US3617158A - Multistage rotary compressor - Google Patents
Multistage rotary compressor Download PDFInfo
- Publication number
- US3617158A US3617158A US6382A US3617158DA US3617158A US 3617158 A US3617158 A US 3617158A US 6382 A US6382 A US 6382A US 3617158D A US3617158D A US 3617158DA US 3617158 A US3617158 A US 3617158A
- Authority
- US
- United States
- Prior art keywords
- chambers
- pistons
- pressure stage
- partition plate
- cams
- 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
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Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/10—Construction relative to lubrication
- F16C33/1025—Construction relative to lubrication with liquid, e.g. oil, as lubricant
- F16C33/106—Details of distribution or circulation inside the bearings, e.g. details of the bearing surfaces to affect flow or pressure of the liquid
- F16C33/1065—Grooves on a bearing surface for distributing or collecting the liquid
-
- 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
- F04C18/3562—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 the inner and outer member being in contact along one line or continuous surfaces substantially parallel to the axis of rotation
- F04C18/3564—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 the inner and outer member being in contact along one line or continuous surfaces substantially parallel to the axis of rotation the surfaces of the inner and outer member, forming the working space, being surfaces of revolution
-
- 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
- F04C23/00—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
- F04C23/001—Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids of similar working principle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/10—Sliding-contact bearings for exclusively rotary movement for both radial and axial load
Definitions
- COMPRESSOR ABSTRACT A multistage rotary compressor having longitudinally aligned cylindrical chambers in which cylindrical ro- U.S. Cl tar-y pistons are eccentrically mounted on a shaft A longitu.
- This invention relates to a compressor of air or other gas to be installed at the chemical plant, liquefied-gas tanker, refrigerating apparatus or the like.
- An object of this invention is to provide a rotary compressor which is able to carry out multistage compression without combining with other rotary compressors.
- FIG. 1 is a perspective view of a compressor in accordance with this invention
- FIG. 2 is a longitudinal sectional view thereof
- FIG. 3 is a sectional view taken along the line 3-3 of FIG. 2.
- a double-stage rotary compressor in accordance with this invention, in which the cylindrical casing accordance with this invention, in which the cylindrical casing 10 is divided into the low-pressure stage side cylinder 14 and the high-pressure stage side cylinder 15 by means of partition plates 11, 12 and 13.
- a rotary shaft 17 is supported in the casing 10, and rotary pistons 18, 18a eccentrically fixed to the shaft are accommodated in each cylinder.
- a longitudinal partition plate 20 is arranged in paral lel relation to the cylinder axis and provided in the casing 10 for sliding movement along the radial direction of the cylinder with its inner edge being always kept in engagement with the outer periphery of the rotary pistons.
- the partition plate 20 is provided at longitudinal opposite ends thereof with cam followers 21 and 22 which are in engagement with cams 23 and 24 secured to the rotary shaft 17. Suction ports 25, 26 and discharge ports 27, 28 are formed in the casing 10 at the both sides of the partition plate 20 in the low-pressure stage side and high-pressure stage side, respectively.
- This cooled gas is further fed into the high-pressure stage side cylinder 15 through the suction port 26, and as the highpressure stage side rotary piston 18a rotates it is compressed and discharged through the discharge valve and the discharge port 28.
- the low-pressure stage side rotary piston 18 and the high-pressure stage side rotary piston 18a are provided in-phase relation to each other, but it can be also permitted to provide phase difference between both pistons 18 and 18a.
- the partition plate 20 is divided into two parts.
- this invention provides a single rotary compressor, which can carry out a multistage compression, which is of simplified construction and compact, and which can increase the volumetric, compression, and mechanical efficiencies. Further gases fed from several systemsunder different conditions can be efficiently compressed by a single compressor in accordance with this invention.
- a multistage rotary compressor comprising a casing having low-pressure stage and high-pressure stage cylinder chambers disposed coaxially therein, a shaft mounted coaxial with said chambers for rotation in said casing within said chambers, an eccentric rotary piston in each chamber supported for rotation therein by said shaft, at least two eccentric cams mounted on said shaft for rotation thereby, the eccentricity of said pistons and earns being in phase, a single longitudinal partition plate dividing said chambers and kept in engagement with the pistons therein by said cams, suction and discharge ports in the cylindrical wall of each chamber at opposite side of said partition plate, and an intermediate cooler connecting the discharge port of the low-pressure stage chamber with the suction port of the high-pressure stage chamber to cool the gas between the two stages of compression.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Oil, Petroleum & Natural Gas (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
- Reciprocating Pumps (AREA)
Abstract
A multistage rotary compressor having longitudinally aligned cylindrical chambers in which cylindrical rotary pistons are eccentrically mounted on a shaft. A longitudinal partition plate is slidably mounted in the casing to project into the chambers and engage against the pistons as they rotate, the position of the partition plate being determined by cams eccentrically mounted on the shaft. Gas suction and discharge ports are provided in the cylindrical wall of each chamber on opposite sides of the partition and the low-pressure discharge is directed into the high-pressure suction port by way of an intermediate cooler which operates to cool the partially compressed gas.
