CA2068302A1 - Revolving-rotating vane meter-motor-pump - Google Patents
Revolving-rotating vane meter-motor-pumpInfo
- Publication number
- CA2068302A1 CA2068302A1 CA002068302A CA2068302A CA2068302A1 CA 2068302 A1 CA2068302 A1 CA 2068302A1 CA 002068302 A CA002068302 A CA 002068302A CA 2068302 A CA2068302 A CA 2068302A CA 2068302 A1 CA2068302 A1 CA 2068302A1
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- Prior art keywords
- axis
- closed loop
- rotation
- vanes
- loop cavity
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Rotary Pumps (AREA)
Abstract
REVOLVING-ROTATING VANE METER-MOTOR-PUMP
Abstract of Disclosure A positive displacement fluid handling apparatus comprises a closed loop cavity (45) with continuously varied cross sectional areas between the maximum and minimum values respectively occurring at two diametrically opposite sections thereof, and a plurality of vanes (40) disposed within and traveling through the closed loop cavity (45) and rotatably supported by a rotor (41), wherein the revolving motion of the vanes (40) are coupled to the rotating motion of the rotor (41) by positively meshing gearing in such a way that the individual vane (40) revolves about its own axis (39) at one half of the rotary speed of the rotating motion of the rotor (41) about the rotor axis (38), and the cross sectional areas of the closed loop cavity (45) are closely matched to the areas of sweep of the vanes (40) throughout the closed loop cavity (45).
Abstract of Disclosure A positive displacement fluid handling apparatus comprises a closed loop cavity (45) with continuously varied cross sectional areas between the maximum and minimum values respectively occurring at two diametrically opposite sections thereof, and a plurality of vanes (40) disposed within and traveling through the closed loop cavity (45) and rotatably supported by a rotor (41), wherein the revolving motion of the vanes (40) are coupled to the rotating motion of the rotor (41) by positively meshing gearing in such a way that the individual vane (40) revolves about its own axis (39) at one half of the rotary speed of the rotating motion of the rotor (41) about the rotor axis (38), and the cross sectional areas of the closed loop cavity (45) are closely matched to the areas of sweep of the vanes (40) throughout the closed loop cavity (45).
Description
X
2 This invention re1ates to a positive displacement fluid handling 3 apparatus that operates as a positive displacement flowmeter, a 4 hydraulic-pneumatic motor such as a windmill, a positive displacement pump, or an internal combustion engine, which comprises a plurality of 6 vanes disposed within and traveling through a closed loop cavity (a 7 toroidal cavity), wherein the vanes revolvably supported by the rotor 8 of the apparatus are coupled to the rotating motion of the rotor in 9 such a way that the individual vane revolves about its own axis at one half of the speed of rotation thereof about the axis of rotation of 11 the rotor. The cross section of the closed loop cavity accommodating 12 the vanes is continuously varied between the maximum and minimum values 13 respectively occurring at two diametrically opposite sections of the 14 closed loop cavity in such a way that the cross sectional areas of the closed loop cavity are closely matched to the areas of sweep of the 16 vanes at all angular locations about the axis of rotation.
18 There are a number of inventions teaching the positive displacement 19 apparatus comprising a plurality of vanes operating under a compound combination of the revolving motion and the rotating motion. An 21 Australian patent (643/31) shows a pseudo-positive displacement 22 apparatus that employs a plurality of revolving-rotating vanes, but the 23 cross section of the closed loop cavity accommodating the vanes are not 24 varied to match the cross sectional areas thereof to the areas of sweep of the vanes. A U.S. patent (3,895,893) shows a similar apparatus 26 wherein the closed loop cavity is divided into two sections with two 27 different constant cross sectional areas, and the vanes are supported 28 by the rotor in a spring-biased arrangement whereby the individual vane 29 is forced to pivot about its own axis to conform with the cross sectional geometry of the closed loop cavity. A Japanese patent 31 application (63-279598) shows one of the more intelligent versions of 32 the apparatus wherein the vanes are pivoted over angles significantly 33 less than 90 degrees during each cycle of rotation thereof instead of 34 continuously revolving about the vane axis. These prior arts amount to an attempt to lasso a run-away train by throwing a rope. The positive 36 displacement fluid handling apparatus of the type under discussion, 37 whether they are applied as a flowmeter, a motor or engine, or a pump, 38 are subjected to a brutal loading by the fluid pressure and, - 2 - 2~
1 consequently, the apparatus employing anything less than 100 percent 2 positive mechanical motion coupling means do not have a chance to 3 actually work in the real world. The above-mentioned prior arts 4 employing the vanes under pivoting movements manipulated by the guiding surfaces such as the wall of the closed loop cavity or the 6 cam and cam follower combination are merely a few of many apparatus, 7 which lack the mechanical muscle and precision to be an actually 8 working positive displacement apparatus.
The primary object of the present invention is to provide a 11 positive displacement fluid handling apparatus comprising a plurality 12 of vanes disposed within and traveling through a closed loop cavity 13 (a toroidal cavity), wherein the individual vane revolves about its 14 own axis at one half of the rotating speed thereof about the axis of rotation of the rotor revolvably supporting the vanes whereby the 16 individual vane completes one full revolution about its own axis for 17 every two full rotations-aboutthe axis of rotation of the rotor. The 18 cross section of the closed loop cavity accommodating the vanes is 19 varied in such a way that the cross sectional areas of the closed loop cavity are closely matched to the areas of sweep of the vanes at all 21 angular locations about the axis of rotation.
22 Another object is to provide the apparatus described in the primary 23 object of the present invention, wherein the revolving motion of the 24 individual vane is coupled to the rotating motion thereof by a positively meshing gearing.
26 A further object is to provide the apparatus described in the 27 primary object of the present invention, wherein the axes of revolution 28 of the vanes are disposed on a conical surface coaxial to the axis of 29 rotation of the rotor revolvably supporting the vanes.
Yet another object is to provide the apparatus described in the 31 primary object of the present invention, wherein the axes of revolution 32 of the vanes are disposed on a plane perpendicular to the axis of 33 rotation of the rotor revolvably supporting the vanes.
34 Yet a further object is to provide the apparatus described in the primary object of the present invention, wherein the axes of revolution 36 of the vanes are disposed on a circular cylindrical surface coaxial to 37 the axis of rotation of the rotor revolvably supporting the vanes.
38 Still another object is to provide the apparatus described in the 1 primary object of the present invention, that includes means for 2 injecting fuel into the closed loop cavity accommodating the vanes and 3 means for igniting the fuel-air mixture therein, whereby the apparatus 4 works as an internal combustion engine.
