US2827227A - Compressor - Google Patents
Compressor Download PDFInfo
- Publication number
- US2827227A US2827227A US413276A US41327654A US2827227A US 2827227 A US2827227 A US 2827227A US 413276 A US413276 A US 413276A US 41327654 A US41327654 A US 41327654A US 2827227 A US2827227 A US 2827227A
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- US
- United States
- Prior art keywords
- cam
- stage
- cylinders
- compressor
- pistons
- 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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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B25/00—Multi-stage pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B27/00—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
- F04B27/04—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders in star- or fan-arrangement
- F04B27/0404—Details, component parts specially adapted for such pumps
- F04B27/0414—Cams
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/18—Mechanical movements
- Y10T74/18056—Rotary to or from reciprocating or oscillating
- Y10T74/18248—Crank and slide
- Y10T74/18256—Slidable connections [e.g., scotch yoke]
Definitions
- the present invention relates to compressors, and, more particularly, to an air compressor of the multistage type which is an improvement over the four-stage radial compressor disclosed in United States Patent No. 2,562,954.
- compressors of the type described in the aforementioned patent can be operated at high speeds to supply compressed air or other gases at pressures of 3000 pounds per square inch and a satisfactory rate of flow, it has been found that the compressors vibrate considerably and that the keystone member and follower means are subjected to excessive wear.
- an object of the present invention is to provide a radial multi-stage compressor wherein vibrations are reduced to a minimum.
- Another object is to provide such a compressor wherein the wear life of the cam and follower means is prolonged.
- Another object is to reduce the size and mass of such a compressor without sacrifice of flow rate or output pressure.
- a further object is to simplify the design of such compressors to thereby reduce the cost thereof and facilitate manufacture and assembly.
- the foregoing objects are accomplished by embodying improvements in such compressors which comprise arranging the cylinders so that two are in vertical alignment and two are in horizontal alignment, preferably with the longitudinal axes of the vertical cylinders and one of the horizontal cylinders intersecting at the axis about which the shaft rotates (the other horizontal cylinder being ofiset with respect to the shaft axis) and with the first stage cylinder opposite the fourth stage cylinder and the second stage cylinder opposite the third stage cylinder; providing a cam having two cam surfaces at the sides which are parallel to each other and a third surface at the bottom which is perpendicular to the parallel surfaces with the fourth stage piston cam follower means engaging the bottom surface and the second and third stage piston cam follower means engaging the side surfaces; and providing cam follower means which are rigid with respect to the pistons carrying the same, and which preferably are integrally formed or secured therewith.
- a preferred embodiment of the invention has been chosen for purposes of illustration and description, and is shown in the accompanying drawing, forming a part of the specification, wherein the single figure is a front elevational view, partly in longitudinal section, of a radial multi-stage compressor illustrating the essential elements of the present invention and their arrangement.
- a radial 2,827,227 Patented Mar. 18, 1958 multi-stage compressor generally comprising a casing or housing 10 having a first stage cylinder 11 at the top, sec ond and third stage cylinders 12 and 13 at the sides and a fourth stage cylinder 14 at the bottom; a drive shaft 15 (shown in broken lines) journalled for rotation and supported by the casing, for example, as shown in the aforementioned patent, including an eccentric, such as a crank 16 within the casing; pistons 17, 13, 19 and 20 for the first, second, third and fourth stage cylinders, respectively; and a cam 21 carried by the crank which is operatively associated with the pistons for effecting recip rocation thereof.
- first and fourth stage cylinders are in vertical alignment and the second and third stage cylinders are substantially in horizontal alignment but with axis of the third stage cylinder slightly above the axis of the second stage cylinder. In this manner, torque forces acting on the cam about the axis of the shaft are minimized, and the sum of the components of the vertical forces is substantially equal to that of the horizontal forces.
- the first stage piston 17 carries a horizontal pin or rod 22 at the lower end thereof which extends through a horizontal bearing aperture 23 at the upper end of the cam 21 to slidably connect the cam and piston, whereby circular movement of the cam under the influence of the crank imparts reciprocating movement to the piston 17.
- the cam 21, as shown, has a pair of vertical, parallel side surfaces 24 and 25, and a horizontal bottom surface 26 perpendicular to the side surfaces.
- the second, third and fourth stage pistons have cam follower means 27, 28 and 29, respectively, for engaging the cam surfaces in the order named.
