CN103206399B - Centrifugal compressor and refrigeration equipment comprising same - Google Patents
Centrifugal compressor and refrigeration equipment comprising same Download PDFInfo
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- CN103206399B CN103206399B CN201210016935.XA CN201210016935A CN103206399B CN 103206399 B CN103206399 B CN 103206399B CN 201210016935 A CN201210016935 A CN 201210016935A CN 103206399 B CN103206399 B CN 103206399B
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- 238000005057 refrigeration Methods 0.000 title abstract 2
- 239000000446 fuel Substances 0.000 claims description 37
- 230000007423 decrease Effects 0.000 claims description 3
- 239000000314 lubricant Substances 0.000 description 28
- 238000005461 lubrication Methods 0.000 description 15
- 238000010586 diagram Methods 0.000 description 9
- 230000000694 effects Effects 0.000 description 7
- 238000000034 method Methods 0.000 description 5
- 230000009471 action Effects 0.000 description 3
- 238000001816 cooling Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000009825 accumulation Methods 0.000 description 2
- 230000001771 impaired effect Effects 0.000 description 2
- 230000013011 mating Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 238000012384 transportation and delivery Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 238000004378 air conditioning Methods 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000004069 differentiation Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 230000003094 perturbing effect Effects 0.000 description 1
- 238000004804 winding Methods 0.000 description 1
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Abstract
The invention provides a centrifugal compressor and refrigeration equipment comprising the same. This centrifugal compressor includes rotor (30) and the bearing assembly of cover on rotor (30), rotor (30) include with the axial bearing surface complex axial thrust face of bearing assembly, the bearing assembly includes front bearing (10) and rear bearing (20), the first end of rear bearing (20) is provided with thrust disc (33) outward, thrust disc (33) fixed connection is on rotor (30), the axial thrust face includes rotor thrust face (34) and thrust disc thrust face (35), front bearing (10) set up between two rotor thrust faces (34), the axial bearing surface and the thrust disc thrust face (35) cooperation of rear bearing (20). According to the centrifugal compressor, the bearing bush damage caused by overlarge load applied to the axial thrust surface of a single bearing can be avoided, the load borne by the bearing is in a safe range, and the use safety of the bearing is improved.
Description
Technical field
The present invention relates to filed of air conditioning, in particular to a kind of centrifugal compressor and the chiller plant comprising this centrifugal compressor.
Background technique
In direct connection frequency conversion centrifugal compressor, owing to cancelling gear up structure, all axial forces, radial force act on two bearings before and after motor entirely, and it is much bigger relative to being with the bearing load of gear up structure that load bears in bearing institute.
Conventional centrifugal compressor generally adopts single bearing shaft to carry out spacing to thrust face to the front and back bearings of sliding bearing respectively, makes bearing bear unidirectional thrust, meets the design needs of centrifugal compressor.The bearing shell of fore bearing is generally fixedly installed to thrust face and bearing shell fixed block by one-way shaft, realizes the combination between bearing shell and the rotor of centrifugal compressor.This structure generally can meet usage requirement, but the bearing shell due to fore bearing only bears the thrust of epitrochanterian single bearing shaft to thrust face, therefore, fore bearing bearing shell unbalance stress can be caused, and bearing shell can be excessive and outside the field of load exceeding bearing, cause damage to fore bearing to the thrust of thrust face due to born bearing shaft.
Summary of the invention
The present invention aims to provide a kind of centrifugal compressor and comprises the chiller plant of this centrifugal compressor, single bearing shaft can be avoided excessive and cause bearing shell to damage to thrust face imposed load, make load suffered by bearing in safety range, improve the Security that bearing uses.
To achieve these goals, according to an aspect of the present invention, provide a kind of centrifugal compressor, comprise rotor and be set in epitrochanterian bearing unit, rotor comprises the end thrust face coordinated with the axial load-carrying surface of bearing unit, bearing unit comprises fore bearing and rear bearing, the first end of rear bearing is outside equipped with thrust disc, thrust disc is fixedly connected on rotor, end thrust face comprises rotor thrust face and thrust disc thrust face, fore bearing is arranged between two rotor thrust faces, and the axial load-carrying surface of rear bearing coordinates with thrust disc thrust face.
Further, fore bearing comprises fore bearing bearing shell and fore bearing bearing shell locating piece, the periphery wall of fore bearing bearing shell is provided with fore bearing fuel feeding distributing chute in parallel, fore bearing bearing shell also comprises the radial oil supply gallery of fore bearing and is separately positioned on fore bearing first side direction oil supply gallery and the fore bearing second side direction oil supply gallery of the radial oil supply gallery both sides of fore bearing, the radial oil supply gallery of fore bearing radially runs through fore bearing bearing shell from fore bearing fuel feeding distributing chute in parallel, fore bearing first side direction oil supply gallery extends to the first end end face of fore bearing bearing shell from fore bearing fuel feeding distributing chute in parallel, fore bearing second side direction oil supply gallery extends to the second end end face of fore bearing bearing shell from fore bearing fuel feeding distributing chute in parallel.
