US3072319A - Machine for compressing fluids - Google Patents

Machine for compressing fluids Download PDF

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US3072319A
US3072319A US141559A US14155961A US3072319A US 3072319 A US3072319 A US 3072319A US 141559 A US141559 A US 141559A US 14155961 A US14155961 A US 14155961A US 3072319 A US3072319 A US 3072319A
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air
compressor
chamber
pipe
pressure
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US141559A
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Clarence E Cox
Richard L Nash
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Chicago Pneumatic Tool Co LLC
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Chicago Pneumatic Tool Co LLC
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C28/00Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00

Definitions

  • This application is directed to a machine for compressing iiuids.
  • a general object of this invention is to provide a practical and etiiciently operating machine for compressing iluids.
  • the machine of the present invention includes unloader control means which functions iirst .to slow down the rotating speed of the compressor when the pressure of air discharged from the-compressor exceeds a predetermined initial value, and which functions subsequently to further slow down the speed of the compressor and cut off intake air to the latter when the pressure of air discharged from the compressor rises to a predetermined higher value.
  • a further object of the invention is to provide an improved piston type unloading intake valve assembly for a rotary compressor.
  • a still further object of the invention is to provide practical means to scrub oil from the compressor chambers of a rotary compressor while the machine is running unloaded; and to prevent iiooding of the compression chambers of a rotary compressor with oil after the engine has stopped running.
  • a feature of the unloading intake valve assembly is a by-pass arrangement which facilitates opening of the valve by suction action of the compressor when the compressor starts up; which permits flow of a narrow stream of demand pressure air for re-circulation through the compressor system so as to scrub the latter of oil after intake air flow has been cut off and while the compressor is running unloaded; and which premits iiow of demand pressure air into the compressor system after the engine has stopped and the intake air low has been cut off, so as to counterbalance back pressure of air in the receiver acting upon an oil sump and as a consequence toV avoid oil flooding of the compressor.
  • FIG. 1 is a schematic illustration of the composite machine embodying the invention
  • FIG. 2 is a longitudinal sectional view of the rotary compressor unit of the machine of FIG. l;
  • FIGS. 3, 4 and 5 are vertical sectional views, respectively of the transformer, relay, and combined unloader and throttle control device.
  • FiG. 6 is an enlarged detail of the disc valve arrangement disclosed in FIG. 5.
  • FIGS. l and 2 wherein there is shown an engine 31 coupled to drive through clutch mechanism 82 a double stage air compressor 32 of the rotary vane type, the compressor comprising a low stage rotary compressor 62 drivingly coupled at 74 to a high pressure-stage rotary compressor 67.
  • the compressor comprising a low stage rotary compressor 62 drivingly coupled at 74 to a high pressure-stage rotary compressor 67.
  • air is drawn by suction of the low compressor stage 62 through an intake pipe 37 past an unloading valve assembly 127 and a screen 128 into the chamber 63 of lthe low compressor stage. Air compressed in the latter is passed through an interstage pipe connection 132 into the high compression chamber 63.
  • the compressed air is then discharged from a discharge end 134 of the high compression chamber 68 through a spring loaded one way check valve 139 of a discharge valve assembly 137 to piping 136 connected to a receiver tank 42.
  • the apparatus further includes an oil sump tank d3 disposed below and in communication with the receiver 42. Oil iows from the sump 43 under receiver pressure through pipe 292, a connected oil cleaner 41, and a pipe 295 to an oil cooler 39.
  • a relief valve 2945 is arranged to bypass oil around the oil cleaner i1 by way of a pipe 295 directly into pipe 293.
  • a pipe 296 conducts the oil from the cooler 39 to the inlet (not shown) of a gear pump 104 drivingly connected at 112 to the compressor drive.
  • the oil is forced by the pump into passages 114 and 117 from which it issues through restricted ports 124i and 123 in a iine spray into the compressor chambers 63 and 63 to cool the air in
  • the compressed air that is piped to the receiver 42 is accordingly charged with oil.
  • the compressed air flows from the receiver to a connected oil separator or demand supply tank t4 disposed directly above the receiver.
  • the operating speed of the compressor, and the iiow of air through the intake 37 to the compressor are controlled by a suitable unloading control system.
  • the latter in general, includes the unloading valve assembly 127, a transformer 52, a relay Si., and a combined throttle and unloading device 49.
  • a pipe 229 connects the separator 44- with a chamber 221 of the transformer 52 (FiG. 3).
  • Chamber 221 is eparated from an upper chamber 225 of the transformer by a diaphragm having aiiined to its upper face a valve 211 which is heid by a spring load 214 clear of an open end or valve seat 212 of chamber 225.
  • Air having a pressure not exceeding Se' p.s.i. flowing from the separator ifi over line 229 to chamber 221 is prevented from lmoving the diaphragm 269 to seat the valve 211 because of the greater resistance of the spring load 214.
  • the pressure air entering chamber 221 flows through a narrow passage 227 formed in the body 205 of the transformer to chamber 225.
  • the upper face of diaphragm 243 abuts a tail head 249 of a plunger pin 252.
  • the upper portion of the latter projects externally of the body 244.
  • a nut 259 threaded upon the upper end of pin 252 overlies a short tail end ot a pivotally supported throttle control lever S.
  • An opposite and considerably longer end 25827 is connected by throttle control linkage 261 to the compressor engine 31.
  • a heavy spring within the body 244 ot the device i9 loads the diaphragm 248 and pin 252 to a normal position wherein the nut 259 holds the throttle lever 253 pivoted in a clockwise operative position as in 5.
  • Means is provided to actuate the unloading valve assembly 127 to cut off ow of air from the intake pipe 37 to the compressor as the separator pressure rises above 85 p.s.i. to a selected value.
  • the unloading valve assembly 127 (FIG. 2) includes a closing cylinder 142 which is axed to and Within a housing 126, a piston 1413 slidably positioned in cylinder 142, a plunger or valve 144 having the rear end thereof allixed to the piston, a cylinder head 147 secured to the end of closing cylinder 1412, and an orifice plate 148 fastened to the end of the plunger 14K-l, all as best seen in FIG. 2.
  • the piston 143 is arranged to slide forwardly in the cylinder 142, and move the plunger 14d so that a forward end or" the latter having a leather disc 149 will close upon a valve seat 151 formed within the inta'ke valve assembly housing 126.
  • the piston 143 is provided with suitable piston rings 143e to provide a substantially Huid-tight seal between it and the wall of cylinder 1412.
  • a passage 151 is formed in the cylinder head 1417 to vent the underside of piston 143.
  • An oriiice 152 is provided in orilice plate 14S, while a bore 153 is formed in the plunger 14d.
  • Extending from the bore 1.53 is a passage 154 which is in alignment with a passage 156 formed in the pist-on 1li-3.
  • a chamber 157 is provided between the piston 143 and cylinder 142, the chamber being connected by a passage 153 to a vertically extending passage 159 formed in the cylinder 142.
  • Passage 159 connects with a horizontal passage or by-pass 161 formed in the cylinder 142, the passage 161 having a threaded opening 162 at one end with which is connected a pipe 201 leading from the relay device 51 (FIG. 4); the other end of passage 161 has a restricted orifice 163 opening into the intake housing 126 in the region above the intake screen of the low compression chamber 63.
  • Relay 51 has a chamber 21d in a body section 182. Connected with an upper area of this chamber is an end of a pipe 195 which is a branch od line 199 and communicates through the latter with the separator 411-. Connected with a lower area of chamber 211B is an ⁇ end of pipe 291.
  • a piston valve 194 slidable in chamber 21@ normally blocks ofi llow of air from pipe 195 through chamber' 21@ to pipe The piston valve is held in this normal condition by a spring load 196 supplemented by pressure of air communicated to the bottom end of the chamber 21u below the piston valve by a pipe line 295 which is connected with the discharge end 134y of the high compression chamber.
  • the upper end of the piston valve supports a piston rod 191 which projects with a slide tit through a xed bushing 192.
