CN1092764C - Closed rotary compressor - Google Patents
Closed rotary compressor Download PDFInfo
- Publication number
- CN1092764C CN1092764C CN97111459A CN97111459A CN1092764C CN 1092764 C CN1092764 C CN 1092764C CN 97111459 A CN97111459 A CN 97111459A CN 97111459 A CN97111459 A CN 97111459A CN 1092764 C CN1092764 C CN 1092764C
- Authority
- CN
- China
- Prior art keywords
- cylinder
- exhaust port
- running shaft
- rotary compressor
- mentioned
- 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.)
- Expired - Lifetime
Links
- 238000005057 refrigeration Methods 0.000 claims description 14
- 230000006835 compression Effects 0.000 claims description 11
- 238000007906 compression Methods 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 8
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 238000007599 discharging Methods 0.000 claims description 4
- 239000003921 oil Substances 0.000 description 13
- 239000003795 chemical substances by application Substances 0.000 description 11
- 239000003507 refrigerant Substances 0.000 description 5
- 238000007789 sealing Methods 0.000 description 3
- 238000005303 weighing Methods 0.000 description 3
- 238000004804 winding Methods 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000005728 strengthening Methods 0.000 description 2
- 238000004378 air conditioning Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005755 formation reaction Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C18/00—Rotary-piston pumps specially adapted for elastic fluids
- F04C18/30—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F04C18/34—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members
- F04C18/356—Rotary-piston pumps specially adapted for elastic fluids having the characteristics covered by two or more of groups F04C18/02, F04C18/08, F04C18/22, F04C18/24, F04C18/48, or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F04C18/08 or F04C18/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the outer member
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/0021—Systems for the equilibration of forces acting on the pump
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/06—Silencing
- F04C29/068—Silencing the silencing means being arranged inside the pump housing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
- F04C29/12—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet
- F04C29/124—Arrangements for admission or discharge of the working fluid, e.g. constructional features of the inlet or outlet with inlet and outlet valves specially adapted for rotary or oscillating piston pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2240/00—Components
- F04C2240/50—Bearings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
Abstract
To heighten output and improve C.O.P. by specifying the ratio of the diameter of a rotary shaft from the upper end to the eccentric part to the diameter of the rotary shaft from the eccentric part to the lower end. This rotary shaft 4 is integratedly formed out of an upper rotary shaft 4a (diameter D1), an eccentric part 18, and a lower rotary shaft 4b (diameter D2), the diameter D2 of the lower rotary shaft 4b is made smaller than the diameter D1 of the upper rotary shaft 4a, and hence a problem that a roller 19 can not be mounted on the eccentric part 18 is not generated even if the eccentricity is enlarged. The ratio (D2/D1) is less than one, and it is favorably desired to be over 12.5/16 and less than one. In the case of being less than 12.5/16, a problem of shortage of strength is generated in the rotary shaft 4.
Description
The present invention relates to closed rotary compressor, specifically, relate to high powerization and improve the closed rotary compressor of usefulness coefficient (C.O.P).
Fig. 7 is the sectional view of the existing closed rotary compressor that is used for air-conditioning, refrigeration etc. (real fair 3-26309 number of Japanese patent gazette).
Among Fig. 7, the 50th, the bottom is provided with the seal container of oil storage tank 51, is placing electric assembly 52 at this container internal upper part, and rotation compression assembly 53 is being placed in the bottom.Electric assembly 52 is by being installed in running shaft 54 upper rotor parts 55 and constituting at the stator 57 that periphery forms oil return ditch 56.The 58th, the air clearance that between the interior week of the periphery of rotor 55 and stator 57, forms.59 are mounted in the semi-circular balace weight on the end ring 60 of rotor 55, and 61 are contained in the coil-end of the coiling 62 of stator 57 inside.
The roller 65 that rotation compression assembly 53 rotate cylinder 63 in by cylinder 63, by the eccentric part 64 of running shaft 54, join with this roller and separates the blade 66 of cylinder 63 inside, the upper bearing (metal) portion 67 of sealing cylinder opening and lower bearing portion 68, in this lower bearing portion, have the exhaust port 69A (scheming not show) of expulsion valve 69 and cup-shaped baffler 70 formations of this tap hole of covering.71 are provided in a side of the tap hole in the upper bearing (metal) portion 67, and this tap hole is by being located at the path 72 and cup-shaped baffler 70 internal communication on the cylinder 63.