Further, fore bearing bearing shell also comprise the exit position being arranged on the radial oil supply gallery of fore bearing fore bearing circumference oil supply and along the axial oil supply of the axially extended fore bearing in fore bearing circumference oil supply two ends, the axial oil supply of fore bearing and rotor engagement, the axial oil supply two ends of fore bearing are provided with first and cross oil groove, rotor also comprises circumference arrange and with first cross that oil groove coordinates divide oil groove.
Further, rear bearing comprises rear bearing bearing shell and rear bearing bearing shell locating piece, the inner circle wall of rear bearing bearing shell locating piece is provided with rear bearing fuel feeding distributing chute in parallel, rear bearing bearing shell comprises the radial oil supply gallery of rear bearing and rear bearing side direction oil supply gallery, rear bearing side direction oil supply gallery is communicated with rear bearing fuel feeding distributing chute in parallel, along the axial direction horizontal-extending of rear bearing bearing shell, and be communicated to thrust disc thrust face stores oil groove.
At least one end thrust face is provided with and stores oil groove, store oil groove and be connected with the oil supply gallery in the axial load-carrying surface of bearing unit, the bottom storing oil groove is indent arc.
Further, the outward edge storing oil groove is provided with the oil unloading trough from storing oil groove and extend to end thrust face outer periphery.
Further, oil unloading trough is V-type groove or U-type groove.
Further, store oil groove to successively decrease along the radial extension direction degree of depth of rotor.
Further, storing oil groove has multiple, and the circumferential direction along rotor on end thrust face is uniformly distributed.
According to a further aspect in the invention, provide a kind of chiller plant, comprise centrifugal compressor, this centrifugal compressor is above-mentioned centrifugal compressor.
Apply technological scheme of the present invention, centrifugal compressor comprises rotor and is set in epitrochanterian bearing unit, rotor comprises the end thrust face coordinated with the axial load-carrying surface of bearing unit, bearing unit comprises fore bearing and rear bearing, the first end of rear bearing is outside equipped with thrust disc, and thrust disc is fixedly connected on rotor, and end thrust face comprises rotor thrust face and thrust disc thrust face, fore bearing is arranged between two rotor thrust faces, and the axial load-carrying surface of rear bearing coordinates with thrust disc thrust face.By arranging two rotor thrust faces to rotor, make two end thrust faces of rotor all form end thrust effect to fore bearing, thus make fore bearing two ends stress balance.Because fore bearing two ends are stressed; therefore avoid the fore bearing bearing shell problem that only stressed the caused shaft strength in one end is excessive and impaired, the stressed of fore bearing can be remained in safety range, available protecting is formed to bearing; improve the reliability of compressor operating, improve the Security of bearing.
Accompanying drawing explanation
The accompanying drawing forming a part of the present invention is used to provide a further understanding of the present invention, and schematic description and description of the present invention, for explaining the present invention, does not form inappropriate limitation of the present invention.In the accompanying drawings:
Fig. 1 shows the oil supply structure schematic diagram of the motor fore bearing of centrifugal compressor according to an embodiment of the invention;
Fig. 2 shows the structure for amplifying schematic diagram at the L place of the motor fore bearing of the centrifugal compressor according to Fig. 1;
The oil supply structure schematic diagram that the electric motor back shaft that Fig. 3 shows centrifugal compressor according to an embodiment of the invention holds;
Fig. 4 shows the structure for amplifying schematic diagram at the M place of holding according to the electric motor back shaft of the centrifugal compressor of Fig. 3;
Fig. 5 shows the sectional structure schematic diagram of the fore bearing bearing shell of the motor fore bearing of centrifugal compressor according to an embodiment of the invention;
Fig. 6 shows the perspective view of the fore bearing bearing shell of the motor fore bearing of centrifugal compressor according to an embodiment of the invention;
The sectional structure schematic diagram of the rear bearing bearing shell that the electric motor back shaft that Fig. 7 shows centrifugal compressor according to an embodiment of the invention holds;
The perspective view of the rear bearing bearing shell that the electric motor back shaft that Fig. 8 shows centrifugal compressor according to an embodiment of the invention holds;
Fig. 9 shows the structural representation in the rotor thrust face of centrifugal compressor according to an embodiment of the invention;
The G-G that Figure 10 shows the rotor thrust face of the centrifugal compressor according to Fig. 9 to sectional structure schematic diagram;
The H-H that Figure 11 shows the rotor thrust face of the centrifugal compressor according to Fig. 9 to sectional structure schematic diagram;
The I-I that Figure 12 shows the rotor thrust face of the centrifugal compressor according to Fig. 9 to sectional structure schematic diagram;
Figure 13 shows the structural representation of the thrust disc thrust face of centrifugal compressor according to an embodiment of the invention; And
The K-K that Figure 14 shows the thrust disc thrust face of the centrifugal compressor according to Figure 13 to broken section structural representation.
Embodiment
Hereinafter also describe the present invention in detail with reference to accompanying drawing in conjunction with the embodiments.It should be noted that, when not conflicting, the embodiment in the application and the feature in embodiment can combine mutually.
As shown in Figures 1 to 4, according to embodiments of the invention, centrifugal compressor comprises rotor 30 and bearing unit, and bearing unit is set on rotor 30.Bearing unit had both comprised radial load-carrying surface, also comprised axial load-carrying surface, and like this, this bearing unit plays compound action, can bear the radial load of rotor 30, also can bear axial load, and compact structure.Rotor 30 comprises the end thrust face of matching with the axial load-carrying surface of bearing unit, at least one end thrust face of rotor 30 is provided with and stores oil groove 31, store oil groove 31 to be connected with the oil supply gallery in the axial load-carrying surface of bearing unit, in the process of bearing unit work, accumulate lubricant oil.