  • the projecting end of the piston rod abuts a diaphragm 187 which defines the lower wall of a chamber 263 formed at the upper end of the relay.
  • a collar 197 near the lower end ot rod 191 seats against the underside of bushing 192 so as to space the upper end of valve 19d a short distance below the bushing 192 and clear of the inlet of pipe 19E.
  • Chamber 293 is connected by means of a pipe 252 with an outlet 251 of an unloader section 2412 of the device i9 (FIG. 5).
  • the unloader section 242 (FlGS. 5 and 6) includes a body 263 in which is fitted a valve seat 26% having a bore 277 connected at a dead end thereof by radial ports 278 with an inlet port 279 with which pipe 199 is connected.
  • An opposite open end of bore 277 is normally closed by a slide disc Valve 269 which is guided in its movement relative to the Valve seat by a surrounding bushing 271.
  • a radial port 232 from the bushing Connects through the body 263 with the outlet 251.
  • a spring load 274 compressed between a conical valve holder 273 abutting the disc Valve 269 and a plunger 267 abutting an arm of a bellcrank 287, holds the disc valve seated over the open end of bore 277 of seat 268 against pressure of air in pipe 199, thus closing communication of pipe 199 from pipe 292.
  • Pipe 262 is normally vented through the bushing 271 and about the coned Valve holder 273 to a vent 286.
  • the bellcrank 287 is pivoted to a lixed member 257, and has an arm 237e pivoted at 288 to the external por tion of pin 252.
  • the pin 252 will be caused to rise further relative to the throttle arm 253 to cause the engine to turther slow down, and will cause the bellcrank 287 to pivot further counterclockwise to relax the spring load 274 suinciently s0 that pressure of separator air in line 199 will unseat the disc valve and ow through pipe line 292 to the relay chamber 293 (FIG. 4) to act upon the diaphragm 187.
  • This feature prevents rise in the pressure of air in the separator 42 during the time that no air is being drawn from an outlet manifold d6 of the latter.
  • the air under pressure in pipe 291 also passes at a restricted rate through passage 161 and orifice 1.63 into the intake end of the low compression chamber 63. This air is compressed as it passes through the low and high stage compression chambers and is discharged into the receiver 42.
  • the air passing through the perennial 163 is merely recirculated through the compressor system; it serves to scrub oil through the compressor passages. After the intake air has been cut oft", the machine continues to run unloaded, and at a reduced speed until a predetermined drop occurs in the separator pressure to cause the machine to reload.
  • Reloading occurs automatically as the pressure over pipe 231 acting on the underside of the diaphragm 248 of the device 49 relaxes, and the arm 258 and bellcrank 287 are progressively restored as the pin 252 returns to normal.
  • suction created by the compressor causes air to be vented from the chamber 157 at the rear of the piston 143 over the bypass 163 whereupon intake air in pipe 37 slides the valve 149 to open position and enters the compressor.
  • the control system above described also includes means to prevent flooding of the chambers of the compressor with oil in the event the machine should shut down due to an emergency or because of lack of fuel.
  • the possibility of flooding could arise while the machine is stopped.
  • back pressure of air in the receiver 42 acting on the oil in the sump 43 would tend to force the oil through the gear pump 104 and passages 114 and 123 back into the compressor chambers.
  • This flooding is avoided due to a pressure drop in the discharge end of the high compression chamber 134 above the discharge check valve 139, occurring when the engine stops. Since pipe 205 connects this end of the high pressure chamber with chamber 210 at the underside of piston 194 in the relay 51 (FIG. 4), a consequent drop of pressure of air acting on the piston 194 will occur.