The 73rd, run through the discharge tube of seal container 50 center upper portion, the opening end of this discharge tube is installed in to be had end circular cone tubular refrigeration agent to suck cup 74 to cover on seal container 50 inwalls.The 75th, penetrate the through hole that refrigeration agent sucks cup 74 bottom center, this through hole is near also facing toward running shaft 54.
In the hermetic type compressor of this structure, the refrigeration agent that has compressed through rotation compression assembly 53 is sent to the top of this electric assembly by the air clearance 58 of electric assembly 52.The refrigeration agent that is sent to electric assembly 52 tops is under the rotary centrifugal force effect of rotor 55, and what inside was contained is oily separated.This isolated oil is thrown toward stator 57 1 sides.Therefore, only have the refrigerant gas that does not contain oil on the top of rotor 55, this refrigerant gas flows into from the through hole 75 that is located at refrigeration agent and sucks cup 74 bottoms and sucks in the cup, be discharged to seal container 50 from discharge tube 73 beyond.The oil return ditch that separated oil forms from stator 57 peripheries turns back to the oil storage tank 51 of seal container 50.
Fig. 4 (a) is the sectional view that last running shaft 54a (diameter D1), eccentric part 64, following running shaft 54b (diameter D1) is plotted the existing running shaft 54 of one, and roller 65 is installed on eccentric part 64.Fig. 4 (b) is a sectional view of seeing the running shaft 54 of above-mentioned (a) from the bottom up.
Fig. 5 is explanation cylinder 63, roller 65, blade 66, exhaust port 69A, exhaust port 69A to the explanatory drawing of relation between the part 69B of cylinder 63 inner openings etc.
In order to strengthen the power output of closed rotary compressor, consider to strengthen offset E (bias at the center of the center of running shaft 54 and eccentric part 64 shown in Fig. 4 (b)).But when strengthening this offset E, the external diameter of roller 65 (R) will reduce thereupon, and the wall thickness of roller 65 is also wanted attenuate.The external diameter of eccentric part 64 to be changed over suitable external diameter.
Existing running shaft 54 will be gone up running shaft 54a (diameter D1), eccentric part 64, running shaft 54b (diameter D1) becomes one down, because the diameter D1 of last running shaft 54a is identical with the diameter D1 of following running shaft 54b, so, when having strengthened offset E, exist the problem that roller 65 can not be contained on the eccentric part 64.
As shown in Figure 5, exhaust port 69A is towards the bore portions 69B (part shown in the dotted line) of cylinder 63 inner openings, is by the end face seal of the roller 65 that is capped bore portions 69B, so, when the wall thickness of roller 65 reduced, sealing was not tight, will increase from roller 65 end face gas leakages.
In addition, as adopting the top clearance volume that does not enlarge exhaust port 69A (if enlarge the top clearance volume, then can bring the disadvantage that increases invalid volume), single position that only changes exhaust port 69A, reduce when the area of the bore portions 69B of cylinder 63 inner openings solves this problem, the passage resistance that can cause again discharging gas increases, and the usefulness coefficient (C.O.P) of closed rotary compressor is reduced.
The present invention aims to provide a kind of high output rating and improves the closed rotary compressor of C.O.P.
The present inventor is through research with keen determination, will be if verified by last running shaft, eccentric part, the following running shaft diameter of the whole running shaft formed of rotary part is done forr a short time than last running shaft diameter down, roller can not be installed to the problem on the eccentric part in the time of then can solving increasing offset E.In addition, owing to roller wall thickness also can be thickeied thereupon, even exhaust port strengthens towards the bore portions area of cylinder inner opening, also can fully seal, can solve the problem of gas from the roller face leakage, so, can realize that high outputization improves usefulness coefficient (C.O.P) simultaneously.Made the present invention thus.
The invention of claim 1 of the present invention is a kind of closed rotary compressor, in seal container, the electric assembly with running shaft is being placed on top, is placing by the shaft-driven compression assembly of the rotation of this electric assembly the bottom, after the refrigeration agent that sucks is compressed by this compression assembly and is discharged in the seal container, discharge outside seal container, the rotation compression assembly is by the cylinder that has suction port again, the roller that in cylinder, rotates by the eccentric part of running shaft, join with this roller and separate the blade in space in the cylinder, seal uncovered upper bearing (metal) portion of cylinder and lower bearing portion, be located at the exhaust port that has expulsion valve in this upper bearing (metal) portion, the cup-shaped baffler that covers this expulsion valve constitutes; It is characterized in that, with above-mentioned running shaft from the upper end to the eccentric part one section diameter D1 with make less than 1 from running shaft ratio (D2/D1) of diameter D2 of one section from the eccentric part to the lower end.