When centrifugal compressor meets accident and stops operating; the lubricant oil be accumulated in oil groove 31 can discharge; participate in the lubrication between bearing unit and rotor 30; thus protection is formed to the bearing shell of bearing unit; thus can prevent because shortage lubrication causes bearing bush temperature too high and cause tile kilning phenomenon, improving the reliability of compressor operating.
Bearing unit comprises motor fore bearing 10 (hereinafter referred to as fore bearing) and electric motor back shaft holds 20 (hereinafter referred to as rear bearings), and the first end of rear bearing 20 is outside equipped with thrust disc 33, and thrust disc 33 is bolted and is arranged on rotor 30.End thrust face comprises the rotor thrust face 34 coordinated with fore bearing 10 and the thrust disc thrust face 35 coordinated with rear bearing, and fore bearing 10 is arranged between two rotor thrust faces 34 of rotor 30.
Incorporated by reference to see shown in Fig. 5 and Fig. 6, fore bearing 10 is processed as split type structure, and with pin location after being assemblied in rotor 30, the cylindricity keeping two-part bearing to coordinate, is then tightened by bolts.The fore bearing bearing shell locating piece 12 that fore bearing 10 comprises fore bearing bearing shell 11 and is set in outside fore bearing bearing shell 11, fore bearing bearing shell locating piece 12 is fixedly installed, and forms positioning action to fore bearing bearing shell 11.When fore bearing bearing shell 11 is installed, fore bearing 10 is set on rotor 30, make fore bearing 10 and rotor 30 be assembled into assembly, the assembly then fore bearing bearing shell 11 and rotor 30 are assembled into is installed by bearing assemble face and is positioned in fore bearing bearing shell locating piece 12.Fore bearing bearing shell locating piece 12 and fore bearing bearing shell 11 closely cooperate, and prevent fore bearing bearing shell 11 from following rotor journal and rotate together.Bearing assemble face is provided with seal groove, Sealing is provided with in seal groove, the seal makes to form sealing between fore bearing bearing shell 11 and fore bearing bearing shell locating piece 12, prevents lubricant oil from leaking along the matching gap of fore bearing bearing shell 11 and fore bearing bearing shell locating piece 12.After fixing fore bearing bearing shell 11, relative position between rotor 30 and fore bearing bearing shell locating piece 12, with bolt, the fore bearing bearing shell 11 of fore bearing 10 and fore bearing bearing shell locating piece 12 are locked.
Fore bearing bearing shell locating piece 12 comprises the main oil supply gallery 121 of fore bearing arranged along fore bearing radial direction, the first end of the main oil supply gallery 121 of fore bearing is communicated to bearing shell, second end of the main oil supply gallery 121 of fore bearing is communicated to oil sources, thus lubricant oil is introduced participation lubrication and cooling in fore bearing 10.
Fore bearing bearing shell 11 comprises and being arranged on the bearing assemble face of fore bearing bearing shell 11, and the fuel feeding distributing chute 111 in parallel be connected mutually with the main oil supply gallery of fore bearing 121 on fore bearing bearing shell locating piece 12.Fuel feeding distributing chute 111 in parallel along the circumferential direction winding in the bearing assemble face (i.e. the external cylindrical surface coordinated with fore bearing bearing shell locating piece 12 of fore bearing bearing shell 11) of fore bearing bearing shell 11 on the outer wall of fore bearing bearing shell 11.
Fore bearing bearing shell 11 also comprises the radial oil supply gallery 112 of the fore bearing be connected with fuel feeding distributing chute 111 in parallel and fore bearing side direction oil supply gallery.The radial oil supply gallery 112 of fore bearing is positioned at the medium position of the axial direction of fore bearing bearing shell 10, and the radial direction along fore bearing bearing shell 11 runs through fore bearing bearing shell 11.The exit position of the radial oil supply gallery 112 of fore bearing is provided with fore bearing circumference oil supply 115.Fore bearing circumference oil supply 115 arranges along the inwall circumference of fore bearing bearing shell 11 oil supply forming annular.The first end end inwall of fore bearing bearing shell 11 including bearing bush 11 in the past is in axial direction through to the axial oil supply 116 of fore bearing of the second end end of fore bearing bearing shell 11, the axial oil supply 116 of fore bearing runs through fore bearing circumference oil supply 115, after lubricant oil enters fore bearing circumference oil supply 115, the mating part of rotor 30 and fore bearing bearing shell 11 is entered by the axial oil supply 116 of fore bearing, and dynamic pressure oil film is formed between rotor 30 and fore bearing bearing shell 11, rotor 30 is avoided to contact with the direct of fore bearing bearing shell 11, available protecting is formed to fore bearing bearing shell 11.
