing of airway assembly 2, improve airway The production efficiency of assembly 2, thus reduce the processing cost of compressor 100.Wherein, on the axial direction of airway assembly 2, The thickness of heat-insulation chamber 22 can keep consistent, can be inconsistent.
Compressor 100 according to embodiments of the present invention, by arranging inside and outside nested setting at least in airway assembly 2 Two airways 21, limit heat-insulation chamber 22 between two the most adjacent airways, and make the thickness C of heat-insulation chamber 22 full Foot: C >=0.2mm, thus, is effectively improved effect of heat insulation and the reliability of heat-insulation chamber 22, reduces adjacent two inducing QI Conduction of heat between pipe 21, thus efficiently reduce the heating to the gas flowing through airway assembly 2, reduce suction superheat Degree, and then improve the refrigerating capacity of compressor 100, and improve efficiency and the efficiency of compressor 100.Additionally, the most effectively drop The low difficulty of processing of airway assembly 2, improves the production efficiency of airway assembly 2, thus reduces adding of compressor 100 Work cost.
According to some embodiments of the present invention, at least one end of at least two airway 21 is tightly connected.It is to say, it is every Wherein one end (such as, the left end in Fig. 3 or right-hand member) of two adjacent airways 21 seals and is connected, or the most adjacent two lead The two ends (such as, the left end in Fig. 3 and right-hand member) of trachea 21 all seal and are connected.Such as, in the example of fig. 3, airway 21 is Two, the two ends of two airways 21 are all tightly connected.Thus, it is possible to improve the effect of heat insulation of airway assembly 2 further, from And further increasing efficiency and the efficiency of compressor 100.
Wherein, above-mentioned at least one end of two adjacent airways 21 can be sealed by ring surface contact, but is not limited to This.For example, referring to Fig. 3, the outer peripheral face of above-mentioned at least one end of internal layer airway can be formed generally as cylinder or truncated cone-shaped Deng, the outer peripheral face of above-mentioned at least one end of outer layer airway can be formed as the shape that the outer peripheral face with internal layer airway is adaptive. Thus, it is simple to internal layer airway seals with above-mentioned at least one end of outer layer airway and coordinates, thus further increasing heat insulation The effect of heat insulation in chamber 22.
Alternatively, above-mentioned at least one end welding of at least two airway 21, bonding or interference fit, but it is not limited to this. Such as, above-mentioned at least one end of two the most adjacent airways 21 can be formed by the way of welding, bonding or interference fit For sealing structure.Technique is simple, easy to process, and reliability is high.
According to some specific embodiments of the present invention, when above-mentioned at least one end of at least two airway 21 is connected by welding When connecing, above-mentioned at least one end of at least two airway 21 can pass through Laser Welding, soldering, electric resistance welding, arc welding, friction welding (FW) or Electron beam is welded to connect, but is not limited to this.Technique is simple, it is easy to processing.
According to some embodiments of the present invention, the fit clearance of above-mentioned at least one end of two the most adjacent airways 21 is A, fit clearance A can meet :-0.4mm≤A≤0.4mm.Wherein, A can meet further :-0.4mm≤A < 0mm, 0mm ≤A≤0.4mm.Thus, it is possible to improve the reliability of airway assembly 2.
Here, it should be noted that when fit clearance is negative value, above-mentioned at least one end of two adjacent airways 21 Can be interference fit, when fit clearance be on the occasion of time, above-mentioned at least one end of two adjacent airways 21 can be gap Coordinate.
According to some embodiments of the present invention, the length of fit of above-mentioned at least one end of at least two airway 21 is B, joins Close length B to meet: 0.5mm≤B≤5mm.Its concrete numerical value can be according to airway assembly 2 and the concrete specification of compressor 100 Model adjusted design, such as, length of fit L can meet further: B=3mm, B=5mm etc..Thus, improve airway group The reliability of part 2, and improve the sealing of heat-insulation chamber 22, thus improve the effect of heat insulation of heat-insulation chamber 22.
According to some embodiments of the present invention, in the most adjacent two airway 21 at least two airway 21 outside The wall thickness of layer airway is that t1, t1 meet: 0.3mm≤t1≤3mm.Its concrete numerical value can be according to airway assembly 2 and compression The concrete specifications and models adjusted design of machine 100, such as, the wall thickness t1 of outer layer airway can meet further: t1=1mm etc.. Thus, it is effectively improved the structural strength of outer layer airway, thus improves the overall construction intensity of airway assembly 2, and Simple in construction, it is easy to processing and manufacturing.
According to some embodiments of the present invention, interior in the most adjacent two airway 21 at least two airway 21 The wall thickness of layer airway is that t2, t2 meet: 0.3mm≤t2≤3mm.Its concrete numerical value can be according to airway assembly 2 and compression The concrete specifications and models adjusted design of machine 100, such as, the wall thickness t2 of internal layer airway can meet further: t2=0.8mm, T2=1mm etc..Thus, it is effectively improved the structural strength of internal layer airway, thus further increasing airway assembly 2 Overall construction intensity, and simple in construction, it is easy to processing and manufacturing.
According to some embodiments of the present invention, heat-insulation chamber 22 is vacuum cavity.Thus, further increasing heat-insulation chamber 22 Effect of heat insulation.
According to other embodiments of the present invention, compressor 100 may further include thermal insulation barriers, thermal insulation barriers be filled in every In hot chamber 22.Wherein, thermal insulation barriers can be air or the less heat-barrier material of other heat conductivitys.Specifically, the leading of thermal insulation barriers Hot coefficient is less than the heat conductivity of airway 21.Thus, equally improve the effect of heat insulation of heat-insulation chamber 22, reduce airway group The suction superheat of the gas in part 2, and reduce the difficulty of processing of airway assembly 2, reduce processing cost.
