patents.google.com

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 PDF

Info

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
US
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
Application number
US00350632A
Inventor
B Foster
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
1972-05-01
Filing date
1973-04-12
Publication date
1974-05-28
1973-04-12 Application filed by Individual filed Critical Individual
1973-04-12 Priority to US00350632A priority Critical patent/US3813191A/en
1974-05-28 Application granted granted Critical
1974-05-28 Publication of US3813191A publication Critical patent/US3813191A/en
1991-05-28 Anticipated expiration legal-status Critical
Status Expired - Lifetime legal-status Critical Current

Links

  • 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

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C17/00Arrangements for drive of co-operating members, e.g. for rotary piston and casing
    • F01C17/02Arrangements for drive of co-operating members, e.g. for rotary piston and casing of toothed-gearing type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-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
    • F01C1/34Rotary-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
    • F01C1/344Rotary-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
    • F01C1/352Rotary-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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

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 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). In the design shown, 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. Although 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. Between adjacent

axial slots

61, 62, 63, 64, 65, 66, 67, 68 there may be gusseted arch or

beam sections

71, 72, 73, 74, 75, 76, 77, 78 with cooling ports or

tubes

79. 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.

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

shaft

12 or the

shaft

82 or both of them. The

housing

11 may be provided with

cooling fins

86.

For the engine device of FIG. 1, 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. (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 injector

99 may inject fuel into each working

space

91, 92, 93, 94, 95, 96, 97, 98, in turn as it moves past it.

As the hub-

shaft

12 and the

drum

14 move clockwise, they force the

vanes

31, 32, 33, 34, 35, 36, 37, 38 to follow a prescribed movement and the working

space

91, 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

space

91 is in FIG. 1), it has been reduced to its smallest volume, and a

spark ignition system

100 is timed to explode the fuel in the

space

91 and heat it substantially by a constant volume process to increase its pressure and force the vanes to turn the hub-

shaft

12 clockwise, so the hot gases will expand and do work on the engine shaft. When the

vanes

31, etc., reach the

position

101 of the

housing

11, the hot expanded gases in the

space

91, etc., are exhausted centrifugally by the centrifugal action of rotation. Also, the

fan

88 forces exhaust gases to flow axially out of the

port

87.

ln 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. Also, the

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.

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. As the compressor rotates clockwise, 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). When 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. When 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. In order to increase the volumetric efficiency of the compressor, the volume of

space

191, 192, etc., as the

vane

31, 32, etc., moves past the

station

117 should be kept to a minimum.

When the

device

110 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

port

113, which is now the intake port, into the working

space

191, 192, etc. After the

vanes

31, 32, etc., move past the

station

116, the compressed gases are trapped in the working

space

191, 192, etc. As the motor rotates counterclockwise, 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. When the

exhaust port

112 is open, 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. After the

vane

31, 32, etc., moves past the

station

118, 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. 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

station

117, the compressed gases are returned back to the

intake port

112 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 volume

191, 192, etc. For full admission, 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.

In order to contain lubricating oil inside the

drum

14 or 114, leaf spring scrapers 130 (FIG. 6) 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. The

scrapers

130 may be secured to each

bridge section

71, i

72, 73, 74, 75, 76, 77, 78, by means of

screws

131 and a

nut plate

132 or a quick disconnect clamp. 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. As the

vanes

31, 32, etc., reciprocate and oscillate in the slots 61, 62, etc., 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.

In order to limit the flow of compressed gas into the

drum

14 to a minimum, 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. v

The geometry of the rotary vanes is illustrated in FIG.

8. When a

vane

31 is in its zero 0 position, the radial line R from the centerline of the

drum

14 passes through the centerline of the hub-

shaft

12 and through the pivot point of this

vane

31. This radial line R also passes through the centerline of the

vane

31 and is collinear with the radial line r from the centerline of the hub-

shaft

12. Thus, the angle a between the centerline of the

vane

31 and the radial line r is also zero when 0 0. P, r+ I P, maximum.

As the hub-

shaft

11 and the

drum

14 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

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. 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 r

1 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 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. 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 port

311. 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.