  • an air compressor system including an air compression chamber, an air compressor rotor rotating in the latter, means charging the compression chamber with oil as the compressor rotor rotates, an inlet for admitting free air to the compression chamber, a receiver connected to the discharge end of the compression chamber, and closure means in the inlet responsive to a predetermined rise in receiver air pressure to close ori the free air ow through the inlet; means by-passing the closure means for conducting while the inlet is closed and the compressor is running unloaded a restricted intake flow of receiver pressure air into the compression chamber for scrubbing away oil in its path as it is recirculated by the rotating compressor to the receiver, wherein the means for charging the compression chamber with oil includes an oil sump which is subject to back pressure of air in the receiver when rotation of the compressor is stopped so as to reuX oil into the compression chamber; means responsive to stopping of the compressor to actuate the closure means to close the inlet and to cause a restricted ow of receiver pressure air over the by-pass means into the compression chamber for building up a pressure counteracting the

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Description

Jan. 8 19 53 c. E. cox ETAL 3,072,319
MACHINE FOR COMPRESSING FLUIDS Original. Filed Sept. 14, 1960 4 Sheets-Sheet 1 ATTDRN EY Jan. 8, 1963 c. E. cox ETAL MACHINE FOR COMPRESSING FLUIDS Original Filed Sept. 14, 1960 4 Sheets--Sheel'l 2 6r/lim l. M15/l ATTORNEY Jan. 8, 1963 c. E. cox ETAL A3,072,319
MACHINE FOR COMPRESSING FLUIDS Original Filed Sept. 14, 1960 4 Sheets-Sheet 5 @LJ/am ATTORNEFY Jam 8, 1963 c. E. cox ETAL i 3,072,319
MACHINE FOR COMPRESSING FLUIDS Original Filed Sept. 14, 1960 4 Sheets-Sheet 4 a maw/fw @United tates Patent t claim. (ci. 23o- 207) This application is a division of our pending application bearing Serial Number 55,959 filed September 14, 1960 for an Unloader Control for A Rotary Compressor, which in turn is a division of our original application 'bearing Serial Number 428,942, tiled May 11, 1954 for a Rotary Fluid Compressor. The said original application was abandoned after the tiling of the application mentioned above bearing Serial Number 55,959.
This application is directed to a machine for compressing iiuids.
A general object of this invention is to provide a practical and etiiciently operating machine for compressing iluids.
The machine of the present invention includes unloader control means which functions iirst .to slow down the rotating speed of the compressor when the pressure of air discharged from the-compressor exceeds a predetermined initial value, and which functions subsequently to further slow down the speed of the compressor and cut off intake air to the latter when the pressure of air discharged from the compressor rises to a predetermined higher value.
A further object of the invention is to provide an improved piston type unloading intake valve assembly for a rotary compressor.
A still further object of the invention is to provide practical means to scrub oil from the compressor chambers of a rotary compressor while the machine is running unloaded; and to prevent iiooding of the compression chambers of a rotary compressor with oil after the engine has stopped running.
A feature of the unloading intake valve assembly is a by-pass arrangement which facilitates opening of the valve by suction action of the compressor when the compressor starts up; which permits flow of a narrow stream of demand pressure air for re-circulation through the compressor system so as to scrub the latter of oil after intake air flow has been cut off and while the compressor is running unloaded; and which premits iiow of demand pressure air into the compressor system after the engine has stopped and the intake air low has been cut off, so as to counterbalance back pressure of air in the receiver acting upon an oil sump and as a consequence toV avoid oil flooding of the compressor.
The foregoing and other objects and features of the invention will appear more fully hereinafter from a consideration of the detailed description which follows, taken together with the accompanying drawings, wherein an embodiment of the invention is illustrated. it is to be eX- pressly understood, however, that the drawings are for purpose of illustration and description, and are not to be construed as defining the limits of the invention.
ln the drawings:
FIG. 1 is a schematic illustration of the composite machine embodying the invention;
FIG. 2 is a longitudinal sectional view of the rotary compressor unit of the machine of FIG. l;
FIGS. 3, 4 and 5 are vertical sectional views, respectively of the transformer, relay, and combined unloader and throttle control device; and
FiG. 6 is an enlarged detail of the disc valve arrangement disclosed in FIG. 5.
r process of compression.