According to some embodiments of the present invention, suction nozzle 6 can form as one structure or split knot with airway assembly 2 Structure.
Wherein, when suction nozzle 6 is formed as Split type structure with airway assembly 2, the above-mentioned other end of suction nozzle 6 can be stretched Connect with airway assembly 2 in entering the innermost layer airway of airway assembly 2.Now, suction nozzle 6 can be with innermost layer airway Welding, bonding or interference fit, so that suction nozzle 6 is tightly connected with airway assembly 2.Simple in construction, easy to assembly.
When suction nozzle 6 forms as one structure with airway assembly 2, with reference to Figure 10 and Figure 11, suction nozzle 6 can with lead One of them airway 21 in trachea assembly 2 is one-body molded.Such as, in the example of Figure 10, suction nozzle 6 and internal layer airway One-body molded, and for example, in the example of fig. 11, suction nozzle 6 is one-body molded with outer layer airway.Thus, simplify further The processing technique of airway assembly 2, and simplify assembly technology and improve reliability.
According to some embodiments of the present invention, the most adjacent at least one end of at least one in two airways 21 has Stage portion 23, stage portion 23 along corresponding airway 21 be axially facing its at least end, one end direction, to two airways Another direction in 21 extends so that limiting heat-insulation chamber 22 between two airways 21.
Specifically, the most adjacent wherein one end of one of them in two airways 21 can have stage portion 23, Or the two ends of one of them in two the most adjacent airways 21 are respectively provided with stage portion 23, or two the most adjacent airways 21 In wherein one end of each airway 21 can have each in stage portion 23, or two the most adjacent airways 21 The two ends of airway 21 are respectively provided with stage portion 23.Thus, it is simple between two adjacent airways 21, limit heat-insulation chamber 22, Improve efficiency and the efficiency of compressor 100, and be easy to above-mentioned at least one end of two airways 21 adjacent in airway assembly 2 Form ring surface contact to seal, consequently facilitating the assembling of airway assembly 2.
Such as, in the example of Fig. 3 and Fig. 4, the left end of outer layer airway and the right-hand member of internal layer airway are respectively equipped with one Individual stage portion 23, wherein, the stage portion 23 of the left end of outer layer airway along outer layer airway the direction being axially facing its left end, Inner layer airway tilts to extend, and the stage portion 23 of internal layer airway right-hand member is along the side being axially facing its right-hand member of internal layer airway Tilt to extend to, outer layers airway.
And for example, in the example of hgure 5, the left end of internal layer airway and right-hand member are respectively equipped with a stage portion 23, and outer layer is led Trachea is formed as straight tube.Wherein, the stage portion 23 of internal layer airway left end is along the side being axially facing its left end of internal layer airway Tilting to extend to, outer layers airway, the stage portion 23 of internal layer airway right-hand member is axially facing its right-hand member along internal layer airway Direction, outer layers airway tilt extend.
According to other embodiments of the present invention, the most adjacent at least one end of at least one in two airways 21 End have towards in two airways 21 another bending and with another bending part being connected in two airways 21 24.Specifically, the end of the most adjacent wherein one end of one of them in two airways 21 can have bending part 24, Or the end, two ends of one of them in two the most adjacent airways 21 is respectively provided with bending part 24, or two the most adjacent inducing QIs The end of wherein one end of each airway 21 in pipe 21 can have bending part 24, or two the most adjacent airways 21 In the end, two ends of each airway 21 be respectively provided with bending part 24.Thus, lead at adjacent two the most easily Limit heat-insulation chamber 22 between trachea 21, improve efficiency and the efficiency of compressor 100, and be easy in airway assembly 2 adjacent Above-mentioned at least one end of two airways 21 forms ring surface contact and seals, consequently facilitating the assembling of airway assembly 2.
Such as, in the example of Fig. 6 and Fig. 7, the end at the two ends of internal layer airway is equipped with bending part 24, wherein, interior Layer airway left end end is respectively facing the bending of outer layer airway and is connected with outer layer airway with the bending part 24 of right-hand member end. Thus, it is possible to limit heat-insulation chamber 22 by bending part 24 between two adjacent airways 21, and bending part can be passed through Form ring surface contact between 24 above-mentioned at least one end making adjacent two airway 21 and seal structure, simple in construction, add Work is convenient.
Alternatively, bending part 24 can be spaced apart from each other with corresponding airway 21 end or fit, but is not limited to this.Also That is, the inner surface of bending part 24 can be spaced apart from each other with the outer surface of the end of corresponding airway 21 or fit.Example As, in the example of fig. 6, the bending part 24 of internal layer airway left end and right-hand member is all fitted with the end of corresponding airway 21, It is to say, the outer surface laminating of the left end end of the inner surface of the bending part 24 of internal layer airway left end and internal layer airway, The outer surface laminating of the inner surface of the bending part 24 of internal layer airway right-hand member and internal layer airway right-hand member end.Simple in construction, adds Work is convenient.
And for example, in the example in figure 7, the left end end of the bending part 24 of internal layer airway left end and internal layer airway is each other Spaced apart, the bending part 24 of internal layer airway right-hand member is fitted each other with the right-hand member end of internal layer airway.
Set it is understood that the concrete structure of bending part 24 can adjust according to the concrete specifications and models of compressor 100 Meter, this is not especially limited by the present invention.
According to the still other embodiments of the present invention, the most adjacent at least one end of at least one in two airways 21 sets Have towards in two airways 21 another protrude and with another connection bump being connected 25 in two airways 21.
