This invention relates to impeller mechanisms usable with machines such as engines, pumps, compressors and hydraulic motors.
Impellers, specifically traditional non-constrained vane machines involving reciprocating vanes according to the prior art suffer various disadvantages. In such machines the vane or vanes ride in a slot and are pushed outwardly via centrifugal force, fluid pressure, springs or a combination of these elements such that the vanes ride in direct contact with the bore of the machine. The efficiency of this class of vane machines, when used in a pump or a compressor for example, tends to be low due to friction, which also causes accelerated wear, thereby shortening machine life. Another class of vane machines, known as constrained vane machines, have mechanisms which control the motion of the vanes and prohibit them from running in direct contact with the bore of the machine. This reduces the aforementioned friction associated with non-constrained machines and consequently decreases wear and increases efficiency. However, the design of such machines is often complicated, with many moving parts, which limits the speed at which such impellers may run safely. Machine cost and reliability may also be adversely affected. There is a clear demand for improved impeller designs which do not suffer the manifest disadvantages of prior art devices.
The invention concerns impeller devices. In an example embodiment a device comprises a shaft defining a shaft axis. A cam is mounted on the shaft. The cam has a lobe projecting eccentric to the shaft axis. A plurality of projections are rotatably mounted on the cam. Each of the projections is pivotably mounted relative to the cam. A rotor surrounds the cam and is rotatable relatively thereto about the shaft axis. The rotor comprises a plurality of openings. Each of the openings receives one of the projections. Rotation of the rotor relatively to the cam causes the projections to rotate about the shaft axis while also reciprocating within the openings radially toward and away from the shaft axis.
In one example a plurality of rings surrounds the cam. Each one of the projections are pivotably attached to a respective one of the rings. The rings are rotatable relatively to the cam. Further by way of example, each ring comprises a ring lug extending therefrom. Each ring lug receives a respective pin having a pin axis oriented parallel to the shaft axis. Each projection comprises a projection lug extending therefrom. Each projection lug receives a respective one of the pins. Each of the projections is pivotable relative to one of the rings about one of the pin axes.
An example device further comprises a bearing mounted in the rotor concentric to the shaft. The bearing supports an end of the shaft proximate to the cam. A housing surrounds the rotor. The rotor extends from one end of the housing. The shaft is mounted on an opposite end of the housing. The rotor is rotatable relatively to the housing. By way of example the housing comprises a cylindrical surface facing the rotor. The cylindrical surface is coaxial with a housing axis and the housing axis is offset from the shaft axis. In a specific example embodiment the housing axis is offset from the shaft axis in a direction in which the lobe projects. Further by way of example the lobe is angularly positioned about the shaft with respect to the cylindrical surface so as to maintain an end of each the projection proximate to the cylindrical surface during reciprocal motion of the projections upon relative rotation between the rotor and the shaft.
An example embodiment further comprises first and second apertures in the housing. The apertures are oriented transversely to the shaft axis and angularly offset from one another about the cylinder axis. In an example embodiment a first bearing is positioned at the one end of the housing between the rotor and the housing, and a second bearing is positioned at the opposite end of the housing between the rotor and the housing. In an example embodiment each one of the projections comprises a vane having first and second oppositely arranged surfaces oriented parallel to the shaft axis. Further by way of example, each one of the openings comprises a slot, and each one of the slots receives a respective one of the vanes.
An example embodiment further comprises first and second apertures in the housing. The apertures are oriented transversely to the shaft axis and extend through the cylindrical surface. The apertures are angularly offset from one another about the cylinder axis. In a specific example embodiment the device comprises four of the vanes. In a further example each vane is oriented perpendicularly to an adjacent one of the vanes. By way of example the lobe is angularly positioned about the shaft with respect to the cylindrical surface so as to maintain an edge of each the vane proximate to the cylindrical surface during reciprocal motion of the projections upon relative rotation between the rotor and the shaft.
In an example embodiment each of the vanes comprises a respective seal extending along the edge. The seals contact the cylindrical surface continuously upon relative rotation between the rotor and the shaft. Another example embodiment comprises first and second end plates attached to the rotor in spaced relation to one another. The vanes are positioned between the end plates.
In a specific example the cam and the shaft are integrally formed. By way of example the rotor comprises a rotor body surrounding the cam. The openings are positioned in the rotor body. A rotor shaft is attached to one end of the rotor body and extends therefrom to define a rotor axis of rotation. A hub is attached to an opposite end of the rotor body. The hub is coaxially aligned with the rotor axis of rotation. In a specific example embodiment the openings comprise slots oriented parallel to the rotor axis of rotation.
The invention also comprises an example device, comprising a shaft defining a shaft axis. A cam is mounted on the shaft. The cam has a lobe projecting eccentric to the shaft axis. A plurality of vanes are rotatably mounted on the cam. Each vane is pivotably mounted relative to the cam. A rotor surrounds the cam and is rotatable relatively thereto about the shaft axis. The rotor comprises a plurality of slots. Each slot receives one of the vanes. Rotation of the rotor relatively to the cam causes the vanes to rotate about the shaft axis while also reciprocating within the slots radially toward and away from the shaft axis.
