ARRANGEMENT COMPRISING A ROTOR, A STATOR AND MEANS FOR MUTUAL POSITION DETECTION THEREOF

Abstract

The bearing assembly, consisting of a stator component (S1) and a rotor component (R1), where the rotor component is adapted for a back-and-forth oscillatory movement (P, −P) relative to the stator component, whereby a number of cavities (301 and 302; 303 and 304) coordinated along the outer periphery of the rotor component and the inner periphery of the stator component, formed with an increasing volume (301 and 302) and a decreasing volume (303 and 304), respectively, during rotation of the rotor component in an initial direction (P) from an initial position (IP) and towards a final position (FP), while the cavities allow the volumes to decrease and increase during a rotational motion of the rotor component in a second direction (−P) in relation to the stator component (S1). The invention specifies that the above-mentioned bearing arrangement is to be adapted to interact with an instrument (M1) in order to determine, with the help of at least two components, the momentary position of the rotor component in relation to the stator component.

Claims

1. A bearing arrangement, possessing a stator component and a rotor component where the rotor component is adapted for a back-and-forth oscillatory motion relative to the stator component, and along the outer periphery of the rotor component and inner periphery of the stator component there are a number of coordinated cavities formed with increasing volume and decreasing volume, respectively, during rotation of the rotor component in an initial direction from an initial position and towards a terminal position, while the cavities allow the volumes to decrease and increase during a rotational motion of the rotor component in a second direction in relation to the stator component, wherein the bearing arrangement is adapted to interact with an instrument in order to determine the momentary position of the rotor component in relation to the stator component.

2. A bearing arrangement according to claim 1, wherein the aforementioned instrument contains parts related to the stator and rotor components of the bearing arrangement.

3. A bearing arrangement according to claim 1, wherein the aforementioned instrument contains a first part coordinated with the stator component of the bearing arrangement.

4. A bearing arrangement according to claim 1, wherein the aforementioned instrument contains a second part assigned to the rotor component of the bearing arrangement in the form of a guide rail or guide curve, which is cylindrically-shaped with an axially-oriented extension.

5. A bearing arrangement according to claim 4, wherein the guide curve is oriented at an angle between 0 and 60 degrees, relative to a center line associated with the bearing arrangement.

6. A bearing arrangement according to claim 3, wherein an axially arranged and directed guide pin, movable back-and-forth, is set up to attach to and follow the guide rail and the guide curve during motion of the rotor component.

7. A bearing arrangement according to claim 6, wherein the guide pin's location in relation to the guide rail and the stator component is adapted to correspond to the rotating position of the rotor component in relation of the stator component.

8. A bearing arrangement according to claim 1, wherein a portion of an oil flow generated by oil pressure is transferred through a channel assigned to a stator component to a cavity with increasing volume, while oil compounds within a cavity with a decreasing volume press oil compounds through a shaped hole or holes in the stator component and alongside the cavity under compression.

9. A bearing arrangement according to claim 1, wherein a valve arrangement is connected to the first and second holes assigned to the stator component and allowed to supply and evacuate the oil compounds found in the cavity at an initial rotational movement and vice versa.

10. A bearing arrangement according to claim 1, wherein a number of cavities, referred to as primary, are adapted to be supplied with oil and oil compounds under pressure, and a number of cavities, referred to as secondary, are allowed to evacuate the oil or oil compounds contained therein, and the aforementioned evacuating oil portions are set to be supplied to the aforementioned valve arrangement via one or more conduits and/or channels.

11. An arrangement according to claim 9, wherein several primary cavities and several secondary cavities are distributed peripherally about the axis in the stator component and/or the rotor component.

12. An arrangement according to claim 11, wherein several primary cavities are coordinated via internal conduits for a serial and/or parallel oil supply.

13. An arrangement according to claim 11, wherein several secondary cavities are coordinated via internal conduits to direct evacuating oil compounds through the associated valve arrangement in a serial and/or parallel configuration.

14. An arrangement according to claim 11, wherein the aforementioned stator component is composed of several disc units or discs, where at least two are integrated or coordinated for interaction with an additional disc unit or disc.

15. An arrangement according to claim 14, wherein the aforementioned additional disc unit comprising the stator component is removably attached to the other disc units comprising the stator component.

16. An arrangement according to claim 1, wherein the channels assigned to the rotor component between the cavities occupy different planes.