Description
nited States Paint 1 amuse [72] Inventors Masakazu Yamamoto 1,047,436 12/1912 OConnor 418/1 1 Tokyo; 1,385,101 7/1921 Twardowsky 418/11 Kenji Inaba, Koube, both of Japan 2,804,260 8/1957 Nilsson et a1. 41819 X [21] Appl. No. 6,382 3,106,871 10/1963 Stein 418/11 [22] Filed Jan. 28, 1970 3,107,846 10/1963 Mihalakis 418/11 [45] Patented Nov. 2, 1971 73 Assignee msni Shipbuilding and Engineering Co., 5; utl ky J p Attorney-Howson & Howson [32] Priority, Feb. 8, 1969, 44/9674 [54] COMPRESSOR ABSTRACT: A multistage rotary compressor having longitudinally aligned cylindrical chambers in which cylindrical ro- U.S. Cl tar-y pistons are eccentrically mounted on a shaft A longitu.
418/245 dinal partition plate is slidably mounted in the casing to pro- [51] Int. Cl F0lc 1/30, j into the chambers and engage against the pistons as they F010 l1/ 1 rotate, the position of the partition plate being determined by FliEld of Search 418/11, 12 cams eccent ically mounted on the haft Gas uction and discharge ports are provided in the cylindrical wall of each [56] Reierences cued chamber on opposite sides of the partition and the low-pres- UNITED STATES PATENTS sure discharge is directed into the high-pressure suction port 346,741 8/1886 Elliott 418/11 by way of an intermediate cooler which operates to cool the 647,015 4/1900 Miller 418/11 partially compressed gas.
PATENTEnuuv 2 IBYI mvENrons' YAMAMOTO MASAKAZU BY KENJ! INABA Maw/44 W ATT S.
MULTISTAGE ROTARY COMPRESSOR This invention relates to a compressor of air or other gas to be installed at the chemical plant, liquefied-gas tanker, refrigerating apparatus or the like.
l-Ieretofore in the reciprocating compressor generally at above a compression ratio of 8-9, deterioration of lubricating oil has been accelerated with overheated discharge-gas, thus causing remarkable decrease in durability of compressor. Also because of considerable decrease of volumetric efficiency and compression efficiency, a large-sized compressor should have been used in combination with other compressors of the same type or rotary type in order to increase discharge pressure, while a small-sized compressor should have to make multistage compression of two or three stages by dividing multiple cylinders into 23 cylinder groups.
On the other hand, in the rotary compressor the temperature of discharged gas is not risen so high and the volumetric efficiency is not so decreased as that of reciprocating compressor, therefore it is able to increase the compression ratio up to 25 by single stage. However, because of an unavoidable decrease in the compression efficiency, it has been necessary to use a compressor in combination with other compressors of the same type to form a multistage compressor in case of high compression ratio.
An object of this invention is to provide a rotary compressor which is able to carry out multistage compression without combining with other rotary compressors.
Further objects of this invention will become apparent from the following description with reference to the accompanying drawings in which:
FIG. 1 is a perspective view of a compressor in accordance with this invention;
FIG. 2 is a longitudinal sectional view thereof; and
FIG. 3 is a sectional view taken along the line 3-3 of FIG. 2.
Referring now to the drawing, there is shown a double-stage rotary compressor in accordance with this invention, in which the cylindrical casing accordance with this invention, in which the cylindrical casing 10 is divided into the low-pressure stage side cylinder 14 and the high-pressure stage side cylinder 15 by means of partition plates 11, 12 and 13. A rotary shaft 17 is supported in the casing 10, and rotary pistons 18, 18a eccentrically fixed to the shaft are accommodated in each cylinder. A longitudinal partition plate 20 is arranged in paral lel relation to the cylinder axis and provided in the casing 10 for sliding movement along the radial direction of the cylinder with its inner edge being always kept in engagement with the outer periphery of the rotary pistons. The partition plate 20 is provided at longitudinal opposite ends thereof with cam followers 21 and 22 which are in engagement with cams 23 and 24 secured to the rotary shaft 17. Suction ports 25, 26 and discharge ports 27, 28 are formed in the casing 10 at the both sides of the partition plate 20 in the low-pressure stage side and high-pressure stage side, respectively.