Fore bearing side direction oil supply gallery comprises fore bearing first side direction oil supply gallery 113 and fore bearing second side direction oil supply gallery 114.Fore bearing first side direction oil supply gallery 113 and fore bearing second side direction oil supply gallery 114 are separately positioned on the both sides of the radial oil supply gallery 112 of fore bearing, are arranged in parallel with the radial oil supply gallery 112 of fore bearing.Fore bearing first side direction oil supply gallery 113 and fore bearing second side direction oil supply gallery 114 are from fuel feeding distributing chute 111s in parallel, fore bearing first side direction oil supply gallery 113 is obliquely extended to the first end end of fore bearing bearing shell 11, and fore bearing second side direction oil supply gallery 114 is obliquely extended to the second end end of fore bearing bearing shell 11.
In the middle of the present embodiment, in the first end end of fore bearing bearing shell 11, oil supply 116 axial with fore bearing is connected fore bearing first side direction oil supply gallery 113, and in the second end end of fore bearing bearing shell 11, oil supply 116 axial with fore bearing is connected fore bearing second side direction oil supply gallery 114.At fore bearing first side direction oil supply gallery 113 and the fore bearing second side direction oil supply gallery 114 end cohesive position with fore bearing bearing shell 11, all the axial direction of the inwall of fore bearing bearing shell 11 is provided with first and crosses oil groove 117, rotor 30 includes circumference arrange and with first cross that oil groove 117 coordinates divide oil groove 36.
For motor fore bearing 10, because there is load-carrying surface both sides, therefore, fore bearing 10 is processed the oil supply gallery in three directions, and oil supply gallery is all come together in fore bearing fuel feeding distributing chute 111 in parallel.Consider rotor 30 operationally, the bearing load in fore bearing 10 3 directions is different, therefore, need be optimized design to the oil supply gallery in three directions, arranges many group oil supply galleries so that mean allocation fuel feeding oil mass.More even in order to make radial direction or axial fuel feeding distribute, as: for radial direction, can at the fore bearing circumferentially multiple radial oil supply hole of mean allocation, quantity is 1 ~ 6 (being also the quantity of the oil supply gallery in parallel on each end thrust face).Correspondingly, for the axial direction of fore bearing bearing shell 10, also carry out processing corresponding axial oil supply gallery.Specifically with regard to arranging the fore bearing of single group oil supply gallery, the flow area that need meet the radial oil supply gallery 112 of fore bearing first side direction oil supply gallery 113, fore bearing second side direction oil supply gallery 114 and fore bearing is less than or equal to the flow area of fuel feeding distributing chute 111 in parallel with fore bearing.For singly organizing oil supply gallery, its physical dimension feature is as follows: auxiliary side shaft is to thrust face oil supply hole d1: φ 1.5 ~ φ 3.5mm, master end thrust face oil supply hole d2: φ 4.5 ~ φ 7.5mm, radial bearing surface oil supply hole d3: φ 4.5 ~ φ 7.5mm, fuel feeding distributing chute width w1:10 ~ 15mm, fuel feeding distributing chute height h1:4 ~ 8mm in parallel in parallel.Organize oil supply gallery if arranged more, consistent with the fuel delivery only arranged in single group oil supply gallery situation for ensureing to arrange many group oil supply gallery fuel deliveries, should ensure that the multiple radial oil supply gallery flow area sum arranged is equal with the flow area of the radial oil supply gallery only arranged when singly organizing oil supply gallery, and the setting of side direction oil supply gallery is also like this, when single group oil supply gallery is even only set, radial oil supply gallery, first side direction oil supply gallery, the circulation area of the second side direction oil supply gallery is A respectively, B, C, often organizing circulation area corresponding to oil supply gallery time when being provided with N group oil supply gallery is a respectively, b, c, the following equation of demand fulfillment:
A+B+C=N (a+b+c), and A=Na, B=Nb, C=Nc
For the view shown in Fig. 1, the bearing produced due to impeller High Rotation Speed left, therefore the main shaft of fore bearing to thrust face on right side, simultaneously in order to prevent impeller from reversing and reduce perturbing of rotor cantilever segment, left side also arranges end thrust face, and therefore whole fore bearing has concentrated main shaft to thrust face and two kinds, auxiliary end thrust face form.Because two axial thrust face stressing conditions are different, required oil mass is also different, and therefore, fuel feeding aperture is different.Right side is that main shaft is to thrust face, therefore, the sectional area of the fore bearing second side direction oil supply gallery 114 extended to the right along the axial direction of fore bearing bearing shell 11 is greater than the sectional area of the fore bearing first side direction oil supply gallery 113 that the axial direction along fore bearing bearing shell 11 extends to the left, to enable more lubricant oil enter right-hand axis participate in lubrication and cooling to thrust face, obviously, the structure of this differentiation setting is more reasonable.
Incorporated by reference to shown in Figure 2, the fore bearing first side direction oil supply gallery 113 being positioned at left side in this figure is made up of two-part that aperture is different, comprise dispensing section 118 that oil supply gallery 112 radial with fore bearing be connected and be connected with dispensing section 118 and extend to the extending section 119 of the first end end of fore bearing bearing shell 11, the sectional area of extending section 119 is greater than the sectional area of dispensing section 118.Setting like this is to change fuel feeding flow velocity, to make the flow velocity of lubricant oil in fore bearing first side direction oil supply gallery 113 mate with the stressed of rotor thrust face 34.