hee
For a more detailed understanding of the invention reference is directed to the several iigures of the drawings, and now especially to FIGS. l and 2, wherein there is shown an engine 31 coupled to drive through clutch mechanism 82 a double stage air compressor 32 of the rotary vane type, the compressor comprising a low stage rotary compressor 62 drivingly coupled at 74 to a high pressure-stage rotary compressor 67. When the engine is running, air is drawn by suction of the low compressor stage 62 through an intake pipe 37 past an unloading valve assembly 127 and a screen 128 into the chamber 63 of lthe low compressor stage. Air compressed in the latter is passed through an interstage pipe connection 132 into the high compression chamber 63. The compressed air is then discharged from a discharge end 134 of the high compression chamber 68 through a spring loaded one way check valve 139 of a discharge valve assembly 137 to piping 136 connected to a receiver tank 42. The apparatus further includes an oil sump tank d3 disposed below and in communication with the receiver 42. Oil iows from the sump 43 under receiver pressure through pipe 292, a connected oil cleaner 41, and a pipe 295 to an oil cooler 39. A relief valve 2945 is arranged to bypass oil around the oil cleaner i1 by way of a pipe 295 directly into pipe 293. This by-pass arrangement assures flow of oil in the oil circulatory system in the event the oil cleaner i1 should fail, or become so clogged with dirt that oil could not iiow therethrough at the desired rate. A pipe 296 conducts the oil from the cooler 39 to the inlet (not shown) of a gear pump 104 drivingly connected at 112 to the compressor drive. The oil is forced by the pump into passages 114 and 117 from which it issues through restricted ports 124i and 123 in a iine spray into the compressor chambers 63 and 63 to cool the air in The compressed air that is piped to the receiver 42 is accordingly charged with oil. The compressed air flows from the receiver to a connected oil separator or demand supply tank t4 disposed directly above the receiver. Most of the oil settles out of the air in the receiver and dro-ps down into the sump. Residual oil separated from the air by the separator tank is returned from the latter over restricted piping 259 and a choke 291 to the interstage piping 132 where it is drawn by suction of the high compressor stage into the high compression chamber The operating speed of the compressor, and the iiow of air through the intake 37 to the compressor are controlled by a suitable unloading control system. The latter, in general, includes the unloading valve assembly 127, a transformer 52, a relay Si., and a combined throttle and unloading device 49.
A pipe 229 connects the separator 44- with a chamber 221 of the transformer 52 (FiG. 3). Chamber 221 is eparated from an upper chamber 225 of the transformer by a diaphragm having aiiined to its upper face a valve 211 which is heid by a spring load 214 clear of an open end or valve seat 212 of chamber 225. Air having a pressure not exceeding Se' p.s.i. flowing from the separator ifi over line 229 to chamber 221 is prevented from lmoving the diaphragm 269 to seat the valve 211 because of the greater resistance of the spring load 214. The pressure air entering chamber 221 flows through a narrow passage 227 formed in the body 205 of the transformer to chamber 225. Some of this air entering chamber 225 is vented to atmosphere through the open end 212 and a connected vent 234; and some of the air flows from chamber 225 over a line 231 to the underside of a diaphragm 248 forming the upper wall of a chamber 24851 in the body 244 of the device i9 (FIG. 5).
The upper face of diaphragm 243 abuts a tail head 249 of a plunger pin 252. The upper portion of the latter projects externally of the body 244. A nut 259 threaded upon the upper end of pin 252 overlies a short tail end ot a pivotally supported throttle control lever S. An opposite and considerably longer end 25827 is connected by throttle control linkage 261 to the compressor engine 31. A heavy spring within the body 244 ot the device i9 loads the diaphragm 248 and pin 252 to a normal position wherein the nut 259 holds the throttle lever 253 pivoted in a clockwise operative position as in 5. When the pressure of separator air flowing over line 229 to the chamber 221 of the transformer 52 rises above S5 p.s.i., it acts to move the diaphragm 29,9 against the load of spring 21d so as to close the valve 211 upon the seat 212, thus preventing venting of air from chamber 225 to vent 234. Whereupon, air pressure builds up in chamber 225, in line 231, and in chamber 248e at the underside of diaphragm of device di). The pressure increase in chamber 245e causes the diaphragm 249 to carry pin 252 upwardly, thus moving nut 259 away from the tail 255541 of the throttle lever, whereupon the latter pivots at its opposite end downward or counterclockwise (FlG. 5) to slow down the engine and the speed of the compressors; and, as a consequence, reduces the quantity of air being drawn into the compressors through the intake pipe 37.