Specifically, the most adjacent wherein one end of one of them in two airways 21 can be provided with connection bump The two ends of one of them in 25, or two the most adjacent airways 21 are equipped with connection bump 25, or the most adjacent two lead Wherein one end of each airway 21 in trachea 21 can be provided with in connection bump 25, or two the most adjacent airways 21 The two ends of each airway 21 be respectively provided with connection bump 25.Alternatively, the free end of connection bump 25 can be formed as arc Shape face such as arc surface, but it is not limited to this.Thus, it is possible to limited between two adjacent airways 21 by connection bump 25 Go out heat-insulation chamber 22, improve efficiency and the efficiency of compressor 100, it is possible to make adjacent two airway by connection bump 25 Formation ring surface contact sealing structure between 21, simple in construction, easy to process.
Such as, in the example of fig. 8, the left end of outer layer airway be provided with internal layer airway protrude and with internal layer inducing QI The connection bump 25 that pipe is connected, the right-hand member of internal layer airway is provided with the bending of outer layer airway and is connected with outer layer airway Bending part 24, simple in construction, easy to process.
According to some embodiments of the present invention, the most adjacent at least one end of at least one in two airways 21 is provided with The flanging 26 extended towards another in two airways 21, another the corresponding end in flanging 26 and two airways 21 End face connects.Specifically, the most adjacent wherein one end of one of them in two airways 21 can be provided with flanging 26, or The most adjacent two ends of one of them in two airways 21 are equipped with in flanging 26, or two the most adjacent airways 21 Wherein one end of each airway 21 can be provided with each airway in flanging 26, or two the most adjacent airways 21 The two ends of 21 are respectively provided with flanging 26.Thus, it is simple to above-mentioned at least one end of two adjacent airways 21 is formed and seals structure, from And the effect of heat insulation of heat-insulation chamber 22 can be improved.
Such as, in the example of figure 9, the right-hand member of internal layer airway is provided with flanging 26, and flanging 26 prolongs towards outer layer airway Stretch, and flanging 26 is connected with the right-hand member end face of outer layer airway, simple in construction, easy to process.
It is understood that stage portion 23, bending part 24, connection bump 25 and flanging 26 on airway assembly 2 are permissible Specifications and models combination in any design according to airway assembly 2 and compressor 100, this is not especially limited by the present invention.Optional Ground, airway 21 is made up of at least one in copper, copper alloy, ferrum, ferroalloy and ferrum copper facing.It is to say, airway assembly 2 In multiple airways 21 can be made up of the one of which in copper, copper alloy, ferrum, ferroalloy and ferrum copper facing, it is also possible to by copper, Multiple in copper alloy, ferrum, ferroalloy and ferrum copper facing is made.Wherein, two adjacent airways 21 can use same material Material is made, it would however also be possible to employ two kinds of different materials are made, and this is not construed as limiting by the present invention.
Specifically, can be provided with transition part 27 at least two airway 21 at least one, transition part 27 can be one Individual or multiple.Wherein, transition part 27 can by the tube wall of airway 21 towards compression chamber 331, in the airway assembly 2 The direction of mandrel line tilts to extend.For example, referring to Fig. 3, Fig. 4, Fig. 6, Fig. 8, Fig. 9 and Figure 10, on two adjacent airways 21 It is equipped with transition part 27, and transition part 27 is formed approximately at the middle part of airway assembly 2.And for example, with reference to Fig. 5, Fig. 7 and Figure 11, Internal layer airway in two airways 21 being connected is provided with transition part 27, and outer layer airway is formed as straight tube.Thus, just Coordinate with connecting tube 12 and compression chamber 331 in airway assembly 2.
According to some embodiments of the present invention, compressor 100 can be single cylinder compressor or multicylinder compressor.Wherein, when When compressor 100 is single cylinder compressor, as it is shown in figure 1, cylinder assembly 33 includes a cylinder, now base bearing 31 is located at this gas The upper end of cylinder, supplementary bearing 32 is located at the lower end of this cylinder.When compressor 100 is multicylinder compressor (not shown), air cylinder group Part 33 includes multiple such as two cylinders, can be provided with dividing plate between adjacent two cylinders, and base bearing 31 is located at the gas of the top The upper end of cylinder, supplementary bearing 32 is located at the lower end of the cylinder of bottom.
Compressor 100 according to embodiments of the present invention, efficiently reduces the heat biography between adjacent two airway 21 Lead, thus efficiently reduce the heating to the gas flowing through airway assembly 2, reduce suction superheat, and then improve The refrigerating capacity of compressor 100, and improve efficiency and the efficiency of compressor 100.Additionally, also significantly reduce compressor 100 Difficulty of processing, reduce the processing cost of compressor 100.
In the description of this specification, reference term " embodiment ", " some embodiments ", " illustrative examples ", The description of " example ", " concrete example " or " some examples " etc. means to combine this embodiment or the specific features of example description, knot Structure, material or feature are contained at least one embodiment or the example of the present invention.In this manual, to above-mentioned term Schematic representation is not necessarily referring to identical embodiment or example.And, the specific features of description, structure, material or spy Point can combine in any one or more embodiments or example in an appropriate manner.
Although an embodiment of the present invention has been shown and described, it will be understood by those skilled in the art that: not These embodiments can be carried out multiple change in the case of departing from the principle of the present invention and objective, revise, replace and modification, this The scope of invention is limited by claim and equivalent thereof.