Two rotor thrust faces 34 are provided with and store oil groove 31, this stores oil groove 31 and is connected with the first mistake oil groove 117 on fore bearing bearing shell 11, and in the process of rotor turns, the lubricant oil in the first mistake oil groove 117 is under the effect of rotor centrifugal force, enter and store in oil groove 31, and accumulation is got up.First mistake oil groove 117 is arranged along the circumferential direction of fore bearing bearing shell 11, lubricant oil enters first and crosses after in oil groove 117, oil groove 117 circumference can be crossed along first to be uniformly distributed, thus evenly flowed between each end thrust face and the axial load-carrying surface of fore bearing by the first mistake oil groove 117, form good lubrication effect.
In the middle of other embodiment, fore bearing first side direction oil supply gallery 113 and fore bearing second side direction oil supply gallery 114 also can the middle part of the in the past radial oil supply gallery 112 of fore bearing of bearing bush 11 along the axial direction horizontal-extending of fore bearing bearing shell 11, and the sectional area of fore bearing second side direction oil supply gallery 114 is greater than the sectional area of fore bearing first side direction oil supply gallery 113.The main oil supply gallery 121 of fore bearing in lubricant oil the past bearing bush locating piece 12 flows into, enter in the radial oil supply gallery 112 of fore bearing, and be divided into three strands, one flows to the first end end face of fore bearing bearing shell 11, participates in the lubrication between the first end end face of fore bearing bearing shell 11 and rotor thrust face 34; One flows to the second end end face of fore bearing bearing shell 11, participates in the lubrication between the second end end face of fore bearing bearing shell 11 and rotor thrust face 34; One flows to the fore bearing circumference oil supply 115 of fore bearing bearing shell 11, participates in the lubrication between rotor 30 and the inwall of fore bearing bearing shell 11.
Incorporated by reference to see shown in Fig. 7 and Fig. 8, rear bearing 20 comprises rear bearing bearing shell 21 and rear bearing bearing shell locating piece 22.Rear bearing bearing shell locating piece 22 is fixedly installed, and forms positioning supports effect to rear bearing bearing shell 21.Rear bearing bearing shell 21 is set on rotor 30, is fixedly installed thrust disc 33 outside the first end of rear bearing bearing shell 21.Thrust disc 33 is bolted to connection on rotor 30, forms axial force to rear bearing bearing shell 21.
Rear bearing bearing shell locating piece 22 comprises rear bearing fuel feeding distributing chute 221 in parallel and the main oil supply gallery 222 of rear bearing.Rear bearing fuel feeding distributing chute 221 in parallel is circumferentially arranged on the inwall of rear bearing bearing shell locating piece 22 in direction, forms circumferential oil supply gallery.The main oil supply gallery 222 of rear bearing is arranged along the radial direction of rear bearing bearing shell locating piece 22, and is communicated with rear bearing fuel feeding distributing chute 221 in parallel, distributes for lubricant oil being delivered to rear bearing fuel feeding distributing chute 221 in parallel.
Rear bearing bearing shell 21 comprises the radial oil supply gallery 211 of rear bearing, the axial oil supply 213 of rear bearing circumference oil supply 212, rear bearing side direction oil supply gallery and rear bearing.The radial oil supply gallery 211 of rear bearing is arranged on the neutral position of rear bearing bearing shell 21 axial direction, and the radial direction along rear bearing bearing shell 21 is arranged, and runs through the sidewall of rear bearing bearing shell 21.Rear bearing circumference oil supply 212 is arranged on the exit position of the radial oil supply gallery 211 of rear bearing along the circumferential direction of the inwall of rear bearing bearing shell 21, lubricant oil is radially introduced inwall from the outer wall of rear bearing bearing shell 21.The axial oil supply 213 of rear bearing is in axial direction arranged on the inwall of rear bearing bearing shell 21, first end along rear bearing bearing shell 21 extends to the second end of rear bearing bearing shell 21, and be connected with rear bearing circumference oil supply 212, the lubricant oil entered in rear bearing circumference oil supply 212 is in axial direction distributed between rotor 30 and rear bearing bearing shell 21, to form dynamic pressure oil film between rotor 30 and rear bearing bearing shell 21.
One end of rear bearing side direction oil supply gallery is communicated with rear bearing fuel feeding distributing chute 221 in parallel, and the other end extends to the first end endface position of rear bearing bearing shell 21.Rear bearing side direction oil supply gallery is arranged between rear bearing fuel feeding distributing chute 221 in parallel and the axial oil supply 213 of rear bearing.Rear bearing side direction oil supply gallery comprises rear bearing first side direction oil supply gallery 214 and rear bearing second side direction oil supply gallery 215.Rear bearing first side direction oil supply gallery 214 extends to the first end end face of rear bearing bearing shell 21 from the radial oil supply gallery 211 of rear bearing, is introduced between the axial load-carrying surface of rear bearing 20 and the thrust disc thrust face 35 of rotor 30 by lubricant oil from the radial oil supply gallery 211 of rear bearing.
Rear bearing bearing shell 21 also comprises fuel feeding distributing chute 221 in parallel with rear bearing and is communicated with and the heavy oilhole 216 extended along the radial direction of rear bearing bearing shell 21, heavy oilhole 216 is blind hole, and rear bearing second side direction oil supply gallery 215 extends laterally to the first end end of rear bearing bearing shell 21 from the end of heavy oilhole 216.