Means is provided to actuate the unloading valve assembly 127 to cut off ow of air from the intake pipe 37 to the compressor as the separator pressure rises above 85 p.s.i. to a selected value.
The unloading valve assembly 127 (FIG. 2) includes a closing cylinder 142 which is axed to and Within a housing 126, a piston 1413 slidably positioned in cylinder 142, a plunger or valve 144 having the rear end thereof allixed to the piston, a cylinder head 147 secured to the end of closing cylinder 1412, and an orifice plate 148 fastened to the end of the plunger 14K-l, all as best seen in FIG. 2. The piston 143 is arranged to slide forwardly in the cylinder 142, and move the plunger 14d so that a forward end or" the latter having a leather disc 149 will close upon a valve seat 151 formed within the inta'ke valve assembly housing 126. Such action takes place during compressor unloading, as will later be described, and cuts oi ilow of air trom the intake pipe 37 to the compressor. The piston 143 is provided with suitable piston rings 143e to provide a substantially Huid-tight seal between it and the wall of cylinder 1412.
A passage 151 is formed in the cylinder head 1417 to vent the underside of piston 143. An oriiice 152 is provided in orilice plate 14S, while a bore 153 is formed in the plunger 14d. Extending from the bore 1.53 is a passage 154 which is in alignment with a passage 156 formed in the pist-on 1li-3. A chamber 157 is provided between the piston 143 and cylinder 142, the chamber being connected by a passage 153 to a vertically extending passage 159 formed in the cylinder 142. Passage 159 connects with a horizontal passage or by-pass 161 formed in the cylinder 142, the passage 161 having a threaded opening 162 at one end with which is connected a pipe 201 leading from the relay device 51 (FIG. 4); the other end of passage 161 has a restricted orifice 163 opening into the intake housing 126 in the region above the intake screen of the low compression chamber 63.
Relay 51 has a chamber 21d in a body section 182. Connected with an upper area of this chamber is an end of a pipe 195 which is a branch od line 199 and communicates through the latter with the separator 411-. Connected with a lower area of chamber 211B is an `end of pipe 291. A piston valve 194 slidable in chamber 21@ normally blocks ofi llow of air from pipe 195 through chamber' 21@ to pipe The piston valve is held in this normal condition by a spring load 196 supplemented by pressure of air communicated to the bottom end of the chamber 21u below the piston valve by a pipe line 295 which is connected with the discharge end 134y of the high compression chamber. The upper end of the piston valve supports a piston rod 191 which projects with a slide tit through a xed bushing 192. The projecting end of the piston rod abuts a diaphragm 187 which defines the lower wall of a chamber 263 formed at the upper end of the relay. A collar 197 near the lower end ot rod 191 seats against the underside of bushing 192 so as to space the upper end of valve 19d a short distance below the bushing 192 and clear of the inlet of pipe 19E. Chamber 293 is connected by means of a pipe 252 with an outlet 251 of an unloader section 2412 of the device i9 (FIG. 5).
The unloader section 242 (FlGS. 5 and 6) includes a body 263 in which is fitted a valve seat 26% having a bore 277 connected at a dead end thereof by radial ports 278 with an inlet port 279 with which pipe 199 is connected. An opposite open end of bore 277 is normally closed by a slide disc Valve 269 which is guided in its movement relative to the Valve seat by a surrounding bushing 271. A radial port 232 from the bushing Connects through the body 263 with the outlet 251. A spring load 274, compressed between a conical valve holder 273 abutting the disc Valve 269 and a plunger 267 abutting an arm of a bellcrank 287, holds the disc valve seated over the open end of bore 277 of seat 268 against pressure of air in pipe 199, thus closing communication of pipe 199 from pipe 292. Pipe 262 is normally vented through the bushing 271 and about the coned Valve holder 273 to a vent 286. The bellcrank 287 is pivoted to a lixed member 257, and has an arm 237e pivoted at 288 to the external por tion of pin 252.
