US2129960A - Rotary compressor - Google Patents
Rotary compressor Download PDFInfo
- Publication number
- US2129960A US2129960A US123211A US12321137A US2129960A US 2129960 A US2129960 A US 2129960A US 123211 A US123211 A US 123211A US 12321137 A US12321137 A US 12321137A US 2129960 A US2129960 A US 2129960A
- Authority
- US
- United States
- Prior art keywords
- rotor
- vanes
- casing
- parts
- outlet
- 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
- 239000012530 fluid Substances 0.000 description 8
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000002745 absorbent Effects 0.000 description 1
- 239000002250 absorbent Substances 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 210000003462 vein Anatomy 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
- 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
- F04C29/126—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 of the non-return type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C21/00—Component parts, details or accessories not provided for in groups F01C1/00 - F01C20/00
- F01C21/08—Rotary pistons
- F01C21/0809—Construction of vanes or vane holders
- F01C21/0818—Vane tracking; control therefor
- F01C21/0827—Vane tracking; control therefor by mechanical means
- F01C21/0845—Vane tracking; control therefor by mechanical means comprising elastic means, e.g. springs
-
- 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
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K15/00—Check valves
- F16K15/02—Check valves with guided rigid valve members
- F16K15/04—Check valves with guided rigid valve members shaped as balls
- F16K15/042—Check valves with guided rigid valve members shaped as balls with a plurality of balls
-
- 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
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K15/00—Check valves
- F16K15/02—Check valves with guided rigid valve members
- F16K15/04—Check valves with guided rigid valve members shaped as balls
- F16K15/044—Check valves with guided rigid valve members shaped as balls spring-loaded
-
- 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
- F16K—VALVES; TAPS; COCKS; ACTUATING-FLOATS; DEVICES FOR VENTING OR AERATING
- F16K2200/00—Details of valves
- F16K2200/20—Common housing having a single inlet, a single outlet and multiple valve members
- F16K2200/204—Common housing having a single inlet, a single outlet and multiple valve members in series
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/7722—Line condition change responsive valves
- Y10T137/7837—Direct response valves [i.e., check valve type]
- Y10T137/7838—Plural
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/7722—Line condition change responsive valves
- Y10T137/7837—Direct response valves [i.e., check valve type]
- Y10T137/7904—Reciprocating valves
- Y10T137/7922—Spring biased
- Y10T137/7927—Ball valves
- Y10T137/7928—With follower
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/87571—Multiple inlet with single outlet
- Y10T137/87676—With flow control
- Y10T137/87684—Valve in each inlet
Definitions
- the principal object of my invention is to so construct and mount these vanes and the rotor that a highly eiilcient seal is obtained between the relatively moving parts which eliminates the probability of leakage therepast.
- Another object is to arrange the outlet check valves so that the compressor may deliver compressed fluid to the outlet at different pressures, as may be desired, without change in the con- 18 struction of the compressor or in-the speed of the rotor and without the need of utilizing adjust able check valves or the like
- Figure l is a side view of the improved compressor partly in section and with the side plate of the casing removed.
- Figure 2 is a vertical transverse section substantially on the line 2--2 of Fig. 1.
- the compressor comprises a cylindrical rotor I mounted on an axial shaft 2.
- the rotor is tumably supported in a casing 3 which from the top for a certain arcuate distance in the direction of rota tion of the rotor is concentric and has a running lit with the rotor as at I; and for the remainder ,of its circumferential extent is eccentric to the rotor.
- a fluid intake paxage member 5 is formed with the casing and delivers to the same at a point some distance beyond the concentric por-.
- the ports 1 communicate with a common outlet chamber l3 thereabove, which has a large, top outlet port ll normally closed by an upwardly movable ball l2.
- the port ll communicates with the main outlet chamber i3 towhich the outlet passage member I4 is attached.
- the rotor is formed with a plurality of evenly spaced radial slots i5 extending from side to side, the ends of these slots being covered by-plates l6 rigidly secured on and the same diameter; as the rotor, and completely countersunk in the end walls of the casing as shown in Fig. 2, said walls'outwardly of the rotor being spaced th same as the width of 'the rotor. 1
- the casing engaging vanes Slidable in the slots l5 are the casing engaging vanes, alternate ones 19 of which are relatively long while the intermediate ones 20 are relatively short.
- the vanes i9 are arranged to engage the circular wall of the casing throughout its extent, while the vanes 20 only engage said wall for the portions of the same adjacent the intake and outlet ports. The purpose of this is to provide the desired sealed fluid retaining pockets close to the outlet where necessary, while eliminating the additional friction which would be had by the engagement of said vanes 20 along the major portion of the casing wall.