Rear bearing first side direction oil supply gallery 214 and rear bearing second side direction oil supply gallery 215 can obliquely be arranged, also can be horizontally disposed with along the axial direction of rear bearing bearing shell 21, the axial direction that the side direction oil supply gallery in the middle of the present embodiment is along rear bearing bearing shell 21 is horizontally disposed with.All radial oil supply gallery 211 is arranged in parallel with rear bearing for rear bearing first side direction oil supply gallery 214 and rear bearing second side direction oil supply gallery 215, thus lubricant oil is delivered to respectively the axial carrying face of rear bearing 20 and radial supporting plane.
In the endface position coordinated with thrust disc thrust face 35 of rear bearing bearing shell 21, circumferentially direction is provided with second and crosses oil groove, second crosses oil groove is communicated with the axial oil supply 213 of the rear bearing storing oil groove 31 and rear bearing bearing shell 21 on thrust disc thrust face 35, is delivered to by the lubricant oil in axial for rear bearing oil supply 213 stores in oil groove 31 by the second mistake oil groove.
Hold owing to only having a radial load-carrying surface and an axial load-carrying surface for electric motor back shaft, therefore, by the oil supply gallery of bearing machining both direction, respectively lubricant oil is caused two end faces of this bearing, and oil supply gallery is come together in rear bearing fuel feeding distributing chute 221 in parallel.For axial axis to thrust face, in order to make distribution of lubrication oil more even, at circumferentially mean allocation 4 oil supply galleries, its physical dimension feature is as follows: radial bearing surface oil supply hole d4: φ 4.5 ~ φ 7.5mm, end thrust face oil supply hole d5: φ 1 ~ φ 4mm.
Because the side direction oil supply gallery of fore bearing 10 and rear bearing 20 is arranged in parallel with radial oil supply gallery; be delivered in the process of the end thrust face of rotor and the axial load-carrying surface of bearing at lubricant oil; and without the heating of the axial mating part between rotor 30 and bearing; therefore; the oil temperature entering end thrust face can meet the effect of cooling and lubrication; lubricant oil can have better viscosity; formed and stablize dynamic pressure oil film; thus available protecting is formed to bush material, prevent the bearing bush abrasion of bearing.
Incorporated by reference to see shown in Fig. 9 to Figure 14, store oil groove 31 for being arranged on the concave inward structure on the end thrust face of rotor 30, this concave inward structure forms holding space, and is communicated with the oil supply gallery on bearing unit.Operationally, store oil groove 31 and coordinate with the load-carrying surface of bearing unit and form receiving cavity, thus lubricant oil is entered by oil supply gallery store in oil groove 31 and accumulation.
Please specifically see shown in Fig. 9 to Figure 12, the view structure of what these figures mainly illustrated the is axial direction in the rotor thrust face 34 coordinated with fore bearing 10.As can be seen from the figure, storing oil groove 31 sectional shape is in axial direction U-shaped, sectional shape along the radial direction of rotor 30 is interior concave circular arc, and this stores oil groove 31 and successively decreases along the degree of depth in the radial extension direction of rotor 30, comprise be positioned at rotor radial direction innermost layer straight and store oily section and store with this arc that oily section is connected and store oily section.Storing oil groove 31 sectional shape in axial direction also can be ellipse or other shape.
The outward edge storing oil groove 31 is provided with the oil unloading trough 32 from storing oil groove 31 and extend to the outer periphery in rotor thrust face 34, and this oil unloading trough 32 and the arc storing oil groove 31 store oily section and be connected, and are connected storing oil groove 31 with outside emptying space.After lubricant oil lubricates motor fore bearing 10 and takes away heat, come together under the influence of centrifugal force and store in oil groove 31, after storing and accumulating enough lubricant oil in oil groove 31, oil unloading trough 32 can regulate the lubricant oil stored in oil groove 31, make to store oil groove 31 can realize dynamically storing oil, and maintain oil film and form pressure needed for hydrodynamic lubrication and oil mass, thus keep the oil mass needed for bearing stable operation.The sectional shape of oil unloading trough 32 is V-type or U-shaped.The oil groove 31 that stores on rotor thrust face 34 has multiple, and is evenly distributed on rotor thrust face 34 along the circumferential direction of rotor 30, and in the middle of the present embodiment, the oil groove 31 that stores on rotor thrust face 34 has six.
The physical dimension feature that rotor thrust face stores oil groove 31 is as follows: flute length L2:15 ~ 25mm, groove width w2:15 ~ 25mm, groove depth L4:3 ~ 4mm, radius of arc A:R15 ~ R20mm, circular arc B:R15 ~ R20mm, draining groove depth L3:1 ~ 2.5mm, draining groove width w3:1 ~ 2.5mm.
Incorporated by reference to see shown in Figure 13 and Figure 14, what mainly illustrate is the view structure of the axial direction of the thrust disc thrust face 35 coordinated with rear bearing 20.As can be seen from the figure, storing oil groove 31 sectional shape is in axial direction U-shaped, and the sectional shape along the radial direction of rotor 30 is interior concave circular arc.Storing oil groove 31 sectional shape in axial direction also can be ellipse or other shape.
