CN201339577Y - Rotor of screw rod compressor - Google Patents

Rotor of screw rod compressor Download PDF

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Publication number
CN201339577Y
CN201339577Y CNU2009200383431U CN200920038343U CN201339577Y CN 201339577 Y CN201339577 Y CN 201339577Y CN U2009200383431 U CNU2009200383431 U CN U2009200383431U CN 200920038343 U CN200920038343 U CN 200920038343U CN 201339577 Y CN201339577 Y CN 201339577Y
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CN
China
Prior art keywords
rotor
female
curved
male
compressor
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Expired - Fee Related
Application number
CNU2009200383431U
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Chinese (zh)
Inventor
夏天
邢子文
何宁
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Individual
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Individual
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Priority to CNU2009200383431U priority Critical patent/CN201339577Y/en
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Abstract

The utility model discloses a rotor of a screw rod compressor. The structure of the rotor is that: the rotor comprises a female rotor and a male rotor, the two sides of the female rotor and the male rotor are unsymmetrical, curved lines which compose the female rotor and the male rotor are circular arcs and envelope lines, the tooth ratio of the female rotor and the male rotor is 6:5, and clearances exist among teeth. The rotor is characterized in that: with the center point of the female rotor as the origin of coordinates, the clearance between the female rotor and the male rotor is within 0.044 to 0.118mm; the rotor which is manufactured according to the actual profile coordinates has the characteristics of curved-surface to curved-surface, small rotor and high rotating speed. Compared with the prior art, the rotor can completely realize the sealing of curved-surface to curved-surface, is helpful for forming a fluid power lubricating film, and can reduce transverse leakage, thereby improving the efficiency of the compressor. The rotor has the characteristics of stable meshing, less abrasion, good sealing property, convenient processing as well as detecting, weak vibration, low noise and high efficiency of the compressor.

Description

A kind of rotor of helical lobe compressor
(1) technical field:
The utility model relates to a kind of rotor, relates in particular to a kind of rotor of helical lobe compressor.
(2) background technique:
In the helical-lobe compressor, the shape of rotor has determined the performance of helical-lobe compressor substantially, the molded lines of at present existing representative rotor of helical lobe compressor mainly contains: the molded lines of certain company of Germany, the molded lines of Sweden company, and the molded lines of company such as Taiwan, Japan, these molded lines are chosen different molded lines and combination thereof, because the design orientation is different, pluses and minuses are respectively arranged, but the common drawback that prior art exists is: axially tightness is low, and efficient is low, there is cusp in curve, stress is concentrated, and is unfavorable for bearing big load, and is not easy to processing and detection.
(3) summary of the invention:
The purpose of this utility model is to provide the rotor of helical lobe compressor that a kind of axial tightness is better, efficient is high.
Invention thinking of the present utility model is:
New molded lines by the design rotor of helical lobe compressor, the sealing of safety realization " curved surface is to curved surface " between rotor when making helical-lobe compressor work, and do not comprise the sealing of any " curve-curve ", help to form the hydrodynamic lubrication film, reduction improves the efficient of compressor by the axial leakage of contact zones; Simultaneously, also be to control gap width between the negative and positive rotor well, guaranteeing unlikely interference behind the rotor expanded by heating, and can guarantee gas seal between the rotor.Thereby realize between the negative and positive rotor engagement steadily, it is little wear and tear, and good airproof performance is convenient to detect and process, and vibrates for a short time, and noise is low, the compressor efficiency height.
The utility model reaches above purpose by following measure:
A kind of rotor of helical lobe compressor, it comprises female rotor and male rotor, it is characterized by the bilateral asymmetric of female rotor and male rotor, forming curve is circular arc and envelope thereof, the gear ratio of negative and positive rotor is 6: 5, have the gap between the negative and positive rotor, it is characterized in that: the central point with female rotor is a true origin, and the gap between the negative and positive rotor is 0.044-0.118mm.
Gap width between the negative and positive rotor in the technique scheme both can guarantee unlikely interference behind the rotor expanded by heating, and can guarantee gas seal between the rotor.
When the gap between described negative and positive rotor is 0.081mm, ideal.
Further technological scheme is again:
The theory shaped wire coordinate of described negative and positive rotor following (central point with female rotor is a true origin):
Figure Y20092003834300191
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353 42.7422 19.5475 55.2708 20.6432
354 42.7173 19.6018 55.2489 20.7017
355 42.6924 19.6560 55.2270 20.7601
356 42.6674 19.7102 55.2050 20.8185
357 42.6424 19.7643 55.1829 20.8769
358 42.6172 19.8184 55.1608 20.9352
359 42.5921 19.8725 55.1386 20.9936
360 42.5668 19.9266 55.1164 21.0519
361 42.5415 19.9806 55.0941 21.1102
362 42.5161 20.0345 55.0717 21.1685
363 42.4906 20.0885 55.0493 21.2267
364 42.4651 20.1424 55.0268 21.2849
365 42.4395 20.1963 55.0043 21.3431
366 42.4138 20.2502 54.9817 21.4013
367 42.3881 20.3040 54.9590 21.4594
368 42.3795 20.3219 54.9515 21.4788
Compared with the prior art the utility model can produce following good effect:
1. the utility model composition tooth curve is circular arc, ellipse and envelope thereof, and this can make the rotor flank of tooth change face seal into by linear sealing, obviously improves sealing effect, help forming the hydrodynamic lubrication oil film, reduce tooth surface abrasion, reduce transverse leakage, improve compressor efficiency by contact zones;
2. connection is smooth between the utility model flank of tooth, and no cusp is convenient to processing and detection, and cleanliness is good, and noise is low;
3. adopt bilateral molded lines, moment is distributed rationally between rotor, vibrates little;
4. rotor tooth depth radius and addendum are reasonable, displacement and refrigerating capacity height;
5. the negative and positive root diameter is more or less the same, and rotor rigidity is approaching, the bearing capacity height.
Between the utility model negative and positive rotor engagement steadily, it is little wear and tear, good airproof performance is convenient to detect and process, and vibrates for a short time, noise is low, the compressor efficiency height.Realized goal of the invention easily.
(4) description of drawings:
Below with reference to drawings and Examples the utility model is described in further details:
Accompanying drawing 1 is the end surface shape schematic representation of negative and positive rotor in rectangular coordinate system among the utility model embodiment.
Each sequence number is respectively in the accompanying drawing: 1, female rotor; 2, male rotor.
(5) embodiment:
Referring to accompanying drawing 1, a kind of rotor of helical lobe compressor shown in the utility model embodiment comprises female rotor 1 and male rotor 2, described female rotor 1 and male rotor 2 bilateral asymmetric, forming curve is circular arc and envelope thereof, the gear ratio of negative and positive rotor is 6: 5, having the gap between the negative and positive rotor, is true origin with the central point of female rotor 1, and the actual coordinate of female rotor 1, male rotor 2 adopts the concrete profile coordinate in " more further technological scheme ".In order to save space, just do not repeat to have listed here.In entire work process, the gap length between the negative and positive rotor fluctuates about 0.081mm, but remains between 0.044-0.118mm.
Above-mentioned drawings and Examples only are used to illustrate the utility model, and protection domain of the present utility model is not constituted any limitation.