Claims (10)

1. a compressor, it is characterised in that including:
Housing, is provided with compression mechanism in described housing, described compression mechanism has compression chamber;
Airway assembly, one end of described airway assembly through described housing with described compression mechanism be connected and with described compression Intracavity portion connects, and described airway assembly includes the inside and outside nested at least two airway arranged, described at least two airway In limit heat-insulation chamber between the most adjacent two described airways, the minimum thickness of described heat-insulation chamber is C, and described C meets: C ≥0.2mm;
Suction nozzle, described suction nozzle is connected with the other end of described airway assembly.
Compressor the most according to claim 1, it is characterised in that at least one end of described at least two airway seals even Connect.
Compressor the most according to claim 2, it is characterised in that described at least one end weldering of described at least two airway Connect, bonding or interference fit.
4. according to the compressor described in Claims 2 or 3, it is characterised in that described at least the one of described at least two airway The length of fit of end is B, and described B meets: 0.5mm≤B≤5mm.
Compressor the most according to claim 1, it is characterised in that the most adjacent described in described at least two airway The wall thickness of the outer layer airway in two airways is t1, and described t1 meets: 0.3mm≤t1≤3mm.
Compressor the most according to claim 1, it is characterised in that the most adjacent described in described at least two airway The wall thickness of the internal layer airway in two airways is t2, and described t2 meets: 0.3mm≤t2≤3mm.
Compressor the most according to claim 1, it is characterised in that described heat-insulation chamber is vacuum cavity.
Compressor the most according to claim 1, it is characterised in that farther include:
Thermal insulation barriers, described thermal insulation barriers is filled in described heat-insulation chamber.
Compressor the most according to claim 8, it is characterised in that the heat conductivity of described thermal insulation barriers is less than described airway Heat conductivity.
Compressor the most according to claim 1, it is characterised in that described suction nozzle is formed as with described airway assembly Split type structure or integrative-structure.
CN201610605801.XA 2016-07-27 2016-07-27 Compressor Pending CN106122028A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610605801.XA CN106122028A (en) 2016-07-27 2016-07-27 Compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610605801.XA CN106122028A (en) 2016-07-27 2016-07-27 Compressor