These and other objects of the present invention will become 6 clear as the description thereof progresses.
8 The present invention may be described with a greater clarity and 9 specificity by referring to the following figures :
Figure 1 illustrates a developed view of a plurality of vanes 11 disposed within and traveling through a closed loop cavity, which 12 shows the operating principles of the present invention.
13 Figure 2 illustrates a cross section of an embodiment of the 14 positive displacement apparatus of the present invention.
Figure 3 illustrates a cross section of another embodiment of 16 the positive displacement apparatus of the present invention.
17 Figure 4 illustrates another cross section of the embodiment 18 shown in Figure 2.
19 Figure 5 illustrates another cross section of the embodiment shown in Figure 3.
21 Figure 6 illustrates a preferred embodiment of the gearing 22 coupling the revolving and rotating motions of the vanes to one 23 another.
24 Figure 7 illustrates a cross section of a further embodiment of the positive displacement apparatus of the present invention.
26 Figure 8 illustrates an embodiment of gearing usable in 27 constructing the embodiment shown in Figure 7.
28 Figure 9 illustrates an internal combustion engine version of 29 the present invention.
31 In Figure 1 there is illustrated a developed view of the 32 plurality of vanes I, 2, 3, 4, etc. disposed within and traveling 33 through a closed loop cavity (a toroidal cavity) 5. The plurality 34 of vanes are assembled into a rotor assembly of the positive displacement apparatus of the present invention, which rotor 36 assembly of a construction axisymmetric about the axis of rotation 37 thereof forms the core region surrounded by the closed loop cavity 38 5, wherein the individual vane I is supported by the rotor 1 revolvably about its own axis 6 (the axis of revolution) and 2 geared to the rotating motion of the rotor assembly about the axis 3 of rotation coinciding with the center axis of the closed loop cavity 4 5 in such a way that the individual vane revolves about its axis of revolution at one half of the angular velocity of the rotation of 6 the rotor assembly about the axis of rotation, whereby each of the 7 plurality of vanes completes full 360 degree revolution about the 8 respective axes of revolution for every 720 degree rotation of the 9 rotor assembly about the axis of rotation. The cross section of the closed loop cavity is varied between the maximum value at the 0 11 (360) degree section and the minimum value at the 180 degree section 12 in such a way that the cross sectional areas of the closed loop 13 cavity 5 are closely matched to the areas of sweep of the vanes at 14 all angular locations during the rotating motion. Two ports providing a flow passage for the fluid media are respectively open to 16 the two opposite halves of the closed loop cavity 5 located on the 17 two opposite sides of the plane of symmetry passing through the 0 18 (360) and 180 degree sections of the closed loop cavity 5. It is 19 readily noticed that the volume between two adjacent vanes increases in the first half of the closed loop cavity 5 that facilitates the 21 suction of the fluid media through the first port open to the first 22 half of the closed loop cavity 5, or the expansion of the gas in the 23 first half of the closed loop cavity 5 and discharge through the 24 first port, while the volume between two adjacent vanes decreases in the second half of the closed loop cavity 5 that facilitates the 26 discharge of the fluid media through the second port open to the 27 second half of the closed loop cavity 5, or the compression of gas 28 entering through the second port into the second half of the closed 29 loop cavity 5.
In Figure 2 there is illustrated a cross section of an embodi-31 ment of the positive displacement apparatus of the present invention, 32 wherein the axes of revolution of the plurality of vanes are disposed 33 on a plane perpendicular to the axis of rotation of the rotor 34 assembly. The plurality of vanes 7 disposed within and traveling through the closed loop cavity 8 are respectively supported by a 36 plurality of stub shafts 9 which are revolvably supported by the 37 rotor 10. Of course, the central axis of each of the stub shafts 9 38 defines the axis of rovolution of each of the vanes 7, while the axis ~ : ' ~ 3~ ?
1 of rotation of the vane assembly is defined by the central axis 11 2 of the rotor 10. The plurality of stub shafts 9 respectively 3 supporting the plurality of vanes 7 are disposed in a substantially 4 axisymmetrically radiating pattern from the axis 11 of rotation of the rotor 10 and respectively include a plurality of bevel gears 12 6 at the inner extremity thereof.The closed loop cavity 8 has the outer 7 cylindrical wall and two opposite side walls provided by the housing 8 structure 13, and the inner cylindrical wall provided by the rotor 10.
9 The apparatus works best when the outer and inner cylindrical walls respectively coincide with two spherical surfaces concentric to the 11 spherical center of the rotor assembly including the rotor 10 and the 12 vanes 7. The two opposite side walls of the closed loop cavity 8 are 13 curved in such a way that there is no or a little gap between the 14 surface of the vanes and the walls of the closed loop cavity 8 at all angular locations about the axis of rotation 11. In the versions of 16 the apparatus applied as flowmeters,hydraulic or pmeumatic motors or 17 pumps, two ports 14 and 15 are respectively open to the two opposite 18 halves of the closed loop cavity respectively located on the two 19 opposite sides of a plane of symmetry passing through the sections of the maximum and the minimum cross sectional area of the closed loop 21 cavity 8. In order to work as a positive displacement apparatus, 22 the two ports 14 and 15 must be separated from one another by two 23 diametrically oppositely located unbroken sections of the closed 24 loop cavity 8, wherein each section thereof includes at least one vane at all instances during the rotating motion of the vanes about 26 the axis 11 of rotation. The arrangement of the intake and discharge 27 ports in the internal combustion engine version of the apparatus is 28 shown in Figure 9.
29 In Figure 3 there is illustrated a cross section of another embodiment of the positive displacement apparatus of the present 31 invention, wherein the axes of revolution of the plurality of vanes 32 are disposed on a circular cylindrical surface coaxial to the axis 33 16 of rotation of the rotor assembly including one or two supporting 34 flanges coaxial to the axis 16 of rotation and a plurality of vanes 17 disposed therebetween and respectively supported by a plurality of 36 shafts 18, which shafts are revolvably supported by one or two 37 supporting flanges forming a part of the rotor assembly. Of course 38 the axis of revolution of each of the plurality of vanes 17 is defined z~
1 by the central axis of each of the plurality of shafts 18. A
2 plurality of tie-bars 19 disposed intermediate the two supporting 3 flanges in a parallel and axisymmetric pattern with respect to the 4 axis of rotation 16 structurally connect the two supporting flanges to one another. Of course, a rotor assembly employing a single 6 supporting flange would not need these tie-bars 19. The closed 7 loop cavity 20 has the outer and inner cylindrical walls provided by 8 the housing 21, and two opposite side walls provided by the two 9 supporting flanges. Of course, in an embodiment employing a single supporting flange, only one of the two opposite side walls of the 11 closed loop cavity 20 is provided by the supporting flange as the 12 other of the two opposite side walls is provided by the housing 21.