US00350632A 1972-05-01 1973-04-12 Rotary vane device for compressor, motor or engine Expired - Lifetime US3813191A (en)

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
US3813191A true US3813191A (en) 1974-05-28

Family

ID=26953374

Family Applications (1)

Application Number Title Priority Date Filing Date
US00350632A Expired - Lifetime US3813191A (en) 1972-05-01 1973-04-12 Rotary vane device for compressor, motor or engine

Country Status (1)

Country Link
US (1) US3813191A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0011762A1 (en) * 1978-11-28 1980-06-11 Kuechler, Jürgen Dr. Rotary piston engine
EP0067307A2 (en) * 1981-06-12 1982-12-22 Volkswagen Aktiengesellschaft Sliding-vane compressor
US5664940A (en) * 1995-11-03 1997-09-09 Flojet Corporation 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
US6099264A (en) * 1998-08-27 2000-08-08 Itt Manufacturing Enterprises, Inc. Pump controller
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
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

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1039025A (en) * 1910-12-23 1912-09-17 Ralph Carroll Ventilating apparatus.
US1296356A (en) * 1918-05-04 1919-03-04 George Bey Combined motor and pump.
US3685287A (en) * 1970-12-08 1972-08-22 Mcculloch Corp Re-entry type integrated gas turbine engine and method of operation
US3747573A (en) * 1972-05-01 1973-07-24 B Foster Rotary vane device for compressor, motor or engine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1039025A (en) * 1910-12-23 1912-09-17 Ralph Carroll Ventilating apparatus.
US1296356A (en) * 1918-05-04 1919-03-04 George Bey Combined motor and pump.
US3685287A (en) * 1970-12-08 1972-08-22 Mcculloch Corp Re-entry type integrated gas turbine engine and method of operation
US3747573A (en) * 1972-05-01 1973-07-24 B Foster Rotary vane device for compressor, motor or engine

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0011762A1 (en) * 1978-11-28 1980-06-11 Kuechler, Jürgen Dr. Rotary piston engine
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
US6099264A (en) * 1998-08-27 2000-08-08 Itt Manufacturing Enterprises, Inc. Pump controller
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

Similar Documents

Publication Publication Date Title
US3747573A (en) 1973-07-24 Rotary vane device for compressor, motor or engine
CA2642932C (en) 2014-05-06 Vane machine with stationary and rotating cylinder parts
US5501586A (en) 1996-03-26 Non-contact rotary vane gas expanding apparatus
US3813191A (en) 1974-05-28 Rotary vane device for compressor, motor or engine
US10309222B2 (en) 2019-06-04 Revolving outer body rotary vane compressor or expander
US6273694B1 (en) 2001-08-14 Rotary-piston machine
KR102037077B1 (en) 2019-10-29 Rotary machine
JP2001271609A (en) 2001-10-05 Waste heat recovery device of internal combustion engine
US3890071A (en) 1975-06-17 Rotary steam engine
US3902829A (en) 1975-09-02 Rotary power device
US7051698B2 (en) 2006-05-30 Rotary drive mechanism
CN104254692B (en) 2016-06-29 A kind of blade mechanism
US3433167A (en) 1969-03-18 Fluid machines
US7080623B1 (en) 2006-07-25 Rotor for an axial vane rotary device
RU2670475C1 (en) 2018-10-23 Rotary vane device
US3762844A (en) 1973-10-02 Positive displacement rotary heat engine
Zhong et al. 2019 Study on leakage loss via the radial clearance in a double-swing vane compressor for electric vehicle air conditioning systems
US3737248A (en) 1973-06-05 Rotary engine
US9803480B2 (en) 2017-10-31 Liquid ring turbine and method of use
CN106121730B (en) 2018-12-07 A kind of blade aerodynamic machine
US20020020171A1 (en) 2002-02-21 Rotary machine
US3446016A (en) 1969-05-27 Liquid sealed continuous combustion engine
RU2075652C1 (en) 1997-03-20 Rotary bladed device
RU2256808C2 (en) 2005-07-20 Internal combustion turborotor engine
HU186775B (en) 1985-09-30 Flow technical machine having rotary case