Publications (1)

Publication Number Publication Date
CN106122028A true CN106122028A (en) 2016-11-16

Family

ID=57254792

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610605801.XA Pending CN106122028A (en) 2016-07-27 2016-07-27 Compressor

Country Status (1)

Country Link
CN (1) CN106122028A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107420288A (en) * 2017-06-30 2017-12-01 广东美芝制冷设备有限公司 Air-breathing instlated tubular and compressor
CN107489623A (en) * 2017-08-28 2017-12-19 广东美芝制冷设备有限公司 Compressor and refrigeration system
CN112524989A (en) * 2019-09-17 2021-03-19 光和科股份有限公司 Connector for heat exchange system and method of manufacturing the same

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01110890A (en) * 1987-10-21 1989-04-27 Sanyo Electric Co Ltd Rotary compressor
JPH045485A (en) * 1990-04-20 1992-01-09 Hitachi Ltd Rotary compressor
CN1755122A (en) * 2004-09-27 2006-04-05 乐金电子(天津)电器有限公司 Inside structure of rotary compressor liquid-storage tank
CN2797689Y (en) * 2005-06-27 2006-07-19 上海奥申机械有限公司 Liquid storage apparatus for refrigeration compressor
CN201318289Y (en) * 2008-12-16 2009-09-30 珠海格力电器股份有限公司 Dispenser for heat and sound insulation
CN201779032U (en) * 2010-09-15 2011-03-30 广东美芝制冷设备有限公司 Rotary type compressor
JP2012036751A (en) * 2010-08-04 2012-02-23 Panasonic Corp Compressor
CN202833176U (en) * 2012-09-26 2013-03-27 珠海格力电器股份有限公司 Enthalpy increasing pipe of rotary compressor, fixed assembly and compressor
CN203146338U (en) * 2012-02-10 2013-08-21 松下电器产业株式会社 Sealed compressor
CN104595191A (en) * 2015-01-15 2015-05-06 广东美芝制冷设备有限公司 Compressor assembly
CN105221431A (en) * 2015-10-22 2016-01-06 广东美芝制冷设备有限公司 Compressor assembly
CN205858700U (en) * 2016-07-27 2017-01-04 广东美芝制冷设备有限公司 Compressor
CN205858620U (en) * 2016-07-27 2017-01-04 广东美芝制冷设备有限公司 The suction conduit assembly of compressor, compressor and refrigeration system
CN205858703U (en) * 2016-07-27 2017-01-04 广东美芝制冷设备有限公司 Compressor