17. An arrangement according to claim 4, wherein the guide rail or guide curve is helically-shaped.

18. An arrangement according to claim 5, wherein the angle is around 45 degrees.

19. An arrangement according to claim 9, wherein the valve arrangement is a two way valve arrangement.

Description

BR1EF FIGURE DESCR1PTIONS

[0044] The proposed designs, displaying the significant characteristics associated with the present invention, shall now for the purpose of providing an example be described in greater detail with reference to the attached drawings, in which:

[0045] FIG. 1 (corresponding to FIG. 9 in the aforementioned patent publication) allows a side view illustration of the bearing arrangement, consisting of three coordinated disc units in the shape of a reference circle as a stator component and a disc unit in the shape of a reference circle as a rotor component, where the stator and the rotor components with their centered holes are adapted to surround a rotating shaft, and where the stator and the rotor components comprise expanding and compressing cavities within the bearings, formed through interaction between the wings of the stator component and the oscillating rotor component,

[0046] FIG. 2 illustrates the bearing arrangement as per FIG. 1 in a plan view with the internal channels of the rotor component for bonding the expanding cavities and the internal channels of the rotor component for bonding the compressing cavities,

[0047] FIG. 3 shows and describes a lower peripheral section as per FIG. 1 and provides an illustration of a stator component made up of three disc units and a rotor component made up of a single disc unit as an initial design,

[0048] FIG. 4 shows and describes an upper part of the bearing arrangement in a second design where the stator component is composed of two disc units and the rotor component is composed of a disc unit. This figure also illustrates the existence of a means of determining the position of the rotor componentrelative to the stator component,

[0049] FIG. 5 shows the design in a side view as per FIG. 4 in a side view,

[0050] FIG. 6 shows and describes in a plan view the design from FIGS. 4 and 5

[0051] FIG. 7 shows and describes a cross-section A-A in FIG. 6,

[0052] FIG. 8 shows and describes a cross-section B-B in FIG. 6,

[0053] FIG. 9 shows the orientation of a cross-section C-C of a third design, where the assigned channels of the rotor component are oriented in different planes,

[0054] FIG. 10 shows and describes in a plan view the section C-C in FIG. 9 with a duct assigned to the rotor component on a first individual plane,

[0055] FIG. 11 shows a cross-section B-B of the aforementioned third design and the parallel cross-section CC with a duct assigned to the rotor component on a second individual plane,

[0056] FIG. 12 shows and describes in a plan view the section D-D in FIG. 11 and

[0057] FIG. 13 schematically shows a hydraulic circuit diagram of a proposed valve arrangement, by which, and with the valve arrangement in an initial position, one or more expanding cavities can be connected to an oil pump and one or more evacuating cavities can be connected to a tank and simultaneously be influenced to rotate the rotor component relative to the stator component in an initial direction, and where the valve arrangement can assume a second position (not shown) for the opposite function and rotational direction.

DESCR1PTION OF THE CURRENTLY PROPOSED DES1GNS

[0058] It should initially be emphasized that in the following description of the currently proposed designs, specific terms and expressions have been used for the purpose of clarification, while the interpretation of the principles of the invention may also include other terms and expressions.

[0059] The present invention will now be described in more detail by referencing the attached drawings in which three different design examples illustrate the characteristics of the invention.

[0060] Although the present invention is illustrated as a bearing arrangement, it should be taken into account that the invention can also be applied to a motor and/or pump with a rotor component assigned a motion in a back-and-forth direction.

[0061] Thus, FIG. 1 illustrates a bearing arrangement, A1, including the first design, presenting a stator component, S1, and a rotor component, R1, where the rotor component is adapted for a back-and-forth directional oscillatory motion, P, alternatively, −P, relative to the stator component.

[0062] Along the outer periphery of the rotor component, R1, and the inner periphery of the stator component, S1, there are, as per FIG. 2, a number of coordinated cavities, formed with an increasing volume 301, 302, at least in terms of volume, and a decreasing volume 303, 304, at least in terms of volume, during rotation of the rotor component in an initial direction, P, from an initial position, IP, and toward a terminal position, FP, while the cavities allow the volumes to decrease and increase during a rotary motion of the rotor component in a second direction, −P, in relation to the stator component, S1.

[0063] The bearing arrangement, A1, is adapted to interact with an instrument, M1, in FIG. 4, for determining the position of the rotor component, R1, relative to the stator component, S1.

[0064] The referred instrument, M1, contains parts related to the stator and rotor components of the bearing arrangement.

