Lubricated sliding bearing with adjustment of the properties of the lubricant in certain parts of the bearing gap
11261912 · 2022-03-01
Assignee
Inventors
Cpc classification
F16C32/0666
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2210/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2326/30
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C32/0633
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C32/064
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/109
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/103
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C17/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C2210/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/106
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C33/743
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C29/025
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
The invention relates to a bearing device comprising a first surface and a second surface which are moveable relative to one another, wherein the first and second surfaces are separated by a bearing gap filled with a lubricant, which is a magnetorheological or electrorheological liquid, or a lubricant having a temperature dependent viscosity, or a lubricant having a controllable slip velocity. The bearing device further comprising one or more supply inlets in the first or second surface, and one or more activators embedded in the first surface or second surface and configured to locally increase a viscosity or decrease the slip velocity of the lubricant in at least one obstruction zone, thereby inhibiting a flow of the lubricant in the obstruction zone.
Claims
1. A hydrodynamic bearing device, comprising: a first bearing surface, a second bearing surface which faces the first bearing surface, wherein the first and second bearing surface are configured to rotate relative to one another about a main rotation axis, a bearing gap defined between the first and second bearing surface, wherein the first and second bearing surface are smooth and free of any surface texturing, the bearing gap being free of any abrupt changes in the height of the bearing gap, the bearing gap being filled with a lubricant, wherein the lubricant is a magnetorheological liquid or a lubricant having a controllable slip velocity, a plurality of activators embedded in the first or second bearing surface and configured to locally increase a viscosity of the lubricant or locally decrease the slip velocity in a plurality of obstruