US3813191A - Rotary vane device for compressor, motor or engine - Google Patents
- ️Tue May 28 1974
US3813191A - Rotary vane device for compressor, motor or engine - Google Patents
Rotary vane device for compressor, motor or engine Download PDFInfo
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Publication number
- US3813191A US3813191A US00350632A US35063273A US3813191A US 3813191 A US3813191 A US 3813191A US 00350632 A US00350632 A US 00350632A US 35063273 A US35063273 A US 35063273A US 3813191 A US3813191 A US 3813191A Authority
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- United States Prior art keywords
- vane
- working space
- port means
- vanes
- hub Prior art date
- 1972-05-01 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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- 239000012530 fluid Substances 0.000 claims abstract description 11
- 239000007789 gas Substances 0.000 claims description 84
- 230000005484 gravity Effects 0.000 claims description 6
- 230000002000 scavenging effect Effects 0.000 claims description 6
- 238000001816 cooling Methods 0.000 description 4
- 239000000446 fuel Substances 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000010687 lubricating oil Substances 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 241000282326 Felis catus Species 0.000 description 1
- 229910000639 Spring steel Inorganic materials 0.000 description 1
- 241001255830 Thema Species 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Images
Classifications
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- 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
- F01C17/00—Arrangements for drive of co-operating members, e.g. for rotary piston and casing
- F01C17/02—Arrangements for drive of co-operating members, e.g. for rotary piston and casing of toothed-gearing type
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- 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
- F01C1/00—Rotary-piston machines or engines
- F01C1/30—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
- F01C1/34—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 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 F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
- F01C1/344—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 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 F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
- F01C1/352—Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 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 F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member the vanes being pivoted on the axis of the outer member
Definitions
- ABSTRACT An integral vane compressor and vane motor. At least three vanes are pinned to a central hub and extend through respective slots in a generally cylindrical drum with its axis parallel to and displaced radially from that of said hub, the slots guiding the radial position of the vanes. Synchronizing means, such as a gear train, cause the hub and drum to rotate in the same direction and at the same speed, with the vanes reciprocating and oscillating in the guide slots.
- a housing encloses the vanes and cooperates with them and the drum to provide a series of working spaces, one for each vane to compress or expand a fluid. lntakeand exhaust ports lead fluid into and from the working spaces.
- This invention relates to an integral vane compressor and vane motor.
- a feature of the rotary vane device of this invention is that the vanes are pinned to a central hub-shaft, and it has a separate circular drum to help transmit torque through the vanes and to guide the radial direction of the vanes.
- The'vanes are pinned at their centers of gravity to the central hub-shaft, so that they can oscillate back and forth as the central hub-shaft rotates; as a result, the mechanism is kept in dynamicbalance.
- the central hub shaft supports the full centrifugal pull of the vanes; consequently, they have no friction drag at their tips where they nearly. (but not quite) touch the housing.
- the central hub-shaft and the'circular drum both rotate at the samespeed and in the same direction, but the center of rotation of the circular drum is offset from the center of rotation of the central hub-shaft.
- the radius of the circular drum is smaller than the radial distance from the hub center to the tips of the extended vanes in every position of their rotation.
- the circular drum preferably has equally spaced axial slots at its outer periphery, one for each vane; these axial slots are preferably just big enough so that the vanes are forced to oscillate andreciprocate in themas the drum and shaft rotate. As the shaft and drum rotate and the vanes are forced to rotate and oscillate, their tipsform a circumscribed surface.
- the housing of my new rotaryvanedevice is slightly larger than the circumscribed surface of the vanes; thus there is no friction betweenthe vanes and the housing.
- the housing may be provided with an intake port and an exhaust port.
- the space bounded between two adjacent vanes, the cylindrical surface of the drum between these vanes, and the cylindrical and disc surfaces of the housing constitutes the working space.
- the intake port is closed by a rotary vane just after the working space is largest; as the vanes and drum rotate, decreasing the volume of the working space, they give an isentropic compression of the trapped gases.
- the compressed gases are then forced out of the workingspace through a discharge port located where the working space is smallest.
- the integral vane compressor and vane motor have a compressor intake port for low pressure gases, a compressor discharge port for high-pressure gases. :1 motor intake port for hot high-pressure gases and a motor exhaust port for exhaust gases.
- the compressor intake port and the motor exhaust port may connect to the same working space.
- a blower may be used to force a fresh charge into the intake port.
- a jet pump action of the exhaust gases flowing out and the fresh charge flowing in may exhaust, charge, and scavenge the common working space for the intake and exhaust ports.
- This integral vane compressor and vane motor may be used similar to a turbocharger.
- the vane motor may be used similar to a gas turbine, wherein the compressor and motor use the same wheel;
- the working spaces for the vane motor may expand to a larger volume than the intake volume for they vane compressor; thus the device will generate shaft power similar to a gas turbine.
- the working spaces for the vane motor may expand to a volume equal to or only slightly larger than the intake volume for the compressor; in this case the vane device acts like a turbo-charger ora gas turbine gas generator which may supply gases to a free-running gas turbine.
- FIG. 3 is a view in section taken along the line 3-3 in FIG. 2, showing the end view of the gears.
- FIG. 4 is a fragmentary view in section of a modified form of the device that may be used as a compressor or a motor,.depending on whether the hub-shaft and the drum rotate clockwise, when it acts as a compressor, or counterclockwise, when it acts as a motor or steam engme..
- FIG. 5 is an end view in section of the engine of FIG. 4 showing the adjustable sliding circular valve for regulating the cutoff point for steam or compressed gas expan'sion in the vane motor.
- FIG. 6 is a fragmentary detail view of a portion of the motor, showing a spring seal ring to contain the lubrieating oil inside the'drum.
- FIG. 7 is a fragmentary enlarged view, partly diagrammatic, of the gear box with part of the hub shaft broken away to show parts otherwise obscured.
- FIG. 8 is a diagram relative to the geometry of the vanes, hub, and drum as they rotate.
- FIG. 9 is a block flow diagram showing how the rotary vane device maybe used as an integral vane compressor and vane motor.
- the vane engine 10 of FIGS. I to 3 comprises a gen- 3 erally cylindrical housing 11.
- a hub-shaft 12 rotates about a center line 13, having its bearings on or supported by the housing 11 (FIG. 2).
- the hub-shaft 12 has eight equally spaced piano hinges 21, 22, 23, 24, 25, 26, 27, 28, (which may be pinned at the ends only or as shown) and eight vanes 31, 32, 33, 34, 35, 36, 37, and 38 are pinned at their center of gravity to respective piano hinge points 21, 22, 23, 24, 25, 26, 27, and 28 by means of shafts 41, 42, 43, 44, 45, 46, 47, and 48.
- Each of the vanes 31, 32, 33, 34, 35, 36, 37, 38 may have a counter mass 51, 52, 53, 54, 55, 56, 57, 58, so that as the vanes oscillate about their respective shafts 41, 42, 43, 44, 45, 46, 47, 48, the hubshaft 12 remains in dynamic balance as it rotates.
- eight vanes are shown in FIG. 1, any number of equally spaced vanes greater than three may be used.
- a drum 14 rotates about a center line 15 which is displaced from the hub center line 13 by the distance y.
- the drum 14 has its bearing on the housing 11.
- the drum 14 and the hub-shaft 12 are synchronized to rotate in the same direction and at the same rotating speed.
- the drum 14 has slots 61, 62, 63, 64, 65, 66, 67, 68 at its outer diameter, and these slots are just large enough for the corresponding vanes 31, 32, 33, 34, 35, 36, 37, 38 to slide and oscillate in as the hub-shaft 12 and the drum 14 rotate.
- the drum 14 may have discs 16 and 17 (FIG. 2) at its ends for supporting the gusseted arc sections 71, 72, 73, 74, 75, 76, 77, 78.
- the discs 16 and 17 also support the bearings 18 and 19 for the drum 14 on the housing 11.
- the disc 16 may also be provided with an internal gear 80 (FIG. 3).
- the mechanism for synchronizing the hub-shaft 12 and the drum 14 may comprise the internal gear 80 and a meshing spur gear 81, which is keyed to a shaft 82 that has its bearings on the housing 11. Also keyed to shaft 82 is a second spur gear 83.
- the spur gear 83 may be meshed with a pinion gear 84, which is also meshed to a third spur gear 85, or, as shown in FIG. 7, the gear 84 is keyed to a shaft 84a that also carries a gear 84b meshed to the gear 85.
- the spur gear 85 is keyed to the hub-shaft 12.
- the pinion gear 84 has its shaft bearings on the housing 11. The pitch diameter and teeth of the gears 80, 81, 83, 84, and 85 are prescribed so that the hub-shaft 12 and the drum 14 are synchronized to rotate in the same direction and at the same rotating speed.
- the gears have the following pitch diameters:
- the housing 11 may be provided with cooling fins 86.
- the housing 11 may be provided with an intake scavenging and exhaust port 87.
- a fan 88 which is keyed to the hub-shaft 12, may be used to blow a fresh charge of air through the open port 87 to help scavenge the expanded gases out of the exhaust, to cool the vanes 31, 32, 33, 34, 35, 36, 37, and 38 and to cool the outer surface of each drum beam section 71, 72, 73, 74, 75, 76, 77, 78 when it is at the port 87. Also.
- the fan air flows past the cooling fins 86 to cool the engine housing 11 and blows air through the cooling passages 79 between the gussets and the arcuate segments in the beam elements 71, 72, 73, 74, 75, 76, 77, and 78.
- the hub-shaft 12 rotates clockwise, and when, for example, the vane 36 moves past the position 89 of the housing 11, a fresh charge is trapped in a working space 96 bounded by the adjacent vanes 36 and 37, the outer surface of the beam element 76, and the inner surface of the housing 11 between the tips of the vanes 36, 37 and side disc section of the housing 2.
- Each of the adjacent vanes 31, 32, 33, 34, 35, 36, 37, 38 has a working space 91, 92, 93, 94, 95, 96, 97, 98.
- a fuel injector 99 may inject fuel into each working space 91, 92, 93, 94, 95, 96, 97, 98, in turn as it moves past it.
- FIGS. 4 and 5 the rotary vane compressor or motor has most of the same parts as the engine 10 and are given the same reference numerals. The basic differences are that the fuel injector 99 and the spark ignition system 100 are eliminated, and in place of the common exhaust, scavenging, and intake port 87 shown for the engine 10, the housing 111 of the compressor or motor 110 has an intake port 112 separate from the discharge port 113, and these ports 112 and 113 are located diametrically opposite each other.
- vanes 31, 32, 33, 34, 35, 36, and 37 are practically inside the drum 114, when its respective working space 191, 192, 193, 194, 195, 196, 197, 198 is at its minimum volume, which is equal to the working tolerances between the housing 111 and the drum 114 multiplied by the vane width.
- the intake port 112 When operating as a vane compressor 110, the intake port 112 is closed as the vane 31, 32, etc., is forced past the edge 115 of the port 112 by means of clockwise rotation of hub-shaft 12 and the drum 114.
- the working space 191,192, etc. may be close to its largest volume just after the vane 31, 32, etc., closes the intake port 1 5 112 at the station 115.
- the working space 191, 192, etc. is reduced, and the trapped gases are compressed approximately adiabatically until the vanes 31, 32, etc., move past the station 116 in the housing 111 to open the space 191, 192, etc., to the discharge port 113.
- the compressed gases are preferably forced out of the space 191, 192, etc., through the discharge port 113 into a compressed gas accumulator (not shown).
- a compressed gas accumulator not shown.
- the vanes 31, 32, etc. rotate past a station 117, a small volume of compressed gas is trapped in the space 191, 192, etc., this trapped compressed gas expands approximately isentropically and does work on the vanes 31, 32, etc., as the space 191, 192, etc., increases.
- the vanes 31, 32, etc. pass a station 118, the compressed gas in the space 191, 192, etc., is substantially equal to the pressure of the gas in the intake port 112.
- the volume of space 191, 192, etc., as the vane 31, 32, etc., moves past the station 117 should be kept to a minimum.
- the motor turns in a counterclockwise direction.
- Compressed gas or steam, etc. flows from the accumulator, not shown, through the port 113, which is now the intake port, into the working space 191, 192, etc.
- the compressed gases are trapped in the working space 191, 192, etc.
- the working space 191, 192, etc. increases in volume and the compressed gases expand approximately isentropically'to do work on the vanes 31, 32, etc., until they move past the station 115 to open port 112, which is now the exhaust port.
- the pressure in theworking spaces 191, 192, etc. is substantially the same as the gases in the exhaust port 112, except when the cutoff point is increased.
- gases are trapped in the space 191, 192, etc.; this trapped gas is approximately isentropically compressed back to the pressure in the accumulator as the working space 191, 192, etc., is reduced.
- the mass of gas which is compressed back to theaccumulator pressure is designed .to be a minimum.
- an arcuate cutoff valve 120 (FIG. 5) may be turned counterclockwise to give the desired cutoff volume 191, 192, etc.
- an arcuate valve 121 may be turned counterclockwise. The compressed gases flow axially from a chamber 122 through the arc ports into the working spaces 191, 192, etc.
- leaf spring scrapers 130 may be used to scrape the oil of the vanes 31, 32, etc., and keep it inside the drum 14 for lubricating the pivot shafts 41, 42, 43, 44, 45, 46, 47, 48, thebearings for the hub-shaft 12 and the bearings 18 and 19 for the drum-l4.
- scrapers 130 may be secured to each bridge section 71, i
- the beam section 14 has an arcuate surface for the spring 130 to follow as it flexes; so it will have fatigue stresses which are below the endurance limit of the spring steel 130.
- the leaf spring scrapes the excess lubricating oil of the vanes 31, 32, etc., so it will be contained inside the drum 14; just sufficient oil is left on the vane 31, 32, etc., to lubricate the rubbing surface between the vanes 31, 32, etc., and the slots 61, 62, etc.
- seal bars 200 may be provided in axial slots 201 in the ends of the beam arcs 71, etc., that bear on the vanes 31 to 38.
- Metal springs 202 or other fluidpressure means may be used to keep the seal bars 200 tight against the vanes, and the bars 200 fit snugly in the axial slots 201, thus a minimum flow of compressed gas passes from the working space 91-98 into the drum 14.
- vanes 32, 33, 34, 35, 36, 37, 38 undergo the same cycle asthe vane 31. If there are n vanes, they may be placed 21r/n radians apart, so that there will be equal working spaces between vanes.
- the surface which the vane tips circumscribe as they rotate and oscillate about the hub shaft can be derived mathematically; they can be written in polar coordinates with the origin at the centerline of the hub-shaft 12.
- the only variable is the angle 0.
- the angle 0 is zero when a radial line drawn from the centerline of the drum first passes through the centerline of the hub shaft then through the pivot point of the vane and through the centerline of the vane.
- the vane is in its straight line extended position at 0 and P r 1 which is at its largest radius.
- the variable parameters are:
- chord segment distance a for the vane contact at radius R to the vane pivot point at a (R-r) sin 6 The minimum distance I) from the vane pivot point to the chord. a line normal to the chord:
- the cosine law is used to get the radius of curvature P, of the surface circumscribed by the vane with respect to the star shaft centerline.
- FIG. 9 An integral vane compressor and vane motor 30 is shown in FIG. 9. It has a compressor intake port3ll, a compressor exhaust port 312, a motor intake po 313', and a motor exhaust port 314.
- the compressor intake port 311 to each working space is. closed by a'vane after that working space achieves its largest volume,v low pressure gas being compressed in that working space as it is made smaller.
- the compressed gas after it has been compressed to a desired pressure level, is discharged through the compressor exhaust 312, the compressor exhaust port 312 being passed by the vane just before the working space achieves its smallest volume.
- the vane then opens the working space to high pressure gas flowing into the motor intake port 313 just after the working space passes its smallest volume.
- the motor intake port 313 remains open until the space between the vanes is at a prescribed value, then the next vane moving to close the working space off from the intake port 3l3 traps compressed gas in the working space.
- the working space increases in volume,'and the compressed gas expands to do work on the vanes and members rotatingtherwith until the working space is near its largest volume; I then the working space is opened by a vane to the motor exhaust port 314, so that the expanded gases are exhausted.
- An integral vane-compressor and vane motor having compressor intake port means and :exhaust port means and motor intake port means and exhaust port means, comprising:
- synchronizing means mechanically linking said hub and said drum so that they rotate in the same direction and at the same rotating speed. so that said vanes reciprocate and oscillate in said guide slots as the hub and drum rotate,
- a housing enclosing said vanes and cooperating with said vanes and said drum to provide a series of working spaces, one for each said vane to compress or expand afluid, and
- said compressor intake port means to each working space being closed by a said vane after that working space achieves its largest volume, low pressure gas being compressed in said workingispace as it is made smaller, the compressed gas, after it has been compressed to a desired pressure level, being discharged through said compressor exhaust port means,
- said compressor exhaust port means being passed by said vane just before 'said working space achieves its smallest volume
- said vane then opening said working space to high pressure gas flowing into said motor intake port means just after said working space passes its smallest volume, said motor intake port means remaining open until the space between said vanes is at a prescribed value, then the next said vane moving to close said working space off from said intake port means and to trap compressed gas in said working space,
- said working space increasing in volume and said compressed gas expanding to do work on the vanes and members rotating therewith until said working space is near its largest volume
- An integral vane compressor and vane motor having compressor intake port means and exhaust port means and motor intake port means and exhaust port means, comprising? a rotating central hub having a series of vane pivot points spaced therearound at equal radii from the center of the hub,
- synchronizing means mechanically linking said hub and said drum so that they rotate in the same direction and at the same rotating speed, so that said vanes reciprocate and oscillate in said guide slots as the hub and drum rotate,
- a housing enclosing said vanes and cooperating with said vanes and said drum to provide a series of working spaces, one for each said vane to compress or expand a fluid
- intake and exhaust port means for leading fluid into and from said working spaces.
- said compressor intake port means to each working space being closed by a said vane after that working space achieves its largest volume, low pressure gas being compressed in said working space as it is made smaller, the compressed gas, after it has been compressed to a desired pressure level, being discharged through said compressor exhaust port means,
- said compressor exhaust port means being passed by said vane just before said working space achieves its smallest volume
- said vane then opening said working space to high pressure gas flowing into said motor intake port means just after said working space passes its smallest volume, said motor intake port means remaining open until the space between said vanes is at a prescribed value, then the next said vane moving to close said working space off from said intake port means and to trap compressed gas in said working space,
- said working space increasing in volume and said compressed gas expanding to do work on the vanes and members rotating therewith until said working space is near its largest volume
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Abstract
An integral vane compressor and vane motor. At least three vanes are pinned to a central hub and extend through respective slots in a generally cylindrical drum with its axis parallel to and displaced radially from that of said hub, the slots guiding the radial position of the vanes. Synchronizing means, such as a gear train, cause the hub and drum to rotate in the same direction and at the same speed, with the vanes reciprocating and oscillating in the guide slots. A housing encloses the vanes and cooperates with them and the drum to provide a series of working spaces, one for each vane to compress or expand a fluid. Intake and exhaust ports lead fluid into and from the working spaces.
Description
United StatessPatent 1 1 n] 3,813,191 Foster i 1 May 28,1974
1 1 ROTARY VANE DEVICE FOR COMPRESSOR, MOTOR OR ENGINE Berry W. Foster, 2415 Thomas Ave., Redondo Beach, Calif. 90278 Filed: Apr. 12, 1973 Appl.- No.: 350,632
Related US. Application Data Continuation-impart of Ser. No. 268,866, May 1, 1972, Pat. No. 3,747,573, which is a continuation of Ser. No. 41.008, May 22, 1970.
Inventor:
References Cited UNlTED STATES PATENTS 9/1912 Carroll 417/348 3/1919 417/348 8/1972 417/406 7/1973 Foster 418/137 COMPRESSOR DISCHARGE FOR HIGH PRESSURE COMPRESSOR lNTAKE FOR, LOW -PRESSURE GASES Primary Examiner-C. .1. Husar Attorney, Agent, or Firm-Owen, Wickersham &
Erickson [57] ABSTRACT An integral vane compressor and vane motor. At least three vanes are pinned to a central hub and extend through respective slots in a generally cylindrical drum with its axis parallel to and displaced radially from that of said hub, the slots guiding the radial position of the vanes. Synchronizing means, such as a gear train, cause the hub and drum to rotate in the same direction and at the same speed, with the vanes reciprocating and oscillating in the guide slots. A housing encloses the vanes and cooperates with them and the drum to provide a series of working spaces, one for each vane to compress or expand a fluid. lntakeand exhaust ports lead fluid into and from the working spaces.
2 Claims, 9 Drawing Figures Moron INTAKE FOR HOT HIGH PRESSURE GASES \MOTOR EXHAUST FOR GASES PATENTEUMY 2 w 3.8 13191 sum 1 (IF. 7
PATENTEDmzs 1911 3.813.191 SHEET '4 0f 7 FIG. 5
PMENTEMHB I914 38131191 SHEEI 7 0F 7 COMPRESSOR DISCHARGE MOTOR INTAKE FOR FOR HIGH -PRESSURE HOT HIGH PRESSURE OASES\ GASES l 4313 COMPRESSOR INTAKE \MOTOR EXHAUST EOR EOR LOW-PRESSURE I OASES OASES ROTARY VANE DEVICE FOR COMPRESSOR, MOTOR ENGINE No. 3,747,573 which was a continuation of application Ser. No. 41,008 filed May 22, I970.
BACKGROUND AND SUMMARY OF THE INVENTION This invention relates to an integral vane compressor and vane motor.
A feature of the rotary vane device of this invention is that the vanes are pinned to a central hub-shaft, and it has a separate circular drum to help transmit torque through the vanes and to guide the radial direction of the vanes. The'vanes are pinned at their centers of gravity to the central hub-shaft, so that they can oscillate back and forth as the central hub-shaft rotates; as a result, the mechanism is kept in dynamicbalance. The central hub shaftsupports the full centrifugal pull of the vanes; consequently, they have no friction drag at their tips where they nearly. (but not quite) touch the housing. y
The central hub-shaft and the'circular drum both rotate at the samespeed and in the same direction, but the center of rotation of the circular drum is offset from the center of rotation of the central hub-shaft.-The radius of the circular drum is smaller than the radial distance from the hub center to the tips of the extended vanes in every position of their rotation. The circular drum preferably has equally spaced axial slots at its outer periphery, one for each vane; these axial slots are preferably just big enough so that the vanes are forced to oscillate andreciprocate in themas the drum and shaft rotate. As the shaft and drum rotate and the vanes are forced to rotate and oscillate, their tipsform a circumscribed surface.
The housing of my new rotaryvanedevice is slightly larger than the circumscribed surface of the vanes; thus there is no friction betweenthe vanes and the housing. The housing may be provided with an intake port and an exhaust port. The space bounded between two adjacent vanes, the cylindrical surface of the drum between these vanes, and the cylindrical and disc surfaces of the housing constitutes the working space. There may be three or more working spaces in each device, and the volume of each working space varies as the drum and the hub-shaft rotate in the stationary housing. For example, the maximum volume of this working space is l80 out of phase with its minimum volume. I
In the compressor portion, the intake port is closed by a rotary vane just after the working space is largest; as the vanes and drum rotate, decreasing the volume of the working space, they give an isentropic compression of the trapped gases. The compressed gases are then forced out of the workingspace through a discharge port located where the working space is smallest.
In the motor portion, used to expand compressed pressed gas and expand it until the working space is at its largest volume;then the exhaust port opens to exhaust low pressure gases asthe working space becomes smaller.
The integral vane compressor and vane motor have a compressor intake port for low pressure gases, a compressor discharge port for high-pressure gases. :1 motor intake port for hot high-pressure gases and a motor exhaust port for exhaust gases. The compressor intake port and the motor exhaust port may connect to the same working space. A blower may be used to force a fresh charge into the intake port. A jet pump action of the exhaust gases flowing out and the fresh charge flowing in may exhaust, charge, and scavenge the common working space for the intake and exhaust ports. This integral vane compressor and vane motor may be used similar to a turbocharger. Also, it may be used similar to a gas turbine, wherein the compressor and motor use the same wheel; The working spaces for the vane motor may expand to a larger volume than the intake volume for they vane compressor; thus the device will generate shaft power similar to a gas turbine. As an alternate design the working spaces for the vane motor may expand to a volume equal to or only slightly larger than the intake volume for the compressor; in this case the vane device acts like a turbo-charger ora gas turbine gas generator which may supply gases to a free-running gas turbine.
' BRIEF DESCRIPTION OF THE DRAWINGS FIG. 3 is a view in section taken along the line 3-3 in FIG. 2, showing the end view of the gears.
FIG. 4 is a fragmentary view in section of a modified form of the device that may be used as a compressor or a motor,.depending on whether the hub-shaft and the drum rotate clockwise, when it acts as a compressor, or counterclockwise, when it acts as a motor or steam engme..
FIG. 5 is an end view in section of the engine of FIG. 4 showing the adjustable sliding circular valve for regulating the cutoff point for steam or compressed gas expan'sion in the vane motor.
FIG. 6 is a fragmentary detail view of a portion of the motor, showing a spring seal ring to contain the lubrieating oil inside the'drum.
FIG. 7 is a fragmentary enlarged view, partly diagrammatic, of the gear box with part of the hub shaft broken away to show parts otherwise obscured.
FIG. 8 is a diagram relative to the geometry of the vanes, hub, and drum as they rotate.
FIG. 9 is a block flow diagram showing how the rotary vane device maybe used as an integral vane compressor and vane motor.
DESCRIPTION OF THE PARTS AND THEIR OPERATION I The
vane engine10 of FIGS. I to 3 comprises a gen- 3 erally
cylindrical housing11. A hub-
shaft12 rotates about a
center line13, having its bearings on or supported by the housing 11 (FIG. 2). In the design shown, the hub-
shaft12 has eight equally spaced
piano hinges21, 22, 23, 24, 25, 26, 27, 28, (which may be pinned at the ends only or as shown) and eight
vanes31, 32, 33, 34, 35, 36, 37, and 38 are pinned at their center of gravity to respective
piano hinge points21, 22, 23, 24, 25, 26, 27, and 28 by means of
shafts41, 42, 43, 44, 45, 46, 47, and 48. Each of the
vanes31, 32, 33, 34, 35, 36, 37, 38 may have a
counter mass51, 52, 53, 54, 55, 56, 57, 58, so that as the vanes oscillate about their
respective shafts41, 42, 43, 44, 45, 46, 47, 48, the
hubshaft12 remains in dynamic balance as it rotates. Although eight vanes are shown in FIG. 1, any number of equally spaced vanes greater than three may be used.
A
drum14 rotates about a
center line15 which is displaced from the
hub center line13 by the distance y. The
drum14 has its bearing on the
housing11. The
drum14 and the hub-
shaft12 are synchronized to rotate in the same direction and at the same rotating speed. The
drum14 has
slots61, 62, 63, 64, 65, 66, 67, 68 at its outer diameter, and these slots are just large enough for the
corresponding vanes31, 32, 33, 34, 35, 36, 37, 38 to slide and oscillate in as the hub-
shaft12 and the
drum14 rotate. Between adjacent
axial slots61, 62, 63, 64, 65, 66, 67, 68 there may be gusseted arch or
beam sections71, 72, 73, 74, 75, 76, 77, 78 with cooling ports or
tubes79. The
drum14 may have
discs16 and 17 (FIG. 2) at its ends for supporting the
gusseted arc sections71, 72, 73, 74, 75, 76, 77, 78. The
discs16 and 17 also support the
bearings18 and 19 for the
drum14 on the
housing11. The
disc16 may also be provided with an internal gear 80 (FIG. 3).
The mechanism for synchronizing the hub-
shaft12 and the
drum14 may comprise the
internal gear80 and a
meshing spur gear81, which is keyed to a
shaft82 that has its bearings on the
housing11. Also keyed to
shaft82 is a
second spur gear83. The
spur gear83 may be meshed with a
pinion gear84, which is also meshed to a
third spur gear85, or, as shown in FIG. 7, the
gear84 is keyed to a
shaft84a that also carries a
gear84b meshed to the
gear85. The
spur gear85 is keyed to the hub-
shaft12. The
pinion gear84 has its shaft bearings on the
housing11. The pitch diameter and teeth of the
gears80, 81, 83, 84, and 85 are prescribed so that the hub-
shaft12 and the
drum14 are synchronized to rotate in the same direction and at the same rotating speed.
As shown in FIG. 7, the gears have the following pitch diameters:
diameter and the pitch diameters are related so that 01/02 X 03/04 X D.' Dfi Power may be transmitted through the
shaft12 or the
shaft82 or both of them. The
housing11 may be provided with
cooling fins86.
For the engine device of FIG. 1, the
housing11 may be provided with an intake scavenging and
exhaust port87. A
fan88, which is keyed to the hub-
shaft12, may be used to blow a fresh charge of air through the
open port87 to help scavenge the expanded gases out of the exhaust, to cool the
vanes31, 32, 33, 34, 35, 36, 37, and 38 and to cool the outer surface of each
drum beam section71, 72, 73, 74, 75, 76, 77, 78 when it is at the
port87. Also. the fan air flows past the cooling
fins86 to cool the
engine housing11 and blows air through the
cooling passages79 between the gussets and the arcuate segments in the
beam elements71, 72, 73, 74, 75, 76, 77, and 78.
The hub-
shaft12 rotates clockwise, and when, for example, the
vane36 moves past the
position89 of the
housing11, a fresh charge is trapped in a working
space96 bounded by the
adjacent vanes36 and 37, the outer surface of the
beam element76, and the inner surface of the
housing11 between the tips of the
vanes36, 37 and side disc section of the
housing2. Each of the
adjacent vanes31, 32, 33, 34, 35, 36, 37, 38 has a working
space91, 92, 93, 94, 95, 96, 97, 98. (For a three vane engine there would be three working spaces; for every vane, no matter how many, there is a corresponding working space.) A
fuel injector99 may inject fuel into each working
space91, 92, 93, 94, 95, 96, 97, 98, in turn as it moves past it.
As the hub-
shaft12 and the
drum14 move clockwise, they force the
vanes31, 32, 33, 34, 35, 36, 37, 38 to follow a prescribed movement and the working
space91, 92, 93, 94, 95, 96, 97, 98 becomes smaller, thus compressing the gases trapped in it in a manner approaching isentropic compression. When each space is in the top position (where the
space91 is in FIG. 1), it has been reduced to its smallest volume, and a
spark ignition system100 is timed to explode the fuel in the
space91 and heat it substantially by a constant volume process to increase its pressure and force the vanes to turn the hub-
shaft12 clockwise, so the hot gases will expand and do work on the engine shaft. When the
vanes31, etc., reach the
position101 of the
housing11, the hot expanded gases in the
space91, etc., are exhausted centrifugally by the centrifugal action of rotation. Also, the
fan88 forces exhaust gases to flow axially out of the
port87.
ln FIGS. 4 and 5 the rotary vane compressor or motor has most of the same parts as the
engine10 and are given the same reference numerals. The basic differences are that the
fuel injector99 and the
spark ignition system100 are eliminated, and in place of the common exhaust, scavenging, and
intake port87 shown for the
engine10, the
housing111 of the compressor or
motor110 has an
intake port112 separate from the
discharge port113, and these
ports112 and 113 are located diametrically opposite each other. Also, the
vanes31, 32, 33, 34, 35, 36, and 37 are practically inside the
drum114, when its
respective working space191, 192, 193, 194, 195, 196, 197, 198 is at its minimum volume, which is equal to the working tolerances between the
housing111 and the
drum114 multiplied by the vane width.
When operating as a
vane compressor110, the
intake port112 is closed as the
vane31, 32, etc., is forced past the
edge115 of the
port112 by means of clockwise rotation of hub-
shaft12 and the
drum114. The working space 191,192, etc., may be close to its largest volume just after the
vane31, 32, etc., closes the
intake port1 5 112 at the
station115. As the compressor rotates clockwise, the working
space191, 192, etc., is reduced, and the trapped gases are compressed approximately adiabatically until the
vanes31, 32, etc., move past the
station116 in the
housing111 to open the
space191, 192, etc., to the
discharge port113. The compressed gases are preferably forced out of the
space191, 192, etc., through the
discharge port113 into a compressed gas accumulator (not shown). When the
vanes31, 32, etc., rotate past a
station117, a small volume of compressed gas is trapped in the
space191, 192, etc., this trapped compressed gas expands approximately isentropically and does work on the
vanes31, 32, etc., as the
space191, 192, etc., increases. When the
vanes31, 32, etc., pass a
station118, the compressed gas in the
space191, 192, etc., is substantially equal to the pressure of the gas in the
intake port112. In order to increase the volumetric efficiency of the compressor, the volume of
space191, 192, etc., as the
vane31, 32, etc., moves past the
station117 should be kept to a minimum.
When the
device110 is operation as a vane motor or steam engine, the motor turns in a counterclockwise direction. Compressed gas or steam, etc., flows from the accumulator, not shown, through the
port113, which is now the intake port, into the working
space191, 192, etc. After the
vanes31, 32, etc., move past the
station116, the compressed gases are trapped in the working
space191, 192, etc. As the motor rotates counterclockwise, the working
space191, 192, etc., increases in volume and the compressed gases expand approximately isentropically'to do work on the
vanes31, 32, etc., until they move past the
station115 to open
port112, which is now the exhaust port. When the
exhaust port112 is open, the pressure in
theworking spaces191, 192, etc., is substantially the same as the gases in the
exhaust port112, except when the cutoff point is increased. After the
vane31, 32, etc., moves past the
station118, gases are trapped in the
space191, 192, etc.; this trapped gas is approximately isentropically compressed back to the pressure in the accumulator as the working
space191, 192, etc., is reduced. In order to increase the efficiency of the motor, the mass of gas which is compressed back to theaccumulator pressure is designed .to be a minimum. When the, 31, 32, etc., rotates past the
station117, the compressed gases are returned back to the
intake port112 to be combined with more compressed gases for another expansion work cycle.
In order to increase the motor torque per revolution an arcuate cutoff valve 120 (FIG. 5) may be turned counterclockwise to give the desired
cutoff volume191, 192, etc. For full admission, an
arcuate valve121 may be turned counterclockwise. The compressed gases flow axially from a
chamber122 through the arc ports into the working
spaces191, 192, etc.
In order to contain lubricating oil inside the
drum14 or 114, leaf spring scrapers 130 (FIG. 6) may be used to scrape the oil of the
vanes31, 32, etc., and keep it inside the
drum14 for lubricating the
pivot shafts41, 42, 43, 44, 45, 46, 47, 48, thebearings for the hub-
shaft12 and the
bearings18 and 19 for the drum-l4. The
130 may be secured to each
bridge section71, i
72, 73, 74, 75, 76, 77, 78, by means of
screws131 and a
nut plate132 or a quick disconnect clamp. The
beam section14 has an arcuate surface for the
spring130 to follow as it flexes; so it will have fatigue stresses which are below the endurance limit of the
spring steel130. As the
vanes31, 32, etc., reciprocate and oscillate in the slots 61, 62, etc., the leaf spring scrapes the excess lubricating oil of the
vanes31, 32, etc., so it will be contained inside the
drum14; just sufficient oil is left on the
vane31, 32, etc., to lubricate the rubbing surface between the
vanes31, 32, etc., and the slots 61, 62, etc.
In order to limit the flow of compressed gas into the
drum14 to a minimum, seal bars 200 may be provided in
axial slots201 in the ends of the beam arcs 71, etc., that bear on the
vanes31 to 38. Metal springs 202 or other fluidpressure means may be used to keep the seal bars 200 tight against the vanes, and the
bars200 fit snugly in the
axial slots201, thus a minimum flow of compressed gas passes from the working space 91-98 into the
drum14. v
The geometry of the rotary vanes is illustrated in FIG.
8. When a
vane31 is in its zero 0 position, the radial line R from the centerline of the
drum14 passes through the centerline of the hub-
shaft12 and through the pivot point of this
vane31. This radial line R also passes through the centerline of the
vane31 and is collinear with the radial line r from the centerline of the hub-
shaft12. Thus, the angle a between the centerline of the
vane31 and the radial line r is also zero when 0 0. P, r+ I P, maximum.
As the hub-
shaft11 and the
drum14 rotate clockwise, the angle or increases, and the blade tip leads the rotoryand the radial lines r and R remain parallel to each other. The vane 31 (whose length is I) bears on the drum 14 (R) at a distance e from the pivot point. Thus, thetip of the vane I will be at a radial distance P, from the centerline of the hub. As the vane rotates from its 6 0 position to its 0 90 1r/2 radians position, the angle a increases and reaches a maximum when 0= 90; likewise, the radial distance P, is a minimum when 0 90.
As the vane rotatespast its 9 90 position, the angle or decreases, and the radial distance P, increases until 0 l80 7r radians, where P, r I P, maximum again, and where a 0 again.
As the vane rotates past its 6 position,'the angle or becomes negative, and the vane tip lagsbehind the rotor. The radial lines r and R remain parallel to each other, and the radial distance P, from the hub centerline to the tip of the vane I again decreases until the vane reaches its 0 270 position, where P, is at its minimum radial position again and the angle a is at its negative maximum.
As the vane rotates past its 0 270 31r/2 position, the angle 0: decreases and the radial distance P, increases until 0 360 211' radians, where P, r l P, maximum again, and a 0 agaimThe cycle for one vane is then completed and will be repeated.
All of the
vanes32, 33, 34, 35, 36, 37, 38, undergo the same cycle asthe
vane31. If there are n vanes, they may be placed 21r/n radians apart, so that there will be equal working spaces between vanes.
The surface which the vane tips circumscribe as they rotate and oscillate about the hub shaft can be derived mathematically; they can be written in polar coordinates with the origin at the centerline of the hub-
shaft12. For a prescribed design, the only variable is the angle 0. The angle 0 is zero when a radial line drawn from the centerline of the drum first passes through the centerline of the hub shaft then through the pivot point of the vane and through the centerline of the vane. The vane is in its straight line extended position at 0 and
P r1 which is at its largest radius.
The fixed parameters for a prescribed design are: c the distance between the centerlines of the drum and the hub shaft. h the width of the slot in which the vane recipro' cates and oscillates. I the length of the vane from its pivot point to its extended position. r= the radial distance from the hub centerline to the vane pivot point, and R the radius of the drum where the drum bears on the vane. The variable parameters are:
the distance from the vane pivot point to its slot bearing point at R. l the thickness of the vane at e. P the radius from the hub centerline to the vane tip. V 0 the angle of the hub and drum measured from the radial line drawn from the drum centerline to the centerline of the hub shaft. The equation for the radius of the circumscribed surface of the vane tip with its origin at the hub centerline The equation for the distance from the vane pivot point to the point where the drum bears on the drum is:
The equation for the thickness of the vane is:
csin6 These equations may be derived as follows: The distances between the parallel radial lines R and r at angle 0:
s 0 sin 0.
The chord segment distance a for the vane contact at radius R to the vane pivot point at a (R-r) sin 6 The minimum distance I) from the vane pivot point to the chord. a line normal to the chord:
b (R-r) cos 0 c The hypotenuse e of the triangle abe:
e a h (R-r) (sin 0 cos 0) 2(Rr) 0 cos 0 +0 This gives the second equation shown above. The sine of the angle a between the radial line r and 5 the vane centerline 1:
The cosine law is used to get the radius of curvature P, of the surface circumscribed by the vane with respect to the star shaft centerline.
cos a V 1-sin a which is the first equation given above.
The angle B between the vane and the radial line R:
' For a constant slot I1 in the drum at radius R, to determine the vane thickness I with respect to the distance H e from the vane pivot point, so that it will fit snugly in h:
= P /sin a sin (b r/P sin a The area A at 0,:
A, z A (le,) (rlP sin a, [l (r/P,,) sin a, tan 01,]
The area A,, of the working space for n vanes of constant thickness 1:
sin a; [1( :x sin or tan 02 11} The working space or working volume is V the working area times the width of the vane s.
An integral vane compressor and vane motor 30 is shown in FIG. 9. It has a compressor intake port3ll, a
compressor exhaust port312, a motor intake po 313', and a
motor exhaust port314.
The
compressor intake port311 to each working space is. closed by a'vane after that working space achieves its largest volume,v low pressure gas being compressed in that working space as it is made smaller. The compressed gas, after it has been compressed to a desired pressure level, is discharged through the
compressor exhaust312, the
compressor exhaust port312 being passed by the vane just before the working space achieves its smallest volume.
The vane then opens the working space to high pressure gas flowing into the
motor intake port313 just after the working space passes its smallest volume. The
motor intake port313 remains open until the space between the vanes is at a prescribed value, then the next vane moving to close the working space off from the intake port 3l3 traps compressed gas in the working space. The working space increases in volume,'and the compressed gas expands to do work on the vanes and members rotatingtherwith until the working space is near its largest volume; I then the working space is opened by a vane to the
motor exhaust port314, so that the expanded gases are exhausted. The momentum of the hot gases forces them to flow out radially andtangentially, or flow out in radial and tangential directions, while a fan or other device scavenges the hot gases, axially or otherwise, so that afresh charge is blown into the working space where it enters the
compressor intake port311. v
To those skilled in the art to which this invention relates, many changes in construction and widely differing embodiments and applications of the invention will suggest themselves without departingfrom the spirit and scope of the invention. The disclosures and the description herein are purely illustrative and are not intended to be in any sense limiting.
I claim: v
1. An integral vane-compressor and vane motor having compressor intake port means and :exhaust port means and motor intake port means and exhaust port means, comprising: I
a rotating central hub having a series of vane pivot points spaced therearound at equal radii-from the center of the hub, r
at least three vanes, each pinned atits center of gravity to said hub at a said pivot point,
a generally cylindrical drum with its axis parallel'to and displaced radially from that of said hub, said drum having a separate slot for each vane through which the vane extends, for guiding the radial positionof each said vane,
synchronizing means mechanically linking said hub and said drum so that they rotate in the same direction and at the same rotating speed. so that said vanes reciprocate and oscillate in said guide slots as the hub and drum rotate,
a housing enclosing said vanes and cooperating with said vanes and said drum to provide a series of working spaces, one for each said vane to compress or expand afluid, and
intake and exhaust port means for leading fluid into andfrom said working spaces,
said compressor intake port means to each working space being closed by a said vane after that working space achieves its largest volume, low pressure gas being compressed in said workingispace as it is made smaller, the compressed gas, after it has been compressed to a desired pressure level, being discharged through said compressor exhaust port means,
said compressor exhaust port means being passed by said vane just before 'said working space achieves its smallest volume,
said vane then opening said working space to high pressure gas flowing into said motor intake port means just after said working space passes its smallest volume, said motor intake port means remaining open until the space between said vanes is at a prescribed value, then the next said vane moving to close said working space off from said intake port means and to trap compressed gas in said working space,
said working space increasing in volume and said compressed gas expanding to do work on the vanes and members rotating therewith until said working space is near its largest volume,
then said working space being opened by a said vane to said motor exhaust port means, so that said expanded gases are exhausted;
the centrifugal force of the hot gases forcing them to flow out radially and a fan for scavenging said hot gases axially so that a fresh charge is blown into the working space where it enters said compressor intake port means.
2. An integral vane compressor and vane motor having compressor intake port means and exhaust port means and motor intake port means and exhaust port means, comprising? a rotating central hub having a series of vane pivot points spaced therearound at equal radii from the center of the hub,
at least three vanes, each pinned at its center of gravity to said hub at a said pivot point,
a generally cylindrical drum with its axis parallelto and displaced radially from that of said hub, said drum having a separate slot for each vane through which the vane extends, for guiding the radial position of each said vane,
synchronizing means mechanically linking said hub and said drum so that they rotate in the same direction and at the same rotating speed, so that said vanes reciprocate and oscillate in said guide slots as the hub and drum rotate,
a housing enclosing said vanes and cooperating with said vanes and said drum to provide a series of working spaces, one for each said vane to compress or expand a fluid, and
intake and exhaust port means for leading fluid into and from said working spaces.
said compressor intake port means to each working space being closed by a said vane after that working space achieves its largest volume, low pressure gas being compressed in said working space as it is made smaller, the compressed gas, after it has been compressed to a desired pressure level, being discharged through said compressor exhaust port means,
said compressor exhaust port means being passed by said vane just before said working space achieves its smallest volume,
said vane then opening said working space to high pressure gas flowing into said motor intake port means just after said working space passes its smallest volume, said motor intake port means remaining open until the space between said vanes is at a prescribed value, then the next said vane moving to close said working space off from said intake port means and to trap compressed gas in said working space,
said working space increasing in volume and said compressed gas expanding to do work on the vanes and members rotating therewith until said working space is near its largest volume,
then said working space being opened by a said vane to said motor exhaust port means. so that said expanded gases are exhausted;
the momentum of the hot gases forcing them to flow out in a radial and tangential direction, and
means for scavenging said hot gases so that a fresh charge is blown into the working space where it enters said compressor intake port means.