- the cam follower means are in the form of rigid heads integrally formed or secured at the inner ends of their respective pistons and having fiat faces parallel to the cam surface they engage.
- the pistons 18, 19 and 20 are so arranged that they do not displace all the air compressed in their cylinders, whereby the compressed air remaining therein is effective to cause the pistons to be urged towards the cam block 21 after their compression stroke to maintain their followers in engagement with the cam surfaces.
- the cam followers of the horizontal second and third stage pistons serve as a slide or guide to maintain the cam in vertical alignment and all the forces applied between the cam and these followers are parallel to the pin 22, whereby no wedging forces are applied between the pin and the cam so that the wear life of the pin and the bearing is greatly prolonged.
- the only forces applied between these elements are sliding friction between the pin and the bearing, and the vertical thrust of the cam bearing on the pin in moving the first stage piston up and down.
- the followers are constantly in sliding engagement with the cam surfaces without freedom of movement other than such sliding movement, whereby noise and vibration are practically eliminated within the compressor casing.
- the present invention provides a highly improved radial multi-stage compressor'which has a high output weight rating, at a given pressure, and which is economical to manufacture'and durable in construction.
- V p 1 In a radial multi-stage compressor, the combination of a driveshaft including an eccentric, first, second, third and fourth stage cylinders, said cylinders being radially disposed with respect to said shaft and spaced circumferentially with respect to each other with two of said cylinders in vertical alignment and two'of said cylinders substantially in horizontal alignment, acarn mem ber carried by said eccentric for movement in a circular path, said cam member having three linear surfaces, 21
- pistons for said second, third and fourth stage cylinders having follower means each adapted to be slidably engaged; by a surface of said cam-member to effect reciprocation of the last mentioned pistons, the longitudinal axes'of said vertical" cylinders'and one of said horizontal cylinders intersecting at the axis about which said shaft rotates, and the axis of the other of said horizontal cylinders extending slightly above the shaft axis.
Description
March 18 1958 A. E. SCHMiDLlN ETAL 2,
- COMPRESSOR Filed March 1, 1954 FIRST STAGE spam/b $734 CF w/zw 5 224 as F0 UR TH 67?; c5
INVENTORS A/Jerlvsl78o1ngiofi'l; Warren E. Herr ATTORNEY United States Patent C) COMPRESSOR Albertus E. Schmidlin, Caldwell, and Warren E. Herr,
Hasbrouck Heights, N. 3., assignors to Specialties Developrnent Corporation, Belleville, N. 1., a corporation of New Jersey Application March 1, 1954, Serial No. 413,276
5 Claims. (Cl. 230-184) The present invention relates to compressors, and, more particularly, to an air compressor of the multistage type which is an improvement over the four-stage radial compressor disclosed in United States Patent No. 2,562,954.
While compressors of the type described in the aforementioned patent can be operated at high speeds to supply compressed air or other gases at pressures of 3000 pounds per square inch and a satisfactory rate of flow, it has been found that the compressors vibrate considerably and that the keystone member and follower means are subjected to excessive wear.
Accordingly, an object of the present invention is to provide a radial multi-stage compressor wherein vibrations are reduced to a minimum.
Another object is to provide such a compressor wherein the wear life of the cam and follower means is prolonged.
Another object is to reduce the size and mass of such a compressor without sacrifice of flow rate or output pressure.
A further object is to simplify the design of such compressors to thereby reduce the cost thereof and facilitate manufacture and assembly.
Other and further objects of the invention will be obvious upon an understanding of the illustrative embodiment about to be described, or will be indicated in the appended claims, and various advantages not referred to herein will occur to one skilled in the art upon employ ment of the invention in practice.
In accordance with the invention, the foregoing objects are accomplished by embodying improvements in such compressors which comprise arranging the cylinders so that two are in vertical alignment and two are in horizontal alignment, preferably with the longitudinal axes of the vertical cylinders and one of the horizontal cylinders intersecting at the axis about which the shaft rotates (the other horizontal cylinder being ofiset with respect to the shaft axis) and with the first stage cylinder opposite the fourth stage cylinder and the second stage cylinder opposite the third stage cylinder; providing a cam having two cam surfaces at the sides which are parallel to each other and a third surface at the bottom which is perpendicular to the parallel surfaces with the fourth stage piston cam follower means engaging the bottom surface and the second and third stage piston cam follower means engaging the side surfaces; and providing cam follower means which are rigid with respect to the pistons carrying the same, and which preferably are integrally formed or secured therewith.