13 The outer and inner cylindrical wall of the closed loop cavity 20 are 14 spaced from one another in such a way that there is no or a little gap between the surfaces of the vanes 17 and the walls of the closed 16 loop cavity 20 at all instances during the rotating motion of the vanes 17 17 about the axis 16 of the rotation. The pair of ports 22 and 23 18 are included in the manner described in conjunction with the embodi-19 ment shown in Figure 2.
In Figure 4 there is illustrated another cross section of the 21 embodiment of the positive displacement apparatus shown in Figure 2, 22 which cross section is taken along plane 4-4 as shown in Figure 2.
23 The rotor assembly including the plurality of vanes 7 and the rotor 24 10 is supported by the rotor shaft 24, that is rotatably supported by the housing 13. The bevel gear 12 nonrotatably mounted on the 26 vane shaft 8 engages a stationary pinion bevel gear 25 disposed 27 coaxially to the axis 11 of rotation and affixed to the housing 28 13, wherein a plurality of idler bevel gears 26 disposed in an 29 axisymmetric arrangement with respect to the axis 11 of rotation and revolvably supported by the rotor 10 are employed in the gearing 31 engagement between the plurality of bevel gears 12 and the stationary 32 bevel gear 25. The ratio of the pitch diameters or the numbers of 33 gear teeth of the bevel gears 12, 25 and 26 are arranged in such a 34 way that the individual vane revolves about its axis of revolution at one half of the speed of rotation of the rotor assembly about the 36 axis 11 of rotation whereby the individual vane completes one full 37 revolution about its own axis of revolution for every two full 38 rotations of the rotor assembly about the axis 11 of rotation, which ~r~
1 requirement clearly explains why those idler bevel gears 26 have to 2 be employed. A vane motion detector 27 may be employed to measure 3 the speed of rotation of the rotor assembly as a measure of fluid 4 media passing through the apparatus. It is readily realized that the shaft 24 does not need to extend through and out of the housing 6 13 when the apparatus is applied as a flowmeter only.
7 In Figure 5 there is illustrated another cross section of the 8 embodiment of the postive displacement apparatus shown in Figure 3, 9 which cross section is taken along plane 5-5 as shown in Figure 3.
The rotor assembly including the two supporting flanges 28 and 29, 11 and the plurality of vanes 17 is supported by the rotor shaft 30, 12 that is rotatably supported about the axis 16 of rotation by the 13 housing 21. The plurality of vane shafts 18 respectively include 14 a plurality of gears 31, which engage the stationary pinion gear 32 through a plurality of idler gears 33 rotatably supported by the 16 rotor flanges. The stationary pinion gear 32 is disposed coaxially 17 to the axis 16 of rotation and affixed to the housing 21. The gearing 18 ratio of the gears 31, 32 and 33 are selected in such a way that the 19 individual vane 17 revolves about its own axis of revolution at one 20 half of the rotating speed of the rotor assembly about the axis 16 of 21 rotation whereby the individual vane completes a full revolution about 22 its own axis of revolution for every two full rotations of the rotor 23 assembly about the axis 16 of rotation. Of course, in an alternative 24 design, the second flange 29 and the stub vane shafts extending 25 thereinto may be omitted and its place filled up by the housing 26 structure 21.
27 In Figure 6 there is illustrated a schematic diagram showing an 28 arrangement of gearing that couples the revolving motion of the vanes 29 to the rotating motion of the rotor assembly in an one to two rotary 30 speed ratio. Each adjacent pair 34 and 35 of the plurality of vane 31 gears share a common idler gear 36 in engaging the stationary pinion 32 gear 37 affixed to the housing structure of the apparatus. This 33 particular embodiment of the gearing arrangement can be employed in 34 constructing the embodiments of the positive displacement apparatus 35 shown in Figures 4 and 5.
36 In Figure 7 there is illustrated a cross section of a further 37 embodiment of the positive displacement apparatus of the present 38 invention, wherein the axes of revolution of the vanes are disposed d ~ ~
1 on a conical surface coaxial to the axis 38 of rotation of the rotor 2 assembly. The plurality of stub shafts 39 respectively supporting 3 the plurality of vanes 40 are disposed on a conical surface coaxial to 4 the axis 38 of rotation in an axisymmetric arrangement and revolvably supported by the rotor 41, wherein the plurality of bevel 6 gears 42 nonrotatably mounted on the plurality of stub shafts 39 7 engage a stationary pinion bevel gear 42 directly without any idler 8 gears, which stationary pinion bevel gear 42 is disposed coaxially to 9 the axis 38 of rotation and affixed to the housing 44. The closed loop cavity 45 has the outer cylindrical wall and the two conical 11 side walls provided by the housing 44 and the inner cylindrical wall 12 provided by the rotor 41. The two conical walls of the closed loop 13 cavity 45 are arranged in such a way that there is no or a little 14 gap between the surfaces of the vanes 40 and the walls of the closed loop cavity 45 at all angular positions about the axis 38 of rotation.
16 The apparatus works best when the outer and inner cylindrical walls of 17 the closed loop cavity 45 respctively coincide with two spherical 18 surfaces concentric to the point of convergence of the axes of 19 revolution of the plurality of vanes 40. The two ports disposed in an arrangement as described in conjunction with Figure 2 may extend 21 through the outer cylindrical wall of the closed loop cavity 45 or 22 through one of the two conical walls thereof or through a combination 23 of the two walls. The embodiment shown in Figure 7 provides a 24 powerful advantage over those embodiments shown in Figures 4 and 5 in view that it does not employ any idler gears. Of course, the gear 26 ratio between the vane gears 42 and the stationary pinion gear 43 is 27 selected in such a way that the individual vane completes a full 28 revolution for every two full rotations of the rotor assembly.