In the operation of the apparatus, when air pressure in the separator 44 rises above 85 psi., pressure air, as explained earlier herein, flowing from the transformer 52 (FIG. 3) over line 231 to the device 49 acts upon the diaphragm 24S to elevate the pin 252 against the load of spring 254 to actuate lever 258 to throttle and slow down the engine. In this action the bellcrank 287 will be pivoted by pin 252 counterclockwise relative to the plunger 267 causing relaxation of spring 27d. But as long as the separator pressure in pipe 199 does not exceed a predeter- -mined value above p.s.i. the spring load 274 will not be relaxed suliciently to allow the disc valve 269 to move to open condition from seat 268. However, when the separator air pressure does exceed a predetermined value above 85 psi., the pin 252 will be caused to rise further relative to the throttle arm 253 to cause the engine to turther slow down, and will cause the bellcrank 287 to pivot further counterclockwise to relax the spring load 274 suinciently s0 that pressure of separator air in line 199 will unseat the disc valve and ow through pipe line 292 to the relay chamber 293 (FIG. 4) to act upon the diaphragm 187. This pressure on the diaphragm 187 aided by relaxa` tion of pressure in pipe line 2115 due to slowing down of the engine and relaxing of compressor pressure in the discharge end 134 of the compressor chamber above the check valve 141, causes the piston valve 194 to drop so that pipe line 198 communicates through chamber 210 with pipe 291.
Following the latter action, pressure air flows through pipe 201 to the unloading valve assembly 127 and passes through ports 162, 159 and 153 to chamber 157 to torce valve 149 to closed condition on valve seat 151 so that intake air through pipe 37 is cut off. The compressor thereupon runs unloaded at a reduced speed, with the result that no further compressor air is delivered to the receiver 42. Any air that may leak into the compressor past the intake valve 149 is compensated for by a small amount of air which is blown back into the intake pipe 37 under pressure of air in pipe 201 from chamber 157, passages 156, 151i, 153, and orifice 152. This feature prevents rise in the pressure of air in the separator 42 during the time that no air is being drawn from an outlet manifold d6 of the latter. The air under pressure in pipe 291 also passes at a restricted rate through passage 161 and orifice 1.63 into the intake end of the low compression chamber 63. This air is compressed as it passes through the low and high stage compression chambers and is discharged into the receiver 42. The air passing through the orice 163 is merely recirculated through the compressor system; it serves to scrub oil through the compressor passages. After the intake air has been cut oft", the machine continues to run unloaded, and at a reduced speed until a predetermined drop occurs in the separator pressure to cause the machine to reload.
Reloading occurs automatically as the pressure over pipe 231 acting on the underside of the diaphragm 248 of the device 49 relaxes, and the arm 258 and bellcrank 287 are progressively restored as the pin 252 returns to normal. As the engine speed again increases, suction created by the compressor causes air to be vented from the chamber 157 at the rear of the piston 143 over the bypass 163 whereupon intake air in pipe 37 slides the valve 149 to open position and enters the compressor.
The control system above described also includes means to prevent flooding of the chambers of the compressor with oil in the event the machine should shut down due to an emergency or because of lack of fuel. The possibility of flooding could arise while the machine is stopped. In this event, back pressure of air in the receiver 42 acting on the oil in the sump 43 would tend to force the oil through the gear pump 104 and passages 114 and 123 back into the compressor chambers. This flooding is avoided due to a pressure drop in the discharge end of the high compression chamber 134 above the discharge check valve 139, occurring when the engine stops. Since pipe 205 connects this end of the high pressure chamber with chamber 210 at the underside of piston 194 in the relay 51 (FIG. 4), a consequent drop of pressure of air acting on the piston 194 will occur. Whereupon7 the greater pressure of separator air from pipe 198 acting in chamber 210 on the top side of piston 194 will cause the latter to drop and thus put pipe 198 in communication with pipe 261. Pressure air will then flow over pipe 201 and orifice 163 of the valve assembly 127 into the compressor charnbers where it will build up and counterbalance the back pressure of air from the receiver 42 acting on the oil 40 parts without departing from the spirit and scope of the invention, and it is intended, therefore, to claim the invention not only as shown and described but also in all such forms and modifications thereof as may be construed to fall within the spirit of the invention and the scope of the appended claim.