A preferred embodiment of the invention has been chosen for purposes of illustration and description, and is shown in the accompanying drawing, forming a part of the specification, wherein the single figure is a front elevational view, partly in longitudinal section, of a radial multi-stage compressor illustrating the essential elements of the present invention and their arrangement.
Referring to the drawing, there is shown a radial 2,827,227 Patented Mar. 18, 1958 multi-stage compressor generally comprising a casing or housing 10 having a first stage cylinder 11 at the top, sec ond and third stage cylinders 12 and 13 at the sides and a fourth stage cylinder 14 at the bottom; a drive shaft 15 (shown in broken lines) journalled for rotation and supported by the casing, for example, as shown in the aforementioned patent, including an eccentric, such as a crank 16 within the casing; pistons 17, 13, 19 and 20 for the first, second, third and fourth stage cylinders, respectively; and a cam 21 carried by the crank which is operatively associated with the pistons for effecting recip rocation thereof.
As shown herein the first and fourth stage cylinders are in vertical alignment and the second and third stage cylinders are substantially in horizontal alignment but with axis of the third stage cylinder slightly above the axis of the second stage cylinder. In this manner, torque forces acting on the cam about the axis of the shaft are minimized, and the sum of the components of the vertical forces is substantially equal to that of the horizontal forces.
The details of the inlets and outlets of the cylinders and the valving associated therewith, and the outer ends of the pistons are not shown because the present invention is not concerned therewith. A suitable arrangement of such elements is illustrated in the aforementioned pat cut. The outlets of the first, second and third stage cylinders are respectively connected to the inlets of the second, third and fourth stage cylinders. The bore of the cylinders decreases in the order in which the cylinders are named numerically.
The first stage piston 17 carries a horizontal pin or rod 22 at the lower end thereof which extends through a horizontal bearing aperture 23 at the upper end of the cam 21 to slidably connect the cam and piston, whereby circular movement of the cam under the influence of the crank imparts reciprocating movement to the piston 17.
The cam 21, as shown, has a pair of vertical, parallel side surfaces 24 and 25, and a horizontal bottom surface 26 perpendicular to the side surfaces. The second, third and fourth stage pistons have cam follower means 27, 28 and 29, respectively, for engaging the cam surfaces in the order named. As shown herein, the cam follower means are in the form of rigid heads integrally formed or secured at the inner ends of their respective pistons and having fiat faces parallel to the cam surface they engage. Also, as illustrated in the aforementioned patent, the pistons 18, 19 and 20 are so arranged that they do not displace all the air compressed in their cylinders, whereby the compressed air remaining therein is effective to cause the pistons to be urged towards the cam block 21 after their compression stroke to maintain their followers in engagement with the cam surfaces.
With this arrangement, the cam followers of the horizontal second and third stage pistons serve as a slide or guide to maintain the cam in vertical alignment and all the forces applied between the cam and these followers are parallel to the pin 22, whereby no wedging forces are applied between the pin and the cam so that the wear life of the pin and the bearing is greatly prolonged. The only forces applied between these elements are sliding friction between the pin and the bearing, and the vertical thrust of the cam bearing on the pin in moving the first stage piston up and down. Also, since tilting movement of the cam is prevented and the cam followers are rigid, the followers are constantly in sliding engagement with the cam surfaces without freedom of movement other than such sliding movement, whereby noise and vibration are practically eliminated within the compressor casing.
By arranging the stages as indicated herein, the forces acting on the cam and the forces transmitted by the cam are almost in perfect dynamic balance. This also is in- 3 struniental in reducing vibr'ati'on'and wear of contacting parts. In viewof such vibration and wearreduction, the
compressor may be smaller in mass and size than prior compressors of this general type having the same output flow and pressure rating. V
From the foregoing description, it will be seen that the present invention provides a highly improved radial multi-stage compressor'which has a high output weight rating, at a given pressure, and which is economical to manufacture'and durable in construction.
As various changes may be made 'in the form, construction and arrangement of the parts herein, without departing from the spirit and scope'of the invention and without sacrificing any of its advantages, it is to be understood that all matter herein is to be interpreted as illus trative and not in any limiting sense.