29 In Figure 8 there is illustrated a gearing arrangement that may be employed in constructing a positive displacement apparatus of the 31 type shown in Figure 7, when the apparatus comprises relatively 32 many vanes and there is insufficient room to dispose all of the bevel 33 gears simultaneously engaging the stationary pinion bevel gear affixed 34 to the housing. In this particular arrangement of double layering of gearing, every other vane gear 46 engages a first stationary pinion 36 gear 47, while the remaining vane gears 48 engage the second 37 stationary pinion gear 49 coaxially disposed to the first pinion gear 38 47. Of course, the gearing ratios for both sets of gearing are ~ r~ ~
g 1 selected to attain the one to two rotary speed ratio between the 2 revolving motions of the vanes and the rotating motion of the rotor 3 assembly. It is readily recognized that the gearing arrangement may 4 employ a triple or quadruple layer design instead of the double layer design shown and described.
6 In Figure 9 there is illustrated a cross section of an embodi-7 ment of the internal combustion engine version of the positive 8 displcement apparatus of the present invention. An air intake port 9 50 to and an exhaust port 51 from the closed loop cavity 52 are included in the first half of the closed loop cavity 52 including 11 the section with the maximum cross sectional area thereof in such a 12 way that the rotating vanes pass the exhaust port 51 and the intake 13 port 50 in that order, while the fuel injection nozzle 53 and the 14 ignition device 54 are included in the second half of the closed loop cavity 52 including the section with the minimum cross sectional 16 area thereof in such a way that the rotating vanes pass the fuel 17 injection nozzle 53 and the ignition device 54 in that order. The 18 air entering through the intake port 50 may be precompressed by a 19 super- orturbo-charger of conventional design or a type employing one of the embodiments shown in Figures 4, 5 and 7, and the exhaust gas 21 discharged through the exhaust port 51 may run through a pneumatic 22 motor of a conventional design such as a turbine or a type 23 employing one of the embodiments shown in Figures 4, 5 and 7. An 24 embodiment of the positive displacement apparatus of the present invention applied as a compressor or pneumatic motor should have a 26 first port open to a first half of the closed loop cavity near the 27 section of the minimum cross sectional area of the closed loop 28 cavity, and the second port open to a second half of the closed 29 loop cavity near the section of the maximum cross sectional area thereof.
18 There are a number of inventions teaching the positive displacement 19 apparatus comprising a plurality of vanes operating under a compound combination of the revolving motion and the rotating motion. An 21 Australian patent (643/31) shows a pseudo-positive displacement 22 apparatus that employs a plurality of revolving-rotating vanes, but the 23 cross section of the closed loop cavity accommodating the vanes are not 24 varied to match the cross sectional areas thereof to the areas of sweep of the vanes. A U.S. patent (3,895,893) shows a similar apparatus 26 wherein the closed loop cavity is divided into two sections with two 27 different constant cross sectional areas, and the vanes are supported 28 by the rotor in a spring-biased arrangement whereby the individual vane 29 is forced to pivot about its own axis to conform with the cross sectional geometry of the closed loop cavity. A Japanese patent 31 application (63-279598) shows one of the more intelligent versions of 32 the apparatus wherein the vanes are pivoted over angles significantly 33 less than 90 degrees during each cycle of rotation thereof instead of 34 continuously revolving about the vane axis. These prior arts amount to an attempt to lasso a run-away train by throwing a rope. The positive 36 displacement fluid handling apparatus of the type under discussion, 37 whether they are applied as a flowmeter, a motor or engine, or a pump, 38 are subjected to a brutal loading by the fluid pressure and, - 2 - 2~
1 consequently, the apparatus employing anything less than 100 percent 2 positive mechanical motion coupling means do not have a chance to 3 actually work in the real world. The above-mentioned prior arts 4 employing the vanes under pivoting movements manipulated by the guiding surfaces such as the wall of the closed loop cavity or the 6 cam and cam follower combination are merely a few of many apparatus, 7 which lack the mechanical muscle and precision to be an actually 8 working positive displacement apparatus.
The primary object of the present invention is to provide a 11 positive displacement fluid handling apparatus comprising a plurality 12 of vanes disposed within and traveling through a closed loop cavity 13 (a toroidal cavity), wherein the individual vane revolves about its 14 own axis at one half of the rotating speed thereof about the axis of rotation of the rotor revolvably supporting the vanes whereby the 16 individual vane completes one full revolution about its own axis for 17 every two full rotations-aboutthe axis of rotation of the rotor. The 18 cross section of the closed loop cavity accommodating the vanes is 19 varied in such a way that the cross sectional areas of the closed loop cavity are closely matched to the areas of sweep of the vanes at all 21 angular locations about the axis of rotation.
22 Another object is to provide the apparatus described in the primary 23 object of the present invention, wherein the revolving motion of the 24 individual vane is coupled to the rotating motion thereof by a positively meshing gearing.
26 A further object is to provide the apparatus described in the 27 primary object of the present invention, wherein the axes of revolution 28 of the vanes are disposed on a conical surface coaxial to the axis of 29 rotation of the rotor revolvably supporting the vanes.
Yet another object is to provide the apparatus described in the 31 primary object of the present invention, wherein the axes of revolution 32 of the vanes are disposed on a plane perpendicular to the axis of 33 rotation of the rotor revolvably supporting the vanes.
34 Yet a further object is to provide the apparatus described in the primary object of the present invention, wherein the axes of revolution 36 of the vanes are disposed on a circular cylindrical surface coaxial to 37 the axis of rotation of the rotor revolvably supporting the vanes.
38 Still another object is to provide the apparatus described in the 1 primary object of the present invention, that includes means for 2 injecting fuel into the closed loop cavity accommodating the vanes and 3 means for igniting the fuel-air mixture therein, whereby the apparatus 4 works as an internal combustion engine.
These and other objects of the present invention will become 6 clear as the description thereof progresses.
8 The present invention may be described with a greater clarity and 9 specificity by referring to the following figures :
Figure 1 illustrates a developed view of a plurality of vanes 11 disposed within and traveling through a closed loop cavity, which 12 shows the operating principles of the present invention.
13 Figure 2 illustrates a cross section of an embodiment of the 14 positive displacement apparatus of the present invention.
Figure 3 illustrates a cross section of another embodiment of 16 the positive displacement apparatus of the present invention.
17 Figure 4 illustrates another cross section of the embodiment 18 shown in Figure 2.
19 Figure 5 illustrates another cross section of the embodiment shown in Figure 3.
21 Figure 6 illustrates a preferred embodiment of the gearing 22 coupling the revolving and rotating motions of the vanes to one 23 another.
24 Figure 7 illustrates a cross section of a further embodiment of the positive displacement apparatus of the present invention.