Claims (3)

1, a kind of rotor of helical lobe compressor, it comprises female rotor and male rotor, described female rotor and male rotor bilateral asymmetric, forming curve is circular arc and envelope thereof, the gear ratio of negative and positive rotor is 6: 5, have the gap between the negative and positive rotor, it is characterized in that: the central point with female rotor is a true origin, and the gap between the negative and positive rotor is 0.044-0.118mm.
2, rotor of helical lobe compressor according to claim 1 is characterized in that: the gap between described negative and positive rotor is 0.081mm.
3, rotor of helical lobe compressor according to claim 1 is characterized in that: the theory shaped wire coordinate of described negative and positive rotor following (central point with female rotor is a true origin):
Figure Y2009200383430002C1
Figure Y2009200383430004C1
Figure Y2009200383430005C1
Figure Y2009200383430007C1
Figure Y2009200383430008C1
Figure Y2009200383430009C1
Figure Y2009200383430010C1
Figure Y2009200383430011C1
Figure Y2009200383430013C1
Figure Y2009200383430014C1
Figure Y2009200383430016C1
Figure Y2009200383430017C1
CNU2009200383431U 2009-01-15 2009-01-15 Rotor of screw rod compressor Expired - Fee Related CN201339577Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2009200383431U CN201339577Y (en) 2009-01-15 2009-01-15 Rotor of screw rod compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2009200383431U CN201339577Y (en) 2009-01-15 2009-01-15 Rotor of screw rod compressor

Publications (1)

Publication Number Publication Date
CN201339577Y true CN201339577Y (en) 2009-11-04

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Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2009200383431U Expired - Fee Related CN201339577Y (en) 2009-01-15 2009-01-15 Rotor of screw rod compressor

Country Status (1)

Country Link
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104234996A (en) * 2014-06-13 2014-12-24 台州市德嘉机电科技有限公司 Measuring method of clearance leakage amount of multi-rotor screw pump
CN104728117A (en) * 2015-02-17 2015-06-24 上海偌托新能源科技有限公司 Helical teeth of compression heat pump helix main engine and compression heat pump helix main engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104234996A (en) * 2014-06-13 2014-12-24 台州市德嘉机电科技有限公司 Measuring method of clearance leakage amount of multi-rotor screw pump
CN104728117A (en) * 2015-02-17 2015-06-24 上海偌托新能源科技有限公司 Helical teeth of compression heat pump helix main engine and compression heat pump helix main engine
CN104728117B (en) * 2015-02-17 2017-03-22 上海偌托新能源科技有限公司 Helical teeth of compression heat pump helix main engine and compression heat pump helix main engine

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