Weclaim': V p 1; In a radial multi-stage compressor, the combination of a driveshaft including an eccentric, first, second, third and fourth stage cylinders, said cylinders being radially disposed with respect to said shaft and spaced circumferentially with respect to each other with two of said cylinders in vertical alignment and two'of said cylinders substantially in horizontal alignment, acarn mem ber carried by said eccentric for movement in a circular path, said cam member having three linear surfaces, 21
piston for said first stage cylinder, means for slidably connecting 'said cam member to said piston whereby said cam member imparts reciprocating motion thereto, and
' pistons for said second, third and fourth stage cylinders having follower means each adapted to be slidably engaged; by a surface of said cam-member to effect reciprocation of the last mentioned pistons, the longitudinal axes'of said vertical" cylinders'and one of said horizontal cylinders intersecting at the axis about which said shaft rotates, and the axis of the other of said horizontal cylinders extending slightly above the shaft axis.
2. A compressor according, to claim 1, wherein two of said cam surfaces are parallel to each other and the, other of said cam surfaces :isperpendicular to said two parallel surfaces.
3. A compressor according-to claim 2, whereinzsaid 7 I References Cited in thefile of this patent UNITED STATES PATENTS 2,427,253 Browne Sept. 9', 1'94? 2,450,468 Cornelius Oct. 5, 1948 2,562,954 Schmidlin Aug. 7, 1951 V FOREIGN PATENTS 902,097 France Nov. 27; 1944 France Oct. 15, 1952
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US413276A US2827227A (en) | 1954-03-01 | 1954-03-01 | Compressor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US413276A US2827227A (en) | 1954-03-01 | 1954-03-01 | Compressor |
Publications (1)
Publication Number | Publication Date |
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US2827227A true US2827227A (en) | 1958-03-18 |
Family
ID=23636595
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US413276A Expired - Lifetime US2827227A (en) | 1954-03-01 | 1954-03-01 | Compressor |
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US (1) | US2827227A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3068526A (en) * | 1958-10-10 | 1962-12-18 | Kenneth F Croan | Improved method of molding thinwalled articles from expandable thermoplastic beads |
US3077836A (en) * | 1960-02-01 | 1963-02-19 | Kobe Inc | High speed triplex pump |
US3093301A (en) * | 1960-07-05 | 1963-06-11 | Mitchell Co John E | Lubricating system for compressor |
US5846059A (en) * | 1995-08-24 | 1998-12-08 | Sanyo Electric Co., Ltd. | Scotch yoke mechanism for multistage compressor having a spring-biased liner plate |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR902097A (en) * | 1943-09-28 | 1945-08-17 | Freins Hydrauliques Sa Des | Hydraulic pump |
US2427253A (en) * | 1943-09-21 | 1947-09-09 | American Brake Shoe Co | Epicyclic drive |
US2450468A (en) * | 1943-10-01 | 1948-10-05 | Richard T Cornelius | Motor-driven compressor |
US2562954A (en) * | 1947-02-26 | 1951-08-07 | Specialties Dev Corp | Compressor |
FR1018559A (en) * | 1950-05-24 | 1953-01-09 | Piston compressor |
-
1954
- 1954-03-01 US US413276A patent/US2827227A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2427253A (en) * | 1943-09-21 | 1947-09-09 | American Brake Shoe Co | Epicyclic drive |
FR902097A (en) * | 1943-09-28 | 1945-08-17 | Freins Hydrauliques Sa Des | Hydraulic pump |
US2450468A (en) * | 1943-10-01 | 1948-10-05 | Richard T Cornelius | Motor-driven compressor |
US2562954A (en) * | 1947-02-26 | 1951-08-07 | Specialties Dev Corp | Compressor |
FR1018559A (en) * | 1950-05-24 | 1953-01-09 | Piston compressor |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3068526A (en) * | 1958-10-10 | 1962-12-18 | Kenneth F Croan | Improved method of molding thinwalled articles from expandable thermoplastic beads |
US3077836A (en) * | 1960-02-01 | 1963-02-19 | Kobe Inc | High speed triplex pump |
US3093301A (en) * | 1960-07-05 | 1963-06-11 | Mitchell Co John E | Lubricating system for compressor |
US5846059A (en) * | 1995-08-24 | 1998-12-08 | Sanyo Electric Co., Ltd. | Scotch yoke mechanism for multistage compressor having a spring-biased liner plate |
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