[0065] The instrument referred to, M1, contains a first part, M2, coordinated with the bearing arrangement's stator component, S1, while a second part, a guide rail or guide curve, M3, assigned to a rotor component, R1, is cylindrically-shaped with an axially-oriented small extension by which the guide curve takes on a mild helical form with a pitch of less than one revolution, such as 90 degrees.

[0066] The guide curve, M3, may be oriented at an angle between 0 and 60 degrees in relation to a 15′ center line associated with the bearing arrangement.

[0067] An axially-directed guide pin, M4, with a back-and-forth motion is adapted to attach to and follow the guide rail and guide curve during the reciprocal motion of the rotor component.

[0068] The location of the guide pin, M4, relative to the guide rail and the guide curve, M3, and the stator component, S1, is adapted to directly correspond to the rotational position of the rotor component relative to the stator component. It is proposed that the location of the guide pin, M4, be evaluated mechanically, electrically, or electronically in a circuit, M5, adapted to provide a value corresponding to the location of the guide pin, M4.

[0069] Herewith, not only does the valve arrangement, V10, control the back-and-forth oscillatory motion of the rotor component, but also the speed of the motion between the end positions or its amplitude via the supplied volume of oil compounds.

[0070] A portion of an oil flow generated by oil pressure in an oil pump, P10, is transferred, through a stator-assigned channel, 310, to a cavity, 301, with an increasing volume, while oil compounds in a cavity, 303, with a decreasing volume press oil compounds through a shaped hole or holes, 330, in the stator component, S1, and adjacent to the cavity under compression, 303.

[0071] FIG. 2 illustrates the existence of two serially connected cavities, 301 and 302, active during compression, connected via a channel, 350, assigned to a rotor component, while two serially connected cavities, 303 and 304, active during evacuation, are connected via a channel, 360, assigned to a rotor component.

[0072] The scope of the invention also includes the occurrence of one or more primary cavities, 301, along with one or more secondary cavities, 303, connected in a serial and/or parallel configuration.

[0073] The cavities, 301 and 302, are connected to the oil pump, P10, via a conduit, 310, while the cavities, 303 and 304, are connected to a tank, T10, via a conduit, 330. See FIG. 13.

[0074] A valve arrangement, V10, such as a two-way valve arrangement, is connected to the aforementioned holes, 310 and 330, assigned to stator components in order to supply and evacuate equal amounts of oil compounds associated with the cavity via an initial rotational movement and vice versa.

[0075] It is specifically disclosed that, while a number of cavities, 301 and 302, referred to as primary, are adapted to be supplied with, 310, oil and oil compounds under a specified pressure from a pump, P10, a number of cavities, 303 and 304, referred to as secondary, are allowed to evacuate the oil or oil compounds contained therein, and the aforementioned evacuating oil compounds are connected to the aforementioned tank, T10, via one or more conduits and/or channels, 330.

[0076] It is additionally proposed that several primary cavities and several secondary cavities are distributed peripherally about the axis in the stator component, S1, and/or the rotor component, R1.

[0077] FIG. 2 shows more specifically that the rotor component, R1, and disc, 14, are supplied with diametrically-oriented wings, 220 and 221, which are movable within the stator component, 51, between the wings, 210 and 211, that are related to the stator component. The peripheral length of the wings, 220 and 221, can of course be modified in order to cover a larger or smaller arc angle.

[0078] Several primary cavities, 301 and 302, are coordinated, through the internal conduits, 350, associated with the rotor component, shown in FIG. 2, for a more compact serial oil supply.

[0079] Several secondary cavities, 303 and 304, are coordinated, through the internal conduits, 360, associated with the rotor component, shown in FIG. 2, to serially direct the evacuating oil compounds through the outlet, 330, to an associated valve arrangement, V10.

[0080] FIGS. 1 and 4 show that the aforementioned stator component, S1, is composed of several disc units or discs, 11, 12, and 13, wherein at least two, 12 and 13, are integrated or coordinated, as per FIGS. 4 and 5, for interaction with an additional disc unit or disc, 11.

[0081] The aforementioned additional disc unit, 11, comprising the stator component is fixed but easily removable, for instance with the help of screws, 11a, attached to the other disc units, 12 and 13, comprising the stator component in order to enclose the rotor component, R1.

[0082] The present invention provides additional designs in FIGS. 4 to 13 which fall within the scope of the invention.