The invention of claim 2 of the present invention, be in the described closed rotary compressor of claim 1, to increase following feature, promptly, do not enlarge the top clearance volume of above-mentioned exhaust port, in order to reduce the passage resistance of discharging gas, above-mentioned exhaust port is decided to be more than 50% towards the bore portions area of the cylinder inner opening ratio with the full basal area of exhaust port.
The invention of claim 3 of the present invention, be in the described closed rotary compressor of claim 2, to increase following feature, that is, leak from above-mentioned exhaust port, the wall thickness of above-mentioned roller is made and can be sealed towards the thickness of the above-mentioned bore portions of cylinder inner opening in order to prevent refrigeration agent.
The invention of claim 4 of the present invention is to increase following feature in the described closed rotary compressor in arbitrary top in claim 1 to 3, that is, above-mentioned than (D2/D1) greater than 12.5/16 less than 1.
Fig. 1 is the sectional view of one of expression closed rotary compressor of the present invention example.
Fig. 2 (a) is the sectional view of the used running shaft of the present invention.
Fig. 2 (b) is the sectional view from running shaft shown in the Fig. 2 (a) that sees up down.
Fig. 3 is the explanatory drawing that illustrates that the used cylinder of the present invention, roller, blade, exhaust port, exhaust port concern between the orifice part of cylinder inner opening grades.
Fig. 4 (a) is the sectional view of existing running shaft.
Fig. 4 (b) is the sectional view from running shaft shown in the Fig. 4 (a) that sees up down.
Fig. 5 is the explanatory drawing that illustrates that existing cylinder, roller, blade, exhaust port, exhaust port concern between the orifice part of cylinder inner opening grades.
Fig. 6 is expression towards the bore portions area of the cylinder inner opening plotted curve with respect to usefulness coefficient (C.O.P) ratio of the ratio of the full basal area of exhaust port and closed rotary compressor.
Fig. 7 is the sectional view of existing closed rotary compressor.
Below, with reference to the description of drawings embodiments of the invention.
Fig. 1 is the sectional view of expression closed rotary compressor one example of the present invention.
Among Fig. 1, the 1st, the bottom has the seal container of oil storage tank 2, and in this seal container, electric assembly 3 is being settled on top, and the rotation compression assembly 5 by running shaft 4 drivings of electric assembly is being settled in the bottom.Electric assembly 3 is made of the stator 6 and the rotor 8 that are fixed on seal container 1 inwall, and rotor 8 and this stator interior be across air clearance 7, and is sleeved on the running shaft 4.Stator 6 is made of iron core 10 and coil 12, and unshakable in one's determination 10 periphery otch forms oil return ditch 9, and coil 12 has two winding terminals 11 up and down.Rotor 8 constitutes with the winding end ring 14 that is located at this iron core upper and lower end by unshakable in one's determination 13.
Semiorbicular upper flat weighing apparatus 15 and lower flat weighing apparatus 16 are installed on this winding end ring 14.The roller 19 that rotation compression assembly 5 rotate cylinder 17 in by cylinder 17, by the eccentric part 18 of running shaft 4, and this roller joins and with the blade 20 of cylinder 17 inner spaces separation, seal cylinder 17 uncovered upper bearing (metal) portion 21 and lower bearing portion 22, be located at the exhaust port 23A that has expulsion valve 23 in the upper bearing (metal) portion, the cup-shaped baffler 24 that covers this delivery port constitutes.Above the cup-shaped baffler, be provided with exhaust port 25 at this towards lower flat weighing apparatus 16 revolving graties.
The 26th, refrigerant discharge leader, this refrigerant discharge leader run through the top cover 27 on sealing seal container 1 top.The 28th, liquid container, the 29th, separating plate.Arrow is represented refrigerant flow direction.