In the example embodiment each of the vanes has first and second oppositely arranged surfaces oriented parallel to the shaft axis. By way of example a plurality of rings surround the cam. Each vane is pivotably attached to a respective one of the rings. The rings are rotatable relatively to the cam.
In a specific example embodiment each ring comprises a ring lug extending therefrom. Each the ring lug receives a respective pin having a pin axis oriented parallel to the shaft axis. Each vane comprises a vane lug extending therefrom. Each vane lug receives a respective one of the pins. Each of the vanes is pivotable relative to one of the rings about one of the pin axes.
In a further example embodiment a bearing is mounted in the rotor concentric to the shaft. The bearing supports an end of the shaft proximate to the cam. An example embodiment further comprises a housing surrounding the rotor. The rotor extends from one end of the housing. The shaft is mounted on an opposite end of the housing. The rotor is rotatable relatively to the housing. By way of example the housing comprises a cylindrical surface facing the rotor. The cylindrical surface is coaxial with a housing axis. The housing axis is offset from the shaft axis. In a specific example embodiment the housing axis is offset from the shaft axis in a direction in which the lobe projects. Further by way of example the lobe is angularly oriented about the shaft with respect to the cylindrical surface so as to maintain an edge of each the vane proximate to the cylindrical surface during reciprocal motion of the vanes upon relative rotation between the rotor and the shaft.
In an example embodiment each of the vanes comprises a respective seal extending along the edge. The seals contact the cylindrical surface continuously upon relative rotation between the rotor and the shaft. Another example embodiment further comprises first and second apertures in the housing. The apertures are oriented transversely to the shaft axis and extend through the cylindrical surface. The apertures are angularly offset from one another about the cylinder axis.
An example embodiment of a device further comprises a first bearing positioned at the one end of the housing between the rotor and the housing. A second bearing is positioned at the opposite end of the housing between the rotor and the housing. A particular example embodiment comprises four of the vanes. By way of further example each vane is oriented perpendicularly to an adjacent one of the vanes. Again in an example embodiment, first and second end plates are attached to the rotor in spaced relation to one another. The vanes are positioned between the end plates.
In a specific example embodiment the cam and the shaft are integrally formed. Further by way of example the rotor comprises a rotor body surrounding the cam. The slots are positioned in the rotor body. A rotor shaft is attached to one end the rotor body and extends therefrom to define a rotor axis of rotation. A hub is attached to an opposite end of the rotor body. The hub is coaxially aligned with the rotor axis of rotation. By way of example the slots are oriented parallel to the rotor axis of rotation.
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As rotor 44 rotates concentrically about shaft axis 14 relatively to cam 16 the rings 34 rotate about the cam eccentrically relatively to the shaft axis 14. Each ring lug 40 thus traverses an eccentric orbit about the shaft axis 14. This eccentric orbit of the ring lugs 40 causes the vanes 26, attached to the rings via pins 36 and vane lugs 38, to reciprocate within in the slots 56 of rotor 44 toward and away from the shaft axis 14 as the rotor 44 rotates because the rotor rotates concentrically about the shaft axis 14, and the vanes 26 rotate eccentrically to the shaft axis. Because the vanes 26 are pivotably attached to the rings 34 via pins 36 the vanes can pivot as they rotate and thus they reciprocate radially toward and away from the shaft axis 14 (and the rotor axis of rotation 52) as they are constrained within respective slots 56 in the rotor body 48. The lobe 18 of cam 16 is angularly positioned about the shaft 12 with respect to the cylindrical surface 74 so as to maintain the edges 32 of vanes 26 proximate to the cylindrical surface during reciprocal motion of the vanes upon relative rotation between the rotor 44 and the shaft 12. For a practical design the phrase “proximate to the cylindrical surface” means that the separation distance between the edges 32 of the vanes 26 and the cylindrical surface 74 during rotation is always from about 0.0005 inches to about 0.25 inches. In designs for which an oil seal is impractical each vane 26 may also comprise a respective seal 84 extending along the edge 32 (see
Device 10 is versatile and may be used in many different applications. Rotor shaft 46 may be turned, for example, by an electric motor, driving the rotor 44. If aperture 76 is configured as an intake port and aperture 78 as an exhaust port then device 10 could operate as a pump or a compressor. Similarly, if high pressure fluid (liquid or gas) were pumped at pressure into aperture 78 to turn rotor shaft 46 before the fluid exits housing 68 through aperture 76 the device 10 could serve as a hydraulic motor or other fluid expansion device performing work. Additionally, the device 10 is also expected to be adaptable for use in a rotary engine using one of several thermodynamic cycles including, for example the Otto, Atkinson or Brayton cycles.
Devices such as 10 and 10a according to the invention represent a class of constrained vane machines wherein the vane's position is controlled by mechanisms other than the housing. It is expected that devices 10 and 10a will permit constrained vane machines of simpler design having fewer moving parts which will allow practical machines such as engines, pumps, compressors and hydraulic motors to operate more efficiently, at higher speeds, with less friction and wear than constrained vane machines according to the prior art.
This application is based upon and claims the benefit of priority to U.S. Provisional Application No. 62/218,254, filed Sep. 14, 2015 and hereby incorporated by reference.
Number | Date | Country | |
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62218254 | Sep 2015 | US |