With the compressor of this invention being constructed as mentioned above, when the rotary shaft 17 turns in the direction of the arrow shown in FIG. 3, gas is sucked into the low-pressure stage side cylinder 14 through the suction port 25 and progressively compressed as rotation of the rotary piston. The gas is then exhausted through a discharge valve 30 in the discharge port 27 of the low-pressure stage side and delivered into an intermediate cooler 31 where the gas is cooled.
This cooled gas is further fed into the high-pressure stage side cylinder 15 through the suction port 26, and as the highpressure stage side rotary piston 18a rotates it is compressed and discharged through the discharge valve and the discharge port 28.
In the arrangement of this embodiment, the low-pressure stage side rotary piston 18 and the high-pressure stage side rotary piston 18a are provided in-phase relation to each other, but it can be also permitted to provide phase difference between both pistons 18 and 18a. In that case the partition plate 20 is divided into two parts.
As it IS evident from the above-mentioned this invention provides a single rotary compressor, which can carry out a multistage compression, which is of simplified construction and compact, and which can increase the volumetric, compression, and mechanical efficiencies. Further gases fed from several systemsunder different conditions can be efficiently compressed by a single compressor in accordance with this invention.
We claim:
1. A multistage rotary compressor comprising a casing having low-pressure stage and high-pressure stage cylinder chambers disposed coaxially therein, a shaft mounted coaxial with said chambers for rotation in said casing within said chambers, an eccentric rotary piston in each chamber supported for rotation therein by said shaft, at least two eccentric cams mounted on said shaft for rotation thereby, the eccentricity of said pistons and earns being in phase, a single longitudinal partition plate dividing said chambers and kept in engagement with the pistons therein by said cams, suction and discharge ports in the cylindrical wall of each chamber at opposite side of said partition plate, and an intermediate cooler connecting the discharge port of the low-pressure stage chamber with the suction port of the high-pressure stage chamber to cool the gas between the two stages of compression.
2. A compressor according to claim 1 wherein said rotary pistons and cams are cylindrical in outline.
3. A compressor according to claim 2 wherein said chambers are of equal diameter and are separated by transverse partition plates bearing against the ends of pistons, and said longitudinal partition plate has slots slidably receiving said transverse partition plates.
Claims (3)
1. A multistage rotary compressor comprising a casing having low-pressure stage and high-pressure stage cylinder chambers disposed coaxially therein, a shaft mounted coaxial with said chambers for rotation in said casing within said chambers, an eccentric rotary piston in each chamber supported for rotation therein by said shaft, at least two eccentric cams mounted on said shaft for rotation thereby, the eccentricity of said pistons and cams being in phase, a single longitudinal partition plate dividing said chambers and kept in engagement with the pistons therein by said cams, suction and discharge ports in the cylindrical wall of each chamber at opposite side of said partition plate, and an intermediate cooler connecting the discharge port of the low-pressure stage chamber with the suction port of the high-pressure stage chamber to cool the gas between the two stages of compression.