In the closed rotary compressor of this structure, compressed together by roller 19 and blade 20 from the refrigeration agent that suction port 30 flows in the cylinder 17 through liquid container 28, from the open expulsion valve 23 of exhaust port 23A, be discharged in the cup-shaped baffler 24.Refrigeration agent in this cup-shaped cover is discharged to the top of electric assembly 3 from the air clearance 7 of exhaust port 25 by electric assembly 3.The refrigeration agent that is discharged to electric assembly 3 tops is subjected to the drive of rotor 8 and rotates, and the heavy oil of the quality that its inside is contained is rotated centrifugal force and gets rid of to the inwall of seal container 1 and separate.Refrigeration agent after oil separates is outside discharge tube 26 is discharged to seal container 1.The oil that separates returns oil storage tank 2 from the oil return ditch 9 of stator 6.
Fig. 2 (a) is the sectional view of the used running shaft 4 of expression the present invention, and this running shaft 4 will be gone up running shaft 4a (diameter D1), eccentric part 18, running shaft 4b (diameter D2) consists of one down, and roller 19 is contained on the eccentric part 18.Fig. 2 (b) is the sectional view from running shaft 4 shown in the Fig. 2 (a) that sees up down.
Fig. 3 is explanation the present invention used cylinder 17, roller 19, blade 20, exhaust port 23A, exhaust port 23A towards the explanatory drawing of relation between the bore portions 23B of cylinder 17 openings etc.
The used running shaft 4 of the present invention is that last running shaft 4a (diameter D1), eccentric part 18, following running shaft 4b (diameter D2) are become one, and the diameter D2 of following running shaft 4b is less than the diameter D1 of last running shaft 4a, therefore, even the problem on the eccentric part 18 can not appear roller 19 can not being installed in increasing offset E yet., be preferably greater than 12.5/16 less than 1 than (D2/D1) less than 1.If less than 12.5/16, then there is the not enough problem of running shaft semi-finals degree.
As shown in Figure 3, delivery port 23A is capped the end face seal of the roller 19 of bore portions 23B towards the bore portions 23B (part shown in the dotted line) of cylinder 17 inner openings, because the used roller 19 of the present invention has the thickness that can fully seal, so solved the problem of gas from roller 19 face leakages.
As shown in Figure 3, do not change the top clearance volume of exhaust port 23A, only change the position of exhaust port 23A, promptly strengthened towards the orifice area of cylinder 17 inner openings than the time, usefulness coefficient (C.O.P) result of the closed rotary compressor of mensuration (discharging volume 13.3cc, nominal power 700W) is as shown in Figure 6.
The transverse axis of Fig. 6 is represented exhaust port 23A towards the area of the bore portions 23B of the cylinder 17 inner openings ratio with respect to the full basal area of exhaust port 23A, and the longitudinal axis represents that with existing above-mentioned ratio be the C.O.P ratio that 30% o'clock C.O.P was made as at 1 o'clock.
From Fig. 6 as seen, when strengthening above-mentioned ratio, the C.O.P rate value increases, and it is 50% ideal when above that above-mentioned ratio is decided to be.
Because the present invention has above-mentioned structure, so can realize the high outputization of closed rotary compressor and improve usefulness coefficient (C.O.P).
Claims (4)
1. closed rotary compressor, in seal container, the electric assembly with running shaft is being settled on top, is settling by the shaft-driven compression assembly of the rotation of this electric assembly the bottom, after the refrigeration agent that sucks is compressed by this compression assembly and is discharged in the seal container, discharge outside seal container, the rotation compression assembly is by the cylinder that has suction port again, the roller that in cylinder, rotates by rotating shaft eccentric portion, join with this roller and with the blade of separated by spaces in the cylinder, seal uncovered upper bearing (metal) portion of cylinder and lower bearing portion, be located at the exhaust port that has expulsion valve in this upper bearing (metal) portion, the cup-shaped baffler that covers this expulsion valve constitutes; It is characterized in that, from the upper end of above-mentioned running shaft to one section diameter (D1) of eccentric part with from the eccentric part running shaft to the ratio (D2/D1) of one section diameter (D2) of lower end less than 1.
2. closed rotary compressor as claimed in claim 1, it is characterized in that, do not enlarging under the top clearance volume situation of above-mentioned exhaust port mouth, in order to reduce the passage resistance of discharging gas, above-mentioned exhaust port is set at more than 50% towards the bore portions area of the cylinder inner opening ratio with the full basal area of exhaust port.
3. closed rotary compressor as claimed in claim 2 is characterized in that, leaks from above-mentioned exhaust port in order to prevent refrigeration agent, the wall thickness of above-mentioned roller is made the thickness that is enough to seal towards the above-mentioned bore portions of cylinder inner opening.