26 Figure 8 illustrates an embodiment of gearing usable in 27 constructing the embodiment shown in Figure 7.
28 Figure 9 illustrates an internal combustion engine version of 29 the present invention.
31 In Figure 1 there is illustrated a developed view of the 32 plurality of vanes I, 2, 3, 4, etc. disposed within and traveling 33 through a closed loop cavity (a toroidal cavity) 5. The plurality 34 of vanes are assembled into a rotor assembly of the positive displacement apparatus of the present invention, which rotor 36 assembly of a construction axisymmetric about the axis of rotation 37 thereof forms the core region surrounded by the closed loop cavity 38 5, wherein the individual vane I is supported by the rotor 1 revolvably about its own axis 6 (the axis of revolution) and 2 geared to the rotating motion of the rotor assembly about the axis 3 of rotation coinciding with the center axis of the closed loop cavity 4 5 in such a way that the individual vane revolves about its axis of revolution at one half of the angular velocity of the rotation of 6 the rotor assembly about the axis of rotation, whereby each of the 7 plurality of vanes completes full 360 degree revolution about the 8 respective axes of revolution for every 720 degree rotation of the 9 rotor assembly about the axis of rotation. The cross section of the closed loop cavity is varied between the maximum value at the 0 11 (360) degree section and the minimum value at the 180 degree section 12 in such a way that the cross sectional areas of the closed loop 13 cavity 5 are closely matched to the areas of sweep of the vanes at 14 all angular locations during the rotating motion. Two ports providing a flow passage for the fluid media are respectively open to 16 the two opposite halves of the closed loop cavity 5 located on the 17 two opposite sides of the plane of symmetry passing through the 0 18 (360) and 180 degree sections of the closed loop cavity 5. It is 19 readily noticed that the volume between two adjacent vanes increases in the first half of the closed loop cavity 5 that facilitates the 21 suction of the fluid media through the first port open to the first 22 half of the closed loop cavity 5, or the expansion of the gas in the 23 first half of the closed loop cavity 5 and discharge through the 24 first port, while the volume between two adjacent vanes decreases in the second half of the closed loop cavity 5 that facilitates the 26 discharge of the fluid media through the second port open to the 27 second half of the closed loop cavity 5, or the compression of gas 28 entering through the second port into the second half of the closed 29 loop cavity 5.
In Figure 2 there is illustrated a cross section of an embodi-31 ment of the positive displacement apparatus of the present invention, 32 wherein the axes of revolution of the plurality of vanes are disposed 33 on a plane perpendicular to the axis of rotation of the rotor 34 assembly. The plurality of vanes 7 disposed within and traveling through the closed loop cavity 8 are respectively supported by a 36 plurality of stub shafts 9 which are revolvably supported by the 37 rotor 10. Of course, the central axis of each of the stub shafts 9 38 defines the axis of rovolution of each of the vanes 7, while the axis ~ : ' ~ 3~ ?
1 of rotation of the vane assembly is defined by the central axis 11 2 of the rotor 10. The plurality of stub shafts 9 respectively 3 supporting the plurality of vanes 7 are disposed in a substantially 4 axisymmetrically radiating pattern from the axis 11 of rotation of the rotor 10 and respectively include a plurality of bevel gears 12 6 at the inner extremity thereof.The closed loop cavity 8 has the outer 7 cylindrical wall and two opposite side walls provided by the housing 8 structure 13, and the inner cylindrical wall provided by the rotor 10.
9 The apparatus works best when the outer and inner cylindrical walls respectively coincide with two spherical surfaces concentric to the 11 spherical center of the rotor assembly including the rotor 10 and the 12 vanes 7. The two opposite side walls of the closed loop cavity 8 are 13 curved in such a way that there is no or a little gap between the 14 surface of the vanes and the walls of the closed loop cavity 8 at all angular locations about the axis of rotation 11. In the versions of 16 the apparatus applied as flowmeters,hydraulic or pmeumatic motors or 17 pumps, two ports 14 and 15 are respectively open to the two opposite 18 halves of the closed loop cavity respectively located on the two 19 opposite sides of a plane of symmetry passing through the sections of the maximum and the minimum cross sectional area of the closed loop 21 cavity 8. In order to work as a positive displacement apparatus, 22 the two ports 14 and 15 must be separated from one another by two 23 diametrically oppositely located unbroken sections of the closed 24 loop cavity 8, wherein each section thereof includes at least one vane at all instances during the rotating motion of the vanes about 26 the axis 11 of rotation. The arrangement of the intake and discharge 27 ports in the internal combustion engine version of the apparatus is 28 shown in Figure 9.
29 In Figure 3 there is illustrated a cross section of another embodiment of the positive displacement apparatus of the present 31 invention, wherein the axes of revolution of the plurality of vanes 32 are disposed on a circular cylindrical surface coaxial to the axis 33 16 of rotation of the rotor assembly including one or two supporting 34 flanges coaxial to the axis 16 of rotation and a plurality of vanes 17 disposed therebetween and respectively supported by a plurality of 36 shafts 18, which shafts are revolvably supported by one or two 37 supporting flanges forming a part of the rotor assembly. Of course 38 the axis of revolution of each of the plurality of vanes 17 is defined z~
1 by the central axis of each of the plurality of shafts 18. A
2 plurality of tie-bars 19 disposed intermediate the two supporting 3 flanges in a parallel and axisymmetric pattern with respect to the 4 axis of rotation 16 structurally connect the two supporting flanges to one another. Of course, a rotor assembly employing a single 6 supporting flange would not need these tie-bars 19. The closed 7 loop cavity 20 has the outer and inner cylindrical walls provided by 8 the housing 21, and two opposite side walls provided by the two 9 supporting flanges. Of course, in an embodiment employing a single supporting flange, only one of the two opposite side walls of the 11 closed loop cavity 20 is provided by the supporting flange as the 12 other of the two opposite side walls is provided by the housing 21.
13 The outer and inner cylindrical wall of the closed loop cavity 20 are 14 spaced from one another in such a way that there is no or a little gap between the surfaces of the vanes 17 and the walls of the closed 16 loop cavity 20 at all instances during the rotating motion of the vanes 17 17 about the axis 16 of the rotation. The pair of ports 22 and 23 18 are included in the manner described in conjunction with the embodi-19 ment shown in Figure 2.
In Figure 4 there is illustrated another cross section of the 21 embodiment of the positive displacement apparatus shown in Figure 2, 22 which cross section is taken along plane 4-4 as shown in Figure 2.