- and 22 are arranged for lateral separating movement and have a step out in connection with each other at their adjacent ends as shown at 24. These parts are yieldably pressed apart, to cause, them to closely engagethe end walls of the, casing, by an enclosed compressing spring 25.
- and 22 are provided with a symmetrically disposed T-shaped recess in which the part 23 of similar form is fitted, so that said part is in effect completely countersunk in the parts 21 and 22.
- a strip of felt or other absorbent material 26 is preferably disposed be- 45 tween and extends along the head of part 23 and the adjacent surfaces of parts 2! and 22.
- a radial compression spring 21 acts on the base of part 23 to not only hold the felt strip in coinpressed and tightly sealing relationship with the 50, vane parts, but holds the vane as a whole in close yielding contact with the circular wall of the-casing.
- the vanes 20 are each formed of only two laterally separable parts arranged the same as the corresponding parts of the vanes I9 and yieldably pressed apart by an enclosed spring 28.
- Transversely spaced radial compression springs 29 act on the parts of the vanes 20 to force the same outwardly.
- Outward movement of said vanes is limited by pins 30 seated in the rotor at the ends of and extending across the adjacent portions of the corresponding slots l5, and riding in recesses 3
- a rotor having radial slots, vanes slidably mounted in said slots, said vanes each comprising a pair of sections step-cut at adjacent ends and disposed in overlapping relation, said'sections being movableapart axially of the rotor, an inverted T-shaped slot cut in each vane from the inner end and centrally of its sides, a T-shaped element disposed in said slot, a compression spring interposed between said sections outwardly of the slot and acting to force the sections apart, and another compression spring extending radially between the central leg of'said inverted T-shaped element and the rotor to force each vane radially out.
- a device as in claim 1 in which the inner end of the central leg of the'element is formed with a radial bore to receive the outer end of said other spring, and the rotor is formed with a radial bore to receive the other end of the spring, whereby'to prevent displacement of said spring.
- a rotary compressor including a substantially circular shell, a cylindrical rotor mounted in the shell, said shell being mainly eccentric to the rotor and engaging the same at one point, radial vanes slidably mounted in the rotor to engage the peripheral wall of the shell throughout its entire extent, a row of circumferentially spaced ports in said peripheral wall immediately adjacent but ahead of said one point; a plurality of separate outwardly opening steel ball valves normally closingsaid ports, said row of ports and the steel ball valves seated therein being disposed in a circular plane substantially concentric with the axis of the shell, an outlet pressure chamber into which said valved ports open, a curved plate having its inner face substantially concentric with the axis of the shell disposed in HARRY A.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Rotary Pumps (AREA)
Description
Sept.13,1938. H. A. PRESBY 2,129,960-
ROTARY COMPRESSOR Filed Jan. 30, 19:57 2 Sheets-Sheet 1 14 Raga 12 7 J 8 7 0 20 II", "I 31 I I' I 1 19 O j o 17 2o 16 O O O I O O a V INVENTOR E A. PresJay Y gm Sept. 13, 1938. HA. PRSBY 2,129,960
I ROTARY COMPRESSOR Filed Jan. 50, 1937 2 sheets-sheet 2 INVENTOR v HA.Pre.slay
. BY Q ATTORNEY Patented Sept. 13, 1938 2,129,960
, UNITED STATES PATENT OFFICE M. Smith and twenty-five-perccnt to B. P. Craig, both of Sacramento, Calif.
Application January 30, 1937, Serial No. 123,211
4 Claims.
the walls of the casing.
The principal object of my invention is to so construct and mount these vanes and the rotor that a highly eiilcient seal is obtained between the relatively moving parts which eliminates the probability of leakage therepast.
Another object is to arrange the outlet check valves so that the compressor may deliver compressed fluid to the outlet at different pressures, as may be desired, without change in the con- 18 struction of the compressor or in-the speed of the rotor and without the need of utilizing adjust able check valves or the like These objects I accomplish by means of such structure and relative arrangement of parts as will fully appear by a perusal of the following specification and claims. I In the drawings similar characters of reference indicate corresponding parts in the several views:
Figure l is a side view of the improved compressor partly in section and with the side plate of the casing removed. I
Figure 2 is a vertical transverse section substantially on the line 2--2 of Fig. 1.
Referring now more particularly to the characters of reference thedrawings, the compressor comprises a cylindrical rotor I mounted on an axial shaft 2. The rotor is tumably supported in a casing 3 which from the top for a certain arcuate distance in the direction of rota tion of the rotor is concentric and has a running lit with the rotor as at I; and for the remainder ,of its circumferential extent is eccentric to the rotor. A fluid intake paxage member 5 is formed with the casing and delivers to the same at a point some distance beyond the concentric por-.
tion 4 as shown at 6.