4. as each the described closed rotary compressor in the claim 1 to 3, it is characterized in that, above-mentioned than (D2/D1) greater than 12.5/16 less than 1.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP143069/96 | 1996-06-05 | ||
| JP8143069A JPH09324777A (en) | 1996-06-05 | 1996-06-05 | Closed type rotary compressor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1170829A CN1170829A (en) | 1998-01-21 |
| CN1092764C true CN1092764C (en) | 2002-10-16 |
Family
ID=15330205
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN97111459A Expired - Lifetime CN1092764C (en) | 1996-06-05 | 1997-05-30 | Closed rotary compressor |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JPH09324777A (en) |
| KR (1) | KR100447514B1 (en) |
| CN (1) | CN1092764C (en) |
| ID (1) | ID20455A (en) |
| SG (1) | SG75119A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101008389B (en) * | 2006-01-27 | 2010-05-19 | 东芝开利株式会社 | Hermetic rotary compressor and refrigeration cycle device having hermetic rotary compressor |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100414109C (en) * | 2002-12-25 | 2008-08-27 | 乐金电子(天津)电器有限公司 | Rotating shaft fixer of rotary compressor |
| CN106321617B (en) * | 2016-10-26 | 2023-10-31 | 上海海立电器有限公司 | Crankshaft and rotary compressor |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0183332A1 (en) * | 1984-11-13 | 1986-06-04 | Tecumseh Products Company | Suction tube seal for a rotary compressor |
| CN87103613A (en) * | 1986-05-20 | 1987-12-16 | 三洋电机株式会社 | Hermetically sealed rotary compressor |
| EP0438922A1 (en) * | 1989-12-28 | 1991-07-31 | Kabushiki Kaisha Toshiba | Refrigerant compressor for HFC 134a |
| EP0450847A1 (en) * | 1990-03-30 | 1991-10-09 | Kabushiki Kaisha Toshiba | Refrigerant compressor |
| EP0608116A1 (en) * | 1993-01-22 | 1994-07-27 | Copeland Corporation | Multiple compressor in a single shell |
| US5509786A (en) * | 1992-07-01 | 1996-04-23 | Ubukata Industries Co., Ltd. | Thermal protector mounting structure for hermetic refrigeration compressors |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS59115491A (en) * | 1982-12-21 | 1984-07-03 | Toshiba Corp | Enclosed compressor |
-
1996
- 1996-06-05 JP JP8143069A patent/JPH09324777A/en active Pending
-
1997
- 1997-03-19 KR KR1019970009297A patent/KR100447514B1/en not_active IP Right Cessation
- 1997-05-30 CN CN97111459A patent/CN1092764C/en not_active Expired - Lifetime
- 1997-06-05 SG SG1997001923A patent/SG75119A1/en unknown
- 1997-06-05 ID IDP971918A patent/ID20455A/en unknown
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0183332A1 (en) * | 1984-11-13 | 1986-06-04 | Tecumseh Products Company | Suction tube seal for a rotary compressor |
| CN87103613A (en) * | 1986-05-20 | 1987-12-16 | 三洋电机株式会社 | Hermetically sealed rotary compressor |
| EP0438922A1 (en) * | 1989-12-28 | 1991-07-31 | Kabushiki Kaisha Toshiba | Refrigerant compressor for HFC 134a |
| EP0450847A1 (en) * | 1990-03-30 | 1991-10-09 | Kabushiki Kaisha Toshiba | Refrigerant compressor |
| US5509786A (en) * | 1992-07-01 | 1996-04-23 | Ubukata Industries Co., Ltd. | Thermal protector mounting structure for hermetic refrigeration compressors |
| EP0608116A1 (en) * | 1993-01-22 | 1994-07-27 | Copeland Corporation | Multiple compressor in a single shell |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101008389B (en) * | 2006-01-27 | 2010-05-19 | 东芝开利株式会社 | Hermetic rotary compressor and refrigeration cycle device having hermetic rotary compressor |
Also Published As
| Publication number | Publication date |
|---|---|
| KR100447514B1 (en) | 2004-11-16 |
| SG75119A1 (en) | 2000-09-19 |
| CN1170829A (en) | 1998-01-21 |
| JPH09324777A (en) | 1997-12-16 |
| ID20455A (en) | 1998-12-24 |
| KR980002868A (en) | 1998-03-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20021016 |