The outward edge storing oil groove 31 is provided with the oil unloading trough 32 from storing oil groove 31 and extend to the outer periphery of thrust disc thrust face 35, and this oil unloading trough 32 is connected storing oil groove 31 with outside emptying space.Lubricant oil holds 20 lubrications to electric motor back shaft and after taking away heat, come together under the influence of centrifugal force and store in oil groove 31, after storing and accumulating enough lubricant oil in oil groove 31, oil unloading trough 32 can regulate the lubricant oil stored in oil groove 31, make to store oil groove 31 can realize dynamically storing oil, and maintain oil film and form pressure needed for hydrodynamic lubrication and oil mass, thus keep the oil mass needed for bearing stable operation.The sectional shape of oil unloading trough 32 is V-type or U-shaped.The oil groove 31 that stores on thrust disc thrust face 35 has multiple, and is evenly distributed on thrust disc thrust face 35 along the circumferential direction of rotor 30, and in the middle of the present embodiment, the oil groove 31 that stores on thrust disc thrust face 35 has six.
The physical dimension feature that thrust disc stores oil groove 31 is as follows: flute length L5:15 ~ 25mm, groove width w4:13 ~ 20mm, groove depth L7:1 ~ 3mm, circular arc C: R15 ~ R20mm, draining groove depth L6:0.8 ~ 2mm, draining groove width w5:1.5 ~ 3mm.
Centrifugal compressor is in running, when lubricant oil enters bearing shell from the main fuel feeding runner of fore bearing 10 and rear bearing 20, be introduced into fuel feeding distributing chute in parallel around bearing shell one circle, then the radial load-carrying surface of bearing shell and axial load-carrying surface is distributed to along each fuel feeding uniform flow passage in parallel, after bearing shell being lubricated and take away heat, come together under centrifugal action and store in oil groove 31, under the adjustment of drain pan 32, store in oil groove 31 and maintain oil film and form pressure needed for hydrodynamic lubrication and oil mass, keep the oil mass needed for bearing stable operation.When centrifugal compressor stops suddenly because of power down, the lubricant oil be accumulated in oil groove 31 slowly unloads to be put, and provides emergency lubrication to bearing, makes bearing shell be unlikely to occur tile kilning phenomenon because temperature is too high, improves the reliability of compressor operating.According to embodiments of the invention, chiller plant comprises above-mentioned centrifugal compressor.
From above description, can find out, the above embodiments of the present invention achieve following technique effect: centrifugal compressor comprises rotor and is set in epitrochanterian bearing unit, rotor comprises the end thrust face coordinated with the axial load-carrying surface of bearing unit, bearing unit comprises fore bearing and rear bearing, the first end of rear bearing is outside equipped with thrust disc, thrust disc is fixedly connected on rotor, end thrust face comprises rotor thrust face and thrust disc thrust face, fore bearing is arranged between two rotor thrust faces, and the axial load-carrying surface of rear bearing coordinates with thrust disc thrust face.By arranging two rotor thrust faces to rotor, make two end thrust faces of rotor all form end thrust effect to fore bearing, thus make fore bearing two ends stress balance.Because fore bearing two ends are stressed; therefore avoid the fore bearing bearing shell problem that only stressed the caused shaft strength in one end is excessive and impaired, the stressed of fore bearing can be remained in safety range, available protecting is formed to bearing; improve the reliability of compressor operating, improve the Security of bearing.
The foregoing is only the preferred embodiments of the present invention, be not limited to the present invention, for a person skilled in the art, the present invention can have various modifications and variations.Within the spirit and principles in the present invention all, any amendment done, equivalent replacement, improvement etc., all should be included within protection scope of the present invention.
Claims (10)
1. a centrifugal compressor, the bearing unit comprising rotor (30) and be set on described rotor (30), described rotor (30) comprises the end thrust face coordinated with the axial load-carrying surface of described bearing unit, it is characterized in that, described bearing unit comprises fore bearing (10) and rear bearing (20), the first end of described rear bearing (20) is outside equipped with thrust disc (33), described thrust disc (33) is fixedly connected on described rotor (30), described end thrust face comprises rotor thrust face (34) and thrust disc thrust face (35), described fore bearing (10) is arranged between two described rotor thrust faces (34), the axial load-carrying surface of described rear bearing (20) coordinates with described thrust disc thrust face (35), described fore bearing (10) comprises fore bearing bearing shell (11) and fore bearing bearing shell locating piece (12), the periphery wall of described fore bearing bearing shell (11) is provided with fore bearing fuel feeding distributing chute (111) in parallel, described fore bearing bearing shell (11) also comprises the radial oil supply gallery (112) of fore bearing and is separately positioned on fore bearing first side direction oil supply gallery (113) and fore bearing second side direction oil supply gallery (114) of radial oil supply gallery (112) both sides of described fore bearing, the radial oil supply gallery (112) of described fore bearing radially runs through described fore bearing bearing shell (11) from described fore bearing fuel feeding distributing chute (111) in parallel, described fore bearing first side direction oil supply gallery (113) extends to the first end end face of described fore bearing bearing shell (11) from described fore bearing fuel feeding distributing chute (111) in parallel, described fore bearing second side direction oil supply gallery (114) extends to the second end end face of described fore bearing bearing shell (11) from described fore bearing fuel feeding distributing chute (111) in parallel.