23 The rotor assembly including the plurality of vanes 7 and the rotor 24 10 is supported by the rotor shaft 24, that is rotatably supported by the housing 13. The bevel gear 12 nonrotatably mounted on the 26 vane shaft 8 engages a stationary pinion bevel gear 25 disposed 27 coaxially to the axis 11 of rotation and affixed to the housing 28 13, wherein a plurality of idler bevel gears 26 disposed in an 29 axisymmetric arrangement with respect to the axis 11 of rotation and revolvably supported by the rotor 10 are employed in the gearing 31 engagement between the plurality of bevel gears 12 and the stationary 32 bevel gear 25. The ratio of the pitch diameters or the numbers of 33 gear teeth of the bevel gears 12, 25 and 26 are arranged in such a 34 way that the individual vane revolves about its axis of revolution at one half of the speed of rotation of the rotor assembly about the 36 axis 11 of rotation whereby the individual vane completes one full 37 revolution about its own axis of revolution for every two full 38 rotations of the rotor assembly about the axis 11 of rotation, which ~r~
1 requirement clearly explains why those idler bevel gears 26 have to 2 be employed. A vane motion detector 27 may be employed to measure 3 the speed of rotation of the rotor assembly as a measure of fluid 4 media passing through the apparatus. It is readily realized that the shaft 24 does not need to extend through and out of the housing 6 13 when the apparatus is applied as a flowmeter only.
7 In Figure 5 there is illustrated another cross section of the 8 embodiment of the postive displacement apparatus shown in Figure 3, 9 which cross section is taken along plane 5-5 as shown in Figure 3.
The rotor assembly including the two supporting flanges 28 and 29, 11 and the plurality of vanes 17 is supported by the rotor shaft 30, 12 that is rotatably supported about the axis 16 of rotation by the 13 housing 21. The plurality of vane shafts 18 respectively include 14 a plurality of gears 31, which engage the stationary pinion gear 32 through a plurality of idler gears 33 rotatably supported by the 16 rotor flanges. The stationary pinion gear 32 is disposed coaxially 17 to the axis 16 of rotation and affixed to the housing 21. The gearing 18 ratio of the gears 31, 32 and 33 are selected in such a way that the 19 individual vane 17 revolves about its own axis of revolution at one 20 half of the rotating speed of the rotor assembly about the axis 16 of 21 rotation whereby the individual vane completes a full revolution about 22 its own axis of revolution for every two full rotations of the rotor 23 assembly about the axis 16 of rotation. Of course, in an alternative 24 design, the second flange 29 and the stub vane shafts extending 25 thereinto may be omitted and its place filled up by the housing 26 structure 21.
27 In Figure 6 there is illustrated a schematic diagram showing an 28 arrangement of gearing that couples the revolving motion of the vanes 29 to the rotating motion of the rotor assembly in an one to two rotary 30 speed ratio. Each adjacent pair 34 and 35 of the plurality of vane 31 gears share a common idler gear 36 in engaging the stationary pinion 32 gear 37 affixed to the housing structure of the apparatus. This 33 particular embodiment of the gearing arrangement can be employed in 34 constructing the embodiments of the positive displacement apparatus 35 shown in Figures 4 and 5.
36 In Figure 7 there is illustrated a cross section of a further 37 embodiment of the positive displacement apparatus of the present 38 invention, wherein the axes of revolution of the vanes are disposed d ~ ~
1 on a conical surface coaxial to the axis 38 of rotation of the rotor 2 assembly. The plurality of stub shafts 39 respectively supporting 3 the plurality of vanes 40 are disposed on a conical surface coaxial to 4 the axis 38 of rotation in an axisymmetric arrangement and revolvably supported by the rotor 41, wherein the plurality of bevel 6 gears 42 nonrotatably mounted on the plurality of stub shafts 39 7 engage a stationary pinion bevel gear 42 directly without any idler 8 gears, which stationary pinion bevel gear 42 is disposed coaxially to 9 the axis 38 of rotation and affixed to the housing 44. The closed loop cavity 45 has the outer cylindrical wall and the two conical 11 side walls provided by the housing 44 and the inner cylindrical wall 12 provided by the rotor 41. The two conical walls of the closed loop 13 cavity 45 are arranged in such a way that there is no or a little 14 gap between the surfaces of the vanes 40 and the walls of the closed loop cavity 45 at all angular positions about the axis 38 of rotation.
16 The apparatus works best when the outer and inner cylindrical walls of 17 the closed loop cavity 45 respctively coincide with two spherical 18 surfaces concentric to the point of convergence of the axes of 19 revolution of the plurality of vanes 40. The two ports disposed in an arrangement as described in conjunction with Figure 2 may extend 21 through the outer cylindrical wall of the closed loop cavity 45 or 22 through one of the two conical walls thereof or through a combination 23 of the two walls. The embodiment shown in Figure 7 provides a 24 powerful advantage over those embodiments shown in Figures 4 and 5 in view that it does not employ any idler gears. Of course, the gear 26 ratio between the vane gears 42 and the stationary pinion gear 43 is 27 selected in such a way that the individual vane completes a full 28 revolution for every two full rotations of the rotor assembly.
29 In Figure 8 there is illustrated a gearing arrangement that may be employed in constructing a positive displacement apparatus of the 31 type shown in Figure 7, when the apparatus comprises relatively 32 many vanes and there is insufficient room to dispose all of the bevel 33 gears simultaneously engaging the stationary pinion bevel gear affixed 34 to the housing. In this particular arrangement of double layering of gearing, every other vane gear 46 engages a first stationary pinion 36 gear 47, while the remaining vane gears 48 engage the second 37 stationary pinion gear 49 coaxially disposed to the first pinion gear 38 47. Of course, the gearing ratios for both sets of gearing are ~ r~ ~
g 1 selected to attain the one to two rotary speed ratio between the 2 revolving motions of the vanes and the rotating motion of the rotor 3 assembly. It is readily recognized that the gearing arrangement may 4 employ a triple or quadruple layer design instead of the double layer design shown and described.