2. A compressor according to claim 1 wherein said rotary pistons and cams are cylindrical in outline.
3. A compressor according to claim 2 wherein said chambers are of equal diameter and are separated by transverse partition plates bearing against the ends of pistons, and said longitudinal partition plate has slots slidably receiving said transverse partition plates.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP967469 | 1969-02-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3617158A true US3617158A (en) | 1971-11-02 |
Family
ID=11726744
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US6382A Expired - Lifetime US3617158A (en) | 1969-02-08 | 1970-01-28 | Multistage rotary compressor |
Country Status (7)
Country | Link |
---|---|
US (1) | US3617158A (en) |
AT (1) | AT295726B (en) |
CH (1) | CH498300A (en) |
DE (1) | DE2005566A1 (en) |
FR (1) | FR2032793A5 (en) |
GB (1) | GB1299065A (en) |
NL (1) | NL7001354A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4360327A (en) * | 1980-04-23 | 1982-11-23 | Wang Liang Chih | Multipurpose, synchronous, three angle-cross compressor |
US4451214A (en) * | 1980-06-09 | 1984-05-29 | Rokuro Kagamiyama | Rotary piston type fluid machine |
DE3540445A1 (en) * | 1984-11-22 | 1986-05-28 | Mitsubishi Denki K.K., Tokio/Tokyo | TWO-CYLINDER ROTATIONAL COMPRESSOR |
DE4318737A1 (en) * | 1993-06-05 | 1994-12-08 | Juergen Kaiser | Rotary piston compressor |
US6095783A (en) * | 1998-02-20 | 2000-08-01 | Hansen; Craig N. | Fluid mover |
CN100441871C (en) * | 2003-06-17 | 2008-12-10 | 乐金电子(天津)电器有限公司 | Eccentric piston device for sealed rotary compressor |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4141677A (en) * | 1977-08-15 | 1979-02-27 | Ingersoll-Rand Company | Scroll-type two stage positive fluid-displacement apparatus with intercooler |
AT395202B (en) * | 1989-12-13 | 1992-10-27 | Haider Gottfried Dipl Ing | Rotary-piston compressor |
CN106704191A (en) * | 2017-03-07 | 2017-05-24 | 东莞市风能工业设备有限公司 | Multi-stage cam compressor |
Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US346741A (en) * | 1886-08-03 | X elliott | ||
US647015A (en) * | 1899-08-23 | 1900-04-10 | Charles E Miller | Rotary steam-engine. |
US1047436A (en) * | 1912-04-15 | 1912-12-17 | Thomas O'connor | Double spiral pump. |
US1385101A (en) * | 1919-09-12 | 1921-07-19 | Central Scientific Co | Vacuum-pump |
US2804260A (en) * | 1949-07-11 | 1957-08-27 | Svenska Rotor Maskiner Ab | Engines of screw rotor type |
US3106871A (en) * | 1957-12-11 | 1963-10-15 | Clyde R Stein | Hydraulic motor |
US3107846A (en) * | 1961-10-10 | 1963-10-22 | Aim Pump Corp | Rotary pump or motor |
-
1970
- 1970-01-28 US US6382A patent/US3617158A/en not_active Expired - Lifetime
- 1970-01-30 NL NL7001354A patent/NL7001354A/xx unknown
- 1970-02-03 GB GB5063/70A patent/GB1299065A/en not_active Expired
- 1970-02-03 AT AT96670A patent/AT295726B/en not_active IP Right Cessation
- 1970-02-05 CH CH168570A patent/CH498300A/en not_active IP Right Cessation
- 1970-02-06 DE DE19702005566 patent/DE2005566A1/en active Pending
- 1970-02-06 FR FR7004290A patent/FR2032793A5/fr not_active Expired
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US346741A (en) * | 1886-08-03 | X elliott | ||
US647015A (en) * | 1899-08-23 | 1900-04-10 | Charles E Miller | Rotary steam-engine. |
US1047436A (en) * | 1912-04-15 | 1912-12-17 | Thomas O'connor | Double spiral pump. |
US1385101A (en) * | 1919-09-12 | 1921-07-19 | Central Scientific Co | Vacuum-pump |
US2804260A (en) * | 1949-07-11 | 1957-08-27 | Svenska Rotor Maskiner Ab | Engines of screw rotor type |
US3106871A (en) * | 1957-12-11 | 1963-10-15 | Clyde R Stein | Hydraulic motor |
US3107846A (en) * | 1961-10-10 | 1963-10-22 | Aim Pump Corp | Rotary pump or motor |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4360327A (en) * | 1980-04-23 | 1982-11-23 | Wang Liang Chih | Multipurpose, synchronous, three angle-cross compressor |
US4451214A (en) * | 1980-06-09 | 1984-05-29 | Rokuro Kagamiyama | Rotary piston type fluid machine |
DE3540445A1 (en) * | 1984-11-22 | 1986-05-28 | Mitsubishi Denki K.K., Tokio/Tokyo | TWO-CYLINDER ROTATIONAL COMPRESSOR |
US4764097A (en) * | 1984-11-22 | 1988-08-16 | Mitsubishi Denki Kabushiki Kaisha | Two-cylinder type rotary compressor |
DE4318737A1 (en) * | 1993-06-05 | 1994-12-08 | Juergen Kaiser | Rotary piston compressor |
US6095783A (en) * | 1998-02-20 | 2000-08-01 | Hansen; Craig N. | Fluid mover |
CN100441871C (en) * | 2003-06-17 | 2008-12-10 | 乐金电子(天津)电器有限公司 | Eccentric piston device for sealed rotary compressor |
Also Published As
Publication number | Publication date |
---|---|
GB1299065A (en) | 1972-12-06 |
CH498300A (en) | 1970-10-31 |
FR2032793A5 (en) | 1970-11-27 |
AT295726B (en) | 1972-01-10 |
NL7001354A (en) | 1970-08-11 |
DE2005566A1 (en) | 1970-09-24 |
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