Claims (2)
1. An integral vane compressor and vane motor having compressor intake port means and exhaust port means and motor intake port means and exhaust port means, comprising: a rotating central hub having a series of vane pivot points spaced therearound at equal radii from the center of the hub, at least three vanes, each pinned at its center of gravity to said hub at a said pivot point, a generally cylindrical drum with its axis parallel to and displaced radially from that of said hub, said drum having a separate slot for each vane through which the vane extends, for guiding the radial position of each said vane, synchronizing means mechanically linking said hub and said drum so that they rotate in the same direction and at the same rotating speed, so that said vanes reciprocate and oscillate in said guide slots as the hub and drum rotate, a housing enclosing said vanes and cooperating with said vanes and said drum to provide a series of working spaces, one for each said vane to compress or expand a fluid, and intake and exhaust port means for leading fluid into and from said working spaces, said compressor intake port means to each working space being closed by a said vane after that working space achieves its largest volume, low pressure gas being compressed in said working space as it is made smaller, the compressed gas, after it has been compressed to a desired pressure level, being discharged through said compressor exhaust port means, said compressor exhaust port means being passed by said vane just before said working space achieves its smallest volume, said vane then opening said working space to high pressure gas flowing into said motor intake port means just after said working space passes its smallest volume, said motor intake port means remaining open until the space between said vanes is at a prescribed value, then the next said vane moving to close said working space off from said intake port means and to trap compressed gas in said working space, said working space increasing in volume and said compressed gas expanding to do work on the vanes and members rotating therewith until said working space is near its largest volume, then said working space being opened by a said vane to said motor exhaust port means, so that said expanded gases are exhausted; the centrifugal force of the hot gases forcing them to flow out radially and a fan for scavenging said hot gases axially so that a fresh charge is blown into the working space where it enters said compressor intake port means.
2. An integral vane compressor and vane motor having compressor intake port means and exhaust port means and motor intake port means and exhaust port means, comprising: a rotating central hub having a series of vane pivot points spaced therearound at equal radii from the center of the hub, at least three vanes, each pinned at its center of gravity to said hub at a said pivot point, a generally cylindrical drum with its axis parallel to and displaced radially from that of said hub, said drum having a separate slot for each vane through which the vane extends, for guiding the radial position of each said vane, synchronizing means mechanically linking said hub and said drum so that they rotate in the same direction and at the same rotating speed, so that said vanes reciprocate and oscillate in said guide slots as the hub and drum rotate, a housing Enclosing said vanes and cooperating with said vanes and said drum to provide a series of working spaces, one for each said vane to compress or expand a fluid, and intake and exhaust port means for leading fluid into and from said working spaces, said compressor intake port means to each working space being closed by a said vane after that working space achieves its largest volume, low pressure gas being compressed in said working space as it is made smaller, the compressed gas, after it has been compressed to a desired pressure level, being discharged through said compressor exhaust port means, said compressor exhaust port means being passed by said vane just before said working space achieves its smallest volume, said vane then opening said working space to high pressure gas flowing into said motor intake port means just after said working space passes its smallest volume, said motor intake port means remaining open until the space between said vanes is at a prescribed value, then the next said vane moving to close said working space off from said intake port means and to trap compressed gas in said working space, said working space increasing in volume and said compressed gas expanding to do work on the vanes and members rotating therewith until said working space is near its largest volume, then said working space being opened by a said vane to said motor exhaust port means, so that said expanded gases are exhausted; the momentum of the hot gases forcing them to flow out in a radial and tangential direction, and means for scavenging said hot gases so that a fresh charge is blown into the working space where it enters said compressor intake port means.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00350632A US3813191A (en) | 1972-05-01 | 1973-04-12 | Rotary vane device for compressor, motor or engine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US26886672A | 1972-05-01 | 1972-05-01 | |
US00350632A US3813191A (en) | 1972-05-01 | 1973-04-12 | Rotary vane device for compressor, motor or engine |
Publications (1)
Publication Number | Publication Date |
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US3813191A true US3813191A (en) | 1974-05-28 |
Family
ID=26953374
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Application Number | Title | Priority Date | Filing Date |
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US00350632A Expired - Lifetime US3813191A (en) | 1972-05-01 | 1973-04-12 | Rotary vane device for compressor, motor or engine |
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US7074016B1 (en) * | 2002-05-24 | 2006-07-11 | Massachusetts Institute Of Technology | Planar turbopump assembly |
US20060283419A1 (en) * | 2005-06-16 | 2006-12-21 | Ionel Mihailescu | Continuous internal combustion engine |
US20100047088A1 (en) * | 2008-08-20 | 2010-02-25 | Protonex Technology Corporation | Roller vane pump with integrated motor |
US20100047097A1 (en) * | 2008-08-20 | 2010-02-25 | Protonex Technology Corporation | Roller vane pump with integrated motor |
GR20170100407A (en) * | 2017-09-07 | 2019-05-09 | Αριστειδης Εμμανουηλ Δερμιτζακης | Compressor with multiple mechanical vapor recompression chambers |
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EP0067307A2 (en) * | 1981-06-12 | 1982-12-22 | Volkswagen Aktiengesellschaft | Sliding-vane compressor |
EP0067307A3 (en) * | 1981-06-12 | 1983-02-16 | Volkswagen Aktiengesellschaft | Sliding-vane compressor |
US5664940A (en) * | 1995-11-03 | 1997-09-09 | Flojet Corporation | Gas driven pump |
US5833439A (en) * | 1995-11-03 | 1998-11-10 | Du; Benjamin R. | Slide valve of a gas driven pump |
US6062427A (en) * | 1998-08-27 | 2000-05-16 | Du Investments L.L.C. | Beer keg and pre-mixed beverage tank change-over device |
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US6343539B1 (en) | 1999-11-10 | 2002-02-05 | Benjamin R. Du | Multiple layer pump diaphragm |
US7074016B1 (en) * | 2002-05-24 | 2006-07-11 | Massachusetts Institute Of Technology | Planar turbopump assembly |
US20060283419A1 (en) * | 2005-06-16 | 2006-12-21 | Ionel Mihailescu | Continuous internal combustion engine |
US20060283420A1 (en) * | 2005-06-16 | 2006-12-21 | Ionel Mihailescu | Continuous internal combustion engine and rotary machine |
US20100047088A1 (en) * | 2008-08-20 | 2010-02-25 | Protonex Technology Corporation | Roller vane pump with integrated motor |
US20100047097A1 (en) * | 2008-08-20 | 2010-02-25 | Protonex Technology Corporation | Roller vane pump with integrated motor |
GR20170100407A (en) * | 2017-09-07 | 2019-05-09 | Αριστειδης Εμμανουηλ Δερμιτζακης | Compressor with multiple mechanical vapor recompression chambers |
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