Subject matter disclosed in this specification and drawings but not claimed herein is described and claimed in our co-pending applications as follows: Serial No. 55,959, tiled September 14, 1960 for Unloader Control for a Rotary Compressor; and Serial No. 60,748 led October 5, 1960 for a Rotary Fluid Compressor.
What is claimed is:
In an air compressor system including an air compression chamber, an air compressor rotor rotating in the latter, means charging the compression chamber with oil as the compressor rotor rotates, an inlet for admitting free air to the compression chamber, a receiver connected to the discharge end of the compression chamber, and closure means in the inlet responsive to a predetermined rise in receiver air pressure to close ori the free air ow through the inlet; means by-passing the closure means for conducting while the inlet is closed and the compressor is running unloaded a restricted intake flow of receiver pressure air into the compression chamber for scrubbing away oil in its path as it is recirculated by the rotating compressor to the receiver, wherein the means for charging the compression chamber with oil includes an oil sump which is subject to back pressure of air in the receiver when rotation of the compressor is stopped so as to reuX oil into the compression chamber; means responsive to stopping of the compressor to actuate the closure means to close the inlet and to cause a restricted ow of receiver pressure air over the by-pass means into the compression chamber for building up a pressure counteracting the back pressure of the receiver upon the oil sump.
References Cited in the iile of this patent UNITED STATES PATENTS Great Britain Apr. 11, 1951
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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3186630A (en) * 1963-09-05 1965-06-01 Jaeger Machine Co Rotary compressor
US3689197A (en) * 1969-07-17 1972-09-05 Atlas Copco Ab Control device for a motor-compressor
US4086041A (en) * 1975-08-05 1978-04-25 Diesel Kiki Co., Ltd. Rotary compressor comprising improved rotor lubrication system
US4401413A (en) * 1981-06-08 1983-08-30 Dickens Willie G Air compressor switch device
EP0130662A2 (en) * 1983-04-08 1985-01-09 Cash Engineering Co. Pty. Limited Compressor control system
US4998862A (en) * 1989-10-02 1991-03-12 Ingersoll-Rand Company Air compressor pressure regulating valve system

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB686951A (en) * 1950-09-06 1953-02-04 Ingersoll Rand Co Improvements in rotary fluid compressors
US2641405A (en) * 1948-04-14 1953-06-09 Ingersoll Rand Co Fluid compressor unit
US2661893A (en) * 1950-08-10 1953-12-08 Ingersoll Rand Co Control device for fluid compressors

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641405A (en) * 1948-04-14 1953-06-09 Ingersoll Rand Co Fluid compressor unit
US2661893A (en) * 1950-08-10 1953-12-08 Ingersoll Rand Co Control device for fluid compressors
GB686951A (en) * 1950-09-06 1953-02-04 Ingersoll Rand Co Improvements in rotary fluid compressors

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3186630A (en) * 1963-09-05 1965-06-01 Jaeger Machine Co Rotary compressor
US3689197A (en) * 1969-07-17 1972-09-05 Atlas Copco Ab Control device for a motor-compressor
US4086041A (en) * 1975-08-05 1978-04-25 Diesel Kiki Co., Ltd. Rotary compressor comprising improved rotor lubrication system
US4401413A (en) * 1981-06-08 1983-08-30 Dickens Willie G Air compressor switch device
EP0130662A2 (en) * 1983-04-08 1985-01-09 Cash Engineering Co. Pty. Limited Compressor control system
EP0130662A3 (en) * 1983-04-08 1985-02-06 Cash Engineering Co. Pty. Limited Compressor control system
US4549856A (en) * 1983-04-08 1985-10-29 Cash Engineering Co. Pty. Ltd. Compressor control system
US4998862A (en) * 1989-10-02 1991-03-12 Ingersoll-Rand Company Air compressor pressure regulating valve system

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