Formed in the top of the casing ahead of the portion I is av circumferentially spaced series of transverse rows of ports I normally closed by upwardly opening ball checks 8. These are all engaged and yieldably held closed by a spring pressed plate 9 arranged for independent upward movement at either end. The ports 1 communicate with a common outlet chamber l3 thereabove, which has a large, top outlet port ll normally closed by an upwardly movable ball l2. The port ll communicates with the main outlet chamber i3 towhich the outlet passage member I4 is attached.
The rotor is formed with a plurality of evenly spaced radial slots i5 extending from side to side, the ends of these slots being covered by-plates l6 rigidly secured on and the same diameter; as the rotor, and completely countersunk in the end walls of the casing as shown in Fig. 2, said walls'outwardly of the rotor being spaced th same as the width of 'the rotor. 1
The-inner surface of the casing as well as the outer surface of the rotor and its end plates are machined and finished throughout so as to provide a close running fit. Endless or segmental rings ll are countersunk in the end walls of the casing and the plates l6 concentric with the shaft 2 and are engaged on one side by springs 5 [8 which act to force the rings against the opposite engaging surfaces. In thismanner possi-' ble leakage past the rotor is prevented. I
Slidable in the slots l5 are the casing engaging vanes, alternate ones 19 of which are relatively long while the intermediate ones 20 are relatively short. The vanes i9 are arranged to engage the circular wall of the casing throughout its extent, while the vanes 20 only engage said wall for the portions of the same adjacent the intake and outlet ports. The purpose of this is to provide the desired sealed fluid retaining pockets close to the outlet where necessary, while eliminating the additional friction which would be had by the engagement of said vanes 20 along the major portion of the casing wall.
The vanes I9-are made up of three parts 2|, 22 and 23 as shown in Fig. 2. The parts 2| and 22 are arranged for lateral separating movement and have a step out in connection with each other at their adjacent ends as shown at 24. These parts are yieldably pressed apart, to cause, them to closely engagethe end walls of the, casing, by an enclosed compressing spring 25. At their inner ends the parts 2| and 22 are provided with a symmetrically disposed T-shaped recess in which the part 23 of similar form is fitted, so that said part is in effect completely countersunk in the parts 21 and 22. A strip of felt or other absorbent material 26 is preferably disposed be- 45 tween and extends along the head of part 23 and the adjacent surfaces of parts 2! and 22. A radial compression spring 21 acts on the base of part 23 to not only hold the felt strip in coinpressed and tightly sealing relationship with the 50, vane parts, but holds the vane as a whole in close yielding contact with the circular wall of the-casing. By means of this vane construction, close contact of the vane with the walls of the casing, and take-up as wear occurs is automatically at- 55 tained, without the possibility of leakage past the mainsplit parts of the vane from side to side,
. since the inner end of the step cut 24 is closed by the felt.
The vanes 20 are each formed of only two laterally separable parts arranged the same as the corresponding parts of the vanes I9 and yieldably pressed apart by an enclosed spring 28. Transversely spaced radial compression springs 29 act on the parts of the vanes 20 to force the same outwardly. Outward movement of said vanes is limited by pins 30 seated in the rotor at the ends of and extending across the adjacent portions of the corresponding slots l5, and riding in recesses 3| cut in the ends of the vanes 20. These pins and recesses are of course disposed so that the recesses are never exposed outwardly of the periphery of the rotor.
In operation it will be seen that with the rotation of the rotor, by means of power applied to the shaft 2, the fluid from the intake 5 is drawn into the casing and conflned as individual masses by the adjacent vanes l8.
As each such mass of fluid approaches the outlet portions it is divided into two parts by the veins 2!! which then engage the circular wall of the casing. If a relatively low pressure is present in the pressure chambersilfl and I3, as determined by the pressure in the outlet I l and the pressure reservoir etc. to which it leads, the first row of balls! are left. This'is because the com- I pressed fluid between adjacent vanes and converging walls of the rotor and easing at that point will be sufllcient to overcome the resistance to opening of said balls. If a greater P u e is in said chambers which correspondingly increases the resistance to opening of the balls, the vanes must move further around to more highly conflne and compress the individual masses of fluid, and either the intermediate or last row of balls will then open. The compressor thus compresses the fluid before discharging the samev to the expresent and preferred construction of the device,
still in practice such deviations from such detail may be resorted to as do not form a departure from the spirit of the invention, as deflned'by the appended claims.