6 In Figure 9 there is illustrated a cross section of an embodi-7 ment of the internal combustion engine version of the positive 8 displcement apparatus of the present invention. An air intake port 9 50 to and an exhaust port 51 from the closed loop cavity 52 are included in the first half of the closed loop cavity 52 including 11 the section with the maximum cross sectional area thereof in such a 12 way that the rotating vanes pass the exhaust port 51 and the intake 13 port 50 in that order, while the fuel injection nozzle 53 and the 14 ignition device 54 are included in the second half of the closed loop cavity 52 including the section with the minimum cross sectional 16 area thereof in such a way that the rotating vanes pass the fuel 17 injection nozzle 53 and the ignition device 54 in that order. The 18 air entering through the intake port 50 may be precompressed by a 19 super- orturbo-charger of conventional design or a type employing one of the embodiments shown in Figures 4, 5 and 7, and the exhaust gas 21 discharged through the exhaust port 51 may run through a pneumatic 22 motor of a conventional design such as a turbine or a type 23 employing one of the embodiments shown in Figures 4, 5 and 7. An 24 embodiment of the positive displacement apparatus of the present invention applied as a compressor or pneumatic motor should have a 26 first port open to a first half of the closed loop cavity near the 27 section of the minimum cross sectional area of the closed loop 28 cavity, and the second port open to a second half of the closed 29 loop cavity near the section of the maximum cross sectional area thereof.
Claims (12)
1. An apparatus for executing a function related to flow of fluid comprising in combination :
a) a housing;
b) a rotor member with a shaft supported by the housing rotatably about an axis of rotation coinciding with the central axis of the shaft;
c) a closed loop cavity encircling the axis of rotation wherein at least a portion of wall of the closed loop cavity is provided by an annular surface encircling the axis of rotation and belonging to the rotor member, and the other portion of the wall of the closed loop cavity is provided by the housing, wherein the closed loop cavity has a cross sectional areas continuously varying from a maximum value at a first cross section substantially coinciding with a plane including the axis of rotation to a minimum value at a second cross section diametrically opposite to the first cross section across the axis of rotation, and has a cross sectional dimensions between two opposing portions of the wall of the closed loop cavity provided by the housing varying from a maximum value at said first cross section to a minimum value at said second cross section, and further has two ports respectively open to two opposite halves of the closed loop cavity respectively located on two opposite sides of said plane;
d) a plurality of vanes with width greater than thickness thereof disposed within the closed loop cavity in a distributed arrangement about the axis of rotation and respectively supported by a plurality of stub shafts disposed following said at least a portion of the wall of the closed loop cavity provided by the rotor member in a substantially axisymmetric arrangement about the axis of rotation and revolvably supported by the rotor member; and e) a plurality of rotary members with positively meshing teeth elements disposed coaxially to respective central axes thereof, each of said plurality of rotary members nonrotatably mounted on each of the plurality of stub shafts supporting the vanes, wherein each of the plurality of rotary members positively engages a stationary round member with positively meshing teeth elements disposed coaxially to the axis of rotation and affixed to the housing in such a way that each of the plurality of vanes revolves about the central axis of each of the plurality of stub shafts supporting the vanes at one half of the angular speed of rotation of the rotor member about the axis of rotation;
wherein cross sectional areas of the closed loop cavity is closely matched to areas of sweep of the vanes throughout the orbiting motions of the vanes about the axis of rotation in such a way that each of the plurality of vanes substantially fills up cross section of the closed loop cavity at all instances during orbiting motions of the vanes about the axis of rotation.
a) a housing;
b) a rotor member with a shaft supported by the housing rotatably about an axis of rotation coinciding with the central axis of the shaft;
c) a closed loop cavity encircling the axis of rotation wherein at least a portion of wall of the closed loop cavity is provided by an annular surface encircling the axis of rotation and belonging to the rotor member, and the other portion of the wall of the closed loop cavity is provided by the housing, wherein the closed loop cavity has a cross sectional areas continuously varying from a maximum value at a first cross section substantially coinciding with a plane including the axis of rotation to a minimum value at a second cross section diametrically opposite to the first cross section across the axis of rotation, and has a cross sectional dimensions between two opposing portions of the wall of the closed loop cavity provided by the housing varying from a maximum value at said first cross section to a minimum value at said second cross section, and further has two ports respectively open to two opposite halves of the closed loop cavity respectively located on two opposite sides of said plane;
d) a plurality of vanes with width greater than thickness thereof disposed within the closed loop cavity in a distributed arrangement about the axis of rotation and respectively supported by a plurality of stub shafts disposed following said at least a portion of the wall of the closed loop cavity provided by the rotor member in a substantially axisymmetric arrangement about the axis of rotation and revolvably supported by the rotor member; and e) a plurality of rotary members with positively meshing teeth elements disposed coaxially to respective central axes thereof, each of said plurality of rotary members nonrotatably mounted on each of the plurality of stub shafts supporting the vanes, wherein each of the plurality of rotary members positively engages a stationary round member with positively meshing teeth elements disposed coaxially to the axis of rotation and affixed to the housing in such a way that each of the plurality of vanes revolves about the central axis of each of the plurality of stub shafts supporting the vanes at one half of the angular speed of rotation of the rotor member about the axis of rotation;
wherein cross sectional areas of the closed loop cavity is closely matched to areas of sweep of the vanes throughout the orbiting motions of the vanes about the axis of rotation in such a way that each of the plurality of vanes substantially fills up cross section of the closed loop cavity at all instances during orbiting motions of the vanes about the axis of rotation.
2. An apparatus as defined in Claim 1 wherein the central axes of said plurality of stub shafts supporting the vanes are disposed on a plane perpendicular to the axis of rotation in a substantially axisymmetrically radiating pattern from the axis of rotation.
3. An apparatus as defined in Claim 2 wherein said at least a portion of the wall of the closed loop cavity provided by the rotor member includes an annular portion of a spherical surface with center coinciding with the point of convergence of the plurality of stub shafts, wherein said annular portion of the spherical surface constiuttes inner circumferential portion of the wall of the closed loop cavity.
4. An apparatus as defined in Claim 3 wherein outer circumfirential portion of the wall of the closed loop cavity includes an annular portion of a second spherical surface concentric to said a spherical surface.
5. An apparatus as defined in Claim 1 wherein the central axes of aid plurality of stub shafts supporting the vanes are disposed on a circular cylindrical surface coaxial to the axis of rotation in a parallel arrangement to the axis of rotation.
6. An apparatus as defined in Claim 5 wherein said at least a portion of the wall of the closed loop cavity provided by the rotor member includes a planar annular surface coaxial and perpendicular to the axis of rotation, wherein said planar annular surface constitutes one side portion of the wall of the closed loop cavity.
7. An apparatus as defined in Claim 6 wherein the other side portion of the wall of the closed loop cavity opposite to said one side portion thereof includes a planar annular surface coaxial and perpendicular to the axis of rotation.
8. An apparatus as defined in Claim 7 wherein said the other side portion of the wall of the closed loop cavity is also provided by the rotor member.