[0083] Thus, FIG. 4 shows and describes the upper part, A1a, of a bearing arrangement, A1, in a second design where the stator component, S1, is composed of two disc units, 12 and 13, and the rotor component, R1, is composed of a disc unit, 11. The figure also illustrates the presence of an instrument, M1, for determining the position of the rotor component relative to the stator component, S1, or the disc unit, 14.

[0084] It is also illustrated here that the instrument, M1, is set at an angle against the 15′ center line of the bearing arrangement which connects at or around a 45 degree angle and rests against a guide curve which is likewise oriented at 45 degrees from the 15′ center line.

[0085] FIG. 4 also illustrates the presence of three O-rings, 101, 102 and 103, which are assigned to bearing surfaces between the stator component, S1, and the rotor component, R1, and where the bearing surfaces, 105 and 106, are oriented in the same, or substantially the same, radial distance from the center line 15′.

[0086] The bearing surface, 105, has a shorter axial extension than the bearing surface, 106, which has been provided with two seals in the form of O-rings 102 and 103.

[0087] The guide disc, M3, with the guide curve is positioned adjacent to the O-ring, 101.

[0088] FIG. 5 shows the design in a side view and a section, as per FIG. 4, which employ the same reference numbers for the same details.

[0089] FIG. 6 shows and illustrates in a plan view the design in FIGS. 4 and 5, whereas FIG. 7 shows and describes a cross-section A-A in FIG. 6, while FIG. 8 shows and describes a cross-section B-B in FIG. 6.

[0090] FIG. 9 shows a cross-section C-C of a third design where the channels assigned to the rotor component are oriented in different planes and where FIG. 10 shows and describes in a plan view the section C-C in FIG. 9 with a duct assigned to the rotor component in a first plane, while FIG. 11 shows a cross-section D-D of the aforementioned third design and the related cross-section C-C with a duct assigned to the rotor component in a second plane.

[0091] FIG. 12 shows and describes in a plan view the section D-D in FIG. 11 with inlaid ducting.

[0092] FIG. 13 schematically shows a hydraulic circuit diagram of a valve arrangement, V10, through which, and with the valve arrangement in the illustrated initial position, one or more expanding cavities, 301 and 301, can be connected through the inlet, 310, to an oil pump, P10, and one or more evacuating cavities, 303 and 304, can be connected through the outlet, 330, to a tank, T10, and simultaneously prompted to rotate the rotor component, R1, relative to the stator component, S1, in an initial direction, P, whereby the valve arrangement can assume a second position (not shown) for an opposite direction of rotation, illustrated in FIG. 2 as −P.

[0093] In the above description the expanding and compressing cavities are designated in order to illustrate the motion of the rotor component in relation to the stator component, and it is apparent that during the reverse movement of the rotor component, a previously expanding cavity will serve as a compressing cavity and vice versa.

[0094] It should be noted that the stator component, S1, is provided with internal wings, 210 and 211, which in the designs, as a result of the number of cavities, are diametrically oriented, while the rotor component, R1, is provided with corresponding external wings, 220 and 221, where these pairs of wings are intended to define the cavities.

[0095] During the illustrated rotational motion of the rotor component, R1, designated “P”, cavities, 301 and 302, are expanding, while cavities, 303 and 304, are compressing an oil supply via a connection, 310, while the cavities, 303 and 304, are compressing to evacuate oil and oil compounds through the outlet, 330, communicating with the cavity, 303.

[0096] The cavities, 301 and 302, are serially connected via a first rotor-associated internal wiring harness, 350, while the cavities, 303 and 304, are serially connected via a second rotor-associated wiring harness, 360, whereby the bearing arrangement only requires one inlet, 310, and one outlet, 330, to rotate the rotor component in relation to the stator component between an initial position, IP, and a final position, FP.

[0097] The invention more specifically indicates that while a number of cavities, 301 and 302, referred to as primary, are adapted to be supplied with oil and oil compounds under pressure, a number of cavities, 303 and 304, referred to as secondary, are allowed to evacuate the enclosed amount of oil, and wherein the aforementioned evacuating amount of oil in the form of oil compounds can be fed to the valve arrangement via one or more conduits, 330.

[0098] Thus, it can be stated that by increasing the radian of the wings, 220 and 221, the amplitude of the oscillatory motion can be decreased, and/or by increasing the radian of the wings, 210 and 211, the amplitude of the oscillatory motion can be decreased.

[0099] The invention is not limited to the above-described designs, but may be modified within the scope of the present invention as it is defined in the first characterizing part of the following patent claim and/or in the sub-claims.