2. centrifugal compressor according to claim 1, it is characterized in that, described fore bearing bearing shell (11) also comprise the exit position being arranged on the radial oil supply gallery of described fore bearing (112) fore bearing circumference oil supply (115) and along the axial oil supply (116) of the axially extended fore bearing in described fore bearing circumference oil supply (115) two ends, the axial oil supply (116) of described fore bearing coordinates with described rotor (30), axial oil supply (116) two ends of described fore bearing are provided with first and cross oil groove (117), described rotor (30) also comprises circumference to arrange and point oil groove (36) coordinated with described first mistake oil groove (117).
3. centrifugal compressor according to claim 1 and 2, it is characterized in that, described rear bearing (20) comprises rear bearing bearing shell (21) and rear bearing bearing shell locating piece (22), the inner circle wall of described rear bearing bearing shell locating piece (22) is provided with rear bearing fuel feeding distributing chute (221) in parallel, described rear bearing bearing shell (21) comprises the radial oil supply gallery (211) of rear bearing and rear bearing side direction oil supply gallery, described rear bearing side direction oil supply gallery is communicated with described rear bearing fuel feeding distributing chute (221) in parallel, along the axial direction horizontal-extending of described rear bearing bearing shell (21), and be communicated to described thrust disc thrust face (35) stores oil groove (31).
4. centrifugal compressor according to claim 1 and 2, it is characterized in that, end thrust face described at least one is provided with and stores oil groove (31), the described oil groove (31) that stores is connected with the oil supply gallery in the axial load-carrying surface of described bearing unit, described in store oil groove (31) bottom be indent arc.
5. centrifugal compressor according to claim 3, it is characterized in that, oil groove (31) is stored described in end thrust face described at least one is provided with, the described oil groove (31) that stores is connected with the oil supply gallery in the axial load-carrying surface of described bearing unit, described in store oil groove (31) bottom be indent arc.
6. centrifugal compressor according to claim 4, is characterized in that, described in store oil groove (31) outward edge be provided with and store from described the oil unloading trough (32) that oil groove (31) extends to described end thrust face outer periphery.
7. centrifugal compressor according to claim 6, is characterized in that, described oil unloading trough (32) is V-type groove or U-type groove.
8. centrifugal compressor according to claim 7, is characterized in that, described in store oil groove (31) and successively decrease along the radial extension direction degree of depth of described rotor (30).
9. centrifugal compressor according to claim 8, is characterized in that, described in store oil groove (31) and have multiple, and to be uniformly distributed along the circumferential direction of described rotor (30) on described end thrust face.
10. a chiller plant, comprises centrifugal compressor, it is characterized in that, the centrifugal compressor of described centrifugal compressor according to any one of claim 1 to 9.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201210016935.XA CN103206399B (en) | 2012-01-17 | 2012-01-17 | Centrifugal compressor and refrigeration equipment comprising same |
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| CN201210016935.XA CN103206399B (en) | 2012-01-17 | 2012-01-17 | Centrifugal compressor and refrigeration equipment comprising same |
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| CN103206399B true CN103206399B (en) | 2015-09-16 |
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| CN107882767B (en) * | 2017-12-11 | 2024-01-12 | 重庆通用工业(集团)有限责任公司 | Compressor bearing and compressor |
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| EP0154673A2 (en) * | 1983-11-30 | 1985-09-18 | Hitachi, Ltd. | Rotary fluid machine |
| DE2043550C2 (en) * | 1970-01-07 | 1985-10-03 | Judson S. Los Angeles Calif. Swearingen | Control device for the axial thrust compensation of a hydrodynamic thrust bearing arrangement |
| CN101581510A (en) * | 2009-06-23 | 2009-11-18 | 大连理工大学 | High-power super-high-speed air floatation turbine air conditioning refrigeration equipment |
| CN201461452U (en) * | 2009-07-30 | 2010-05-12 | 上海新沪电机厂有限公司 | Shielding electric pump with inner circulation structure for lithium bromide absorptive air conditioner |
| CN202402326U (en) * | 2012-01-17 | 2012-08-29 | 珠海格力电器股份有限公司 | Centrifugal compressor and refrigeration equipment comprising same |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL1018212C2 (en) * | 2001-06-05 | 2002-12-10 | Siemens Demag Delaval Turbomac | Compressor unit comprising a centrifugal compressor and an electric motor. |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2043550C2 (en) * | 1970-01-07 | 1985-10-03 | Judson S. Los Angeles Calif. Swearingen | Control device for the axial thrust compensation of a hydrodynamic thrust bearing arrangement |
| EP0154673A2 (en) * | 1983-11-30 | 1985-09-18 | Hitachi, Ltd. | Rotary fluid machine |
| CN101581510A (en) * | 2009-06-23 | 2009-11-18 | 大连理工大学 | High-power super-high-speed air floatation turbine air conditioning refrigeration equipment |
| CN201461452U (en) * | 2009-07-30 | 2010-05-12 | 上海新沪电机厂有限公司 | Shielding electric pump with inner circulation structure for lithium bromide absorptive air conditioner |
| CN202402326U (en) * | 2012-01-17 | 2012-08-29 | 珠海格力电器股份有限公司 | Centrifugal compressor and refrigeration equipment comprising same |
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