Having thus described my invention, what I claim as new and useful and desire to secure by Letters Patent is:
1. In a rotary compressor, a rotor having radial slots, vanes slidably mounted in said slots, said vanes each comprising a pair of sections step-cut at adjacent ends and disposed in overlapping relation, said'sections being movableapart axially of the rotor, an inverted T-shaped slot cut in each vane from the inner end and centrally of its sides, a T-shaped element disposed in said slot, a compression spring interposed between said sections outwardly of the slot and acting to force the sections apart, and another compression spring extending radially between the central leg of'said inverted T-shaped element and the rotor to force each vane radially out.
2. A device as in claim 1 in which the inner end of the central leg of the'element is formed with a radial bore to receive the outer end of said other spring, and the rotor is formed with a radial bore to receive the other end of the spring, whereby'to prevent displacement of said spring.
3. In a rotary compressor including a substantially circular shell, a cylindrical rotor mounted in the shell, said shell being mainly eccentric to the rotor and engaging the same at one point, radial vanes slidably mounted in the rotor to engage the peripheral wall of the shell throughout its entire extent, a row of circumferentially spaced ports in said peripheral wall immediately adjacent but ahead of said one point; a plurality of separate outwardly opening steel ball valves normally closingsaid ports, said row of ports and the steel ball valves seated therein being disposed in a circular plane substantially concentric with the axis of the shell, an outlet pressure chamber into which said valved ports open, a curved plate having its inner face substantially concentric with the axis of the shell disposed in HARRY A. PRESBY.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US123211A US2129960A (en) | 1937-01-30 | 1937-01-30 | Rotary compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US123211A US2129960A (en) | 1937-01-30 | 1937-01-30 | Rotary compressor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2129960A true US2129960A (en) | 1938-09-13 |
Family
ID=22407325
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US123211A Expired - Lifetime US2129960A (en) | 1937-01-30 | 1937-01-30 | Rotary compressor |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2129960A (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2878753A (en) * | 1954-03-17 | 1959-03-24 | American Brake Shoe Co | Vane pump |
| US3931810A (en) * | 1973-07-06 | 1976-01-13 | Mcgathey Wendell H | Rotary-piston internal combustion engine |
| DE3105665A1 (en) | 1980-02-20 | 1982-03-18 | Barmag Barmer Maschinenfabrik Ag, 5630 Remscheid | "Vane vacuum pump with pre-evacuation of the suction chamber, especially for power-assisted braking in motor vehicles" |
| US4408968A (en) * | 1980-03-12 | 1983-10-11 | Nippon Soken, Inc. | Rotary compressor |
| US4639199A (en) * | 1983-04-02 | 1987-01-27 | Leybold-Heraeus Gmbh | Two-shaft vacuum pump with internal compression |
| DE3153685C2 (en) * | 1980-02-20 | 1991-04-25 | Barmag Ag, 5630 Remscheid, De | Sliding vane pump for vehicle braking |
| US6539913B1 (en) | 2002-01-14 | 2003-04-01 | William P. Gardiner | Rotary internal combustion engine |
| US20140369878A1 (en) * | 2011-11-24 | 2014-12-18 | Calsonic Kansei Corporation | Gas compressor |
-
1937
- 1937-01-30 US US123211A patent/US2129960A/en not_active Expired - Lifetime
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2878753A (en) * | 1954-03-17 | 1959-03-24 | American Brake Shoe Co | Vane pump |
| US3931810A (en) * | 1973-07-06 | 1976-01-13 | Mcgathey Wendell H | Rotary-piston internal combustion engine |
| DE3105665A1 (en) | 1980-02-20 | 1982-03-18 | Barmag Barmer Maschinenfabrik Ag, 5630 Remscheid | "Vane vacuum pump with pre-evacuation of the suction chamber, especially for power-assisted braking in motor vehicles" |
| DE3153685C2 (en) * | 1980-02-20 | 1991-04-25 | Barmag Ag, 5630 Remscheid, De | Sliding vane pump for vehicle braking |
| US4408968A (en) * | 1980-03-12 | 1983-10-11 | Nippon Soken, Inc. | Rotary compressor |
| US4639199A (en) * | 1983-04-02 | 1987-01-27 | Leybold-Heraeus Gmbh | Two-shaft vacuum pump with internal compression |
| US6539913B1 (en) | 2002-01-14 | 2003-04-01 | William P. Gardiner | Rotary internal combustion engine |
| US20140369878A1 (en) * | 2011-11-24 | 2014-12-18 | Calsonic Kansei Corporation | Gas compressor |
| US9751384B2 (en) * | 2011-11-24 | 2017-09-05 | Calsonic Kansei Corporation | Gas compressor with discharge section and sub-discharge section |
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