9. An apparatus as defined in Claim 1 wherein the central axes of said plurality of stub shafts supporting the vanes are disposed on a conical surface coaxial to the axis of rotation.
10.An apparatus as defined in Claim 9 wherein said at least a portion of the wall of the closed loop cavity provided by the rotor member includes an annualr portion of a spherical surface with center coinciding with the point of convergence of the plurality of stub shafts, wherein said annular portion of the spherical surface constitutes inner circumferential portion of the wall of the closed loop cavity.
11.An apparatus as defined in Claim 10 wherein outer circumferential portion of the wall of the closed loop cavity includes an annular portion of a second spherical surface concentric to said a spherical surface.
12.An internal combustion engine comprising in combination :
a) a housing;
b) a rotor member supported by the housing rotatably about an axis of rotation and including a power output shaft extending therefrom coaxially to the axis of rotation, c) a closed loop cavity encircling the axis of rotation wherein at least a portion of wall of the closed loop cavity is provided by an annular surface encircling the axis of rotation and belonging to the rotor member, and the other portion of the wall of the closed loop cavity is provided by the housing, wherein the closed loop cavity has cross sectional areas continuously varying from a maximum value at a first cross section substantially coinciding with a plane including the axis of rotation to a minimum value at a second cross section diametrically opposite to the first cross section across the axis of rotation, and has cross sectional dimensions between two opposing portions of the wall of the closed loop cavity provided by the housing varying from a maximum value at said first cross section to a minimum value at said second cross section, and further has an exhaust port and intake port open to a first half of the closed loop cavity including the section of the maximum cross sectional area in such a way that the vanes orbiting about the axis of rotation pass the exhaust port and the intake port in that order;
d) a plurality of vanes with width greater than thickness thereof disposed within the closed loop cavity in a distributed arrangement about the axis of rotation and respectively supported by a plurality of stub shafts disposed following said at least a portion of the wall of the closed loop cavity provided by the rotor member in a substantially axisymmetric arrangement about the axis of rotation and revolvably supported by the rotor member;
e) a plurality of rotary members with positively meshing teeth elements disposed coaxially to respective central axes thereof, each of said plurality of rotary members nonrotatably mounted on each of the plurality of stub shafts supporting the vanes, wherein each of the plurality of rotary members positively engages a stationary round member with positively meshing teeth elements disposed coaxially to the axis of rotation and affixed to the housing in such a way that each of the plurality of vanes revolves about the central axis of each of the plurality of stub shafts supporting the vanes at one half of the angular speed of rotation of the rotor member about the axis of rotation; and f) means for injecting fuel into the closed loop cavity and means for igniting fuel-air mixture contained in the closed loop cavity included in a second half of the closed loop cavity including the section of minimum cross sectional area in such a way that the vanes orbiting about the axis of rotation pass said means for injecting fuel and said means for igniting fuel-air mixture in that order;
wherein cross sectional areas of the closed loop cavity are closely matched to areas of sweep of the vanes throughout orbiting motions of the vanes about the axis of rotation in such a way that each of the plurality of vanes substantially fills up cross section of the closed loop cavity at all instances during orbiting motions of the vanes about the axis of rotation, and expanding volume of combusting fuel-air mixture rotates the combination of the plurality of vanes and the rotor member about the axis of rotation.
a) a housing;
b) a rotor member supported by the housing rotatably about an axis of rotation and including a power output shaft extending therefrom coaxially to the axis of rotation, c) a closed loop cavity encircling the axis of rotation wherein at least a portion of wall of the closed loop cavity is provided by an annular surface encircling the axis of rotation and belonging to the rotor member, and the other portion of the wall of the closed loop cavity is provided by the housing, wherein the closed loop cavity has cross sectional areas continuously varying from a maximum value at a first cross section substantially coinciding with a plane including the axis of rotation to a minimum value at a second cross section diametrically opposite to the first cross section across the axis of rotation, and has cross sectional dimensions between two opposing portions of the wall of the closed loop cavity provided by the housing varying from a maximum value at said first cross section to a minimum value at said second cross section, and further has an exhaust port and intake port open to a first half of the closed loop cavity including the section of the maximum cross sectional area in such a way that the vanes orbiting about the axis of rotation pass the exhaust port and the intake port in that order;
d) a plurality of vanes with width greater than thickness thereof disposed within the closed loop cavity in a distributed arrangement about the axis of rotation and respectively supported by a plurality of stub shafts disposed following said at least a portion of the wall of the closed loop cavity provided by the rotor member in a substantially axisymmetric arrangement about the axis of rotation and revolvably supported by the rotor member;
e) a plurality of rotary members with positively meshing teeth elements disposed coaxially to respective central axes thereof, each of said plurality of rotary members nonrotatably mounted on each of the plurality of stub shafts supporting the vanes, wherein each of the plurality of rotary members positively engages a stationary round member with positively meshing teeth elements disposed coaxially to the axis of rotation and affixed to the housing in such a way that each of the plurality of vanes revolves about the central axis of each of the plurality of stub shafts supporting the vanes at one half of the angular speed of rotation of the rotor member about the axis of rotation; and f) means for injecting fuel into the closed loop cavity and means for igniting fuel-air mixture contained in the closed loop cavity included in a second half of the closed loop cavity including the section of minimum cross sectional area in such a way that the vanes orbiting about the axis of rotation pass said means for injecting fuel and said means for igniting fuel-air mixture in that order;
wherein cross sectional areas of the closed loop cavity are closely matched to areas of sweep of the vanes throughout orbiting motions of the vanes about the axis of rotation in such a way that each of the plurality of vanes substantially fills up cross section of the closed loop cavity at all instances during orbiting motions of the vanes about the axis of rotation, and expanding volume of combusting fuel-air mixture rotates the combination of the plurality of vanes and the rotor member about the axis of rotation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002068302A CA2068302A1 (en) | 1992-05-08 | 1992-05-08 | Revolving-rotating vane meter-motor-pump |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002068302A CA2068302A1 (en) | 1992-05-08 | 1992-05-08 | Revolving-rotating vane meter-motor-pump |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2068302A1 true CA2068302A1 (en) | 1993-11-09 |
Family
ID=4149805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002068302A Abandoned CA2068302A1 (en) | 1992-05-08 | 1992-05-08 | Revolving-rotating vane meter-motor-pump |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2068302A1 (en) |
-
1992
- 1992-05-08 CA CA002068302A patent/CA2068302A1/en not_active Abandoned
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