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01110890A (en) * 1987-10-21 1989-04-27 Sanyo Electric Co Ltd Rotary compressor
JPH045485A (en) * 1990-04-20 1992-01-09 Hitachi Ltd Rotary compressor
CN1755122A (en) * 2004-09-27 2006-04-05 乐金电子(天津)电器有限公司 Inside structure of rotary compressor liquid-storage tank
CN2797689Y (en) * 2005-06-27 2006-07-19 上海奥申机械有限公司 Liquid storage apparatus for refrigeration compressor
CN201318289Y (en) * 2008-12-16 2009-09-30 珠海格力电器股份有限公司 Dispenser for heat and sound insulation
JP2012036751A (en) * 2010-08-04 2012-02-23 Panasonic Corp Compressor
CN201779032U (en) * 2010-09-15 2011-03-30 广东美芝制冷设备有限公司 Rotary type compressor
CN203146338U (en) * 2012-02-10 2013-08-21 松下电器产业株式会社 Sealed compressor
CN202833176U (en) * 2012-09-26 2013-03-27 珠海格力电器股份有限公司 Enthalpy increasing pipe of rotary compressor, fixed assembly and compressor
CN104595191A (en) * 2015-01-15 2015-05-06 广东美芝制冷设备有限公司 Compressor assembly
CN105221431A (en) * 2015-10-22 2016-01-06 广东美芝制冷设备有限公司 Compressor assembly
CN205858700U (en) * 2016-07-27 2017-01-04 广东美芝制冷设备有限公司 Compressor
CN205858620U (en) * 2016-07-27 2017-01-04 广东美芝制冷设备有限公司 The suction conduit assembly of compressor, compressor and refrigeration system
CN205858703U (en) * 2016-07-27 2017-01-04 广东美芝制冷设备有限公司 Compressor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107420288A (en) * 2017-06-30 2017-12-01 广东美芝制冷设备有限公司 Air-breathing instlated tubular and compressor
CN107420288B (en) * 2017-06-30 2020-07-31 广东美芝制冷设备有限公司 Air suction heat insulation pipe and compressor
CN107489623A (en) * 2017-08-28 2017-12-19 广东美芝制冷设备有限公司 Compressor and refrigeration system
CN112524989A (en) * 2019-09-17 2021-03-19 光和科股份有限公司 Connector for heat exchange system and method of manufacturing the same

Similar Documents

Publication Publication Date Title
CN205858703U (en) Compressor
CN106122028A (en) Compressor
US10048010B2 (en) Heat exchanger and method for manufacturing same
CN105387735A (en) Heat exchanger
CN106224243A (en) Compressor
CN205858700U (en) Compressor
CN104595191B (en) Compressor assembly
CN104819130B (en) Compressor
CN204373481U (en) Heat pipe and electronic equipment
CN205858621U (en) Compressor
CN205858619U (en) Compressor
CN105221394B (en) Compressor assembly and there is its refrigeration system
JP2011064142A (en) Water jacket structure
CN105805016A (en) Rotary compressor
CN205858620U (en) The suction conduit assembly of compressor, compressor and refrigeration system
CN206707977U (en) Compressor and there is its refrigeration plant
CN209041123U (en) Compressor assembly and refrigeration equipment
CN206707961U (en) Compressor and there is its refrigeration plant
CN206707978U (en) Compressor and there is its refrigeration plant
CN106884777A (en) Compressor and the refrigeration plant with it
CN207777129U (en) Compressor and refrigeration equipment
CN206429425U (en) Compressor
CN204627932U (en) Compressor
CN207122392U (en) Compressor and refrigeration plant
CN207064189U (en) Air-breathing instlated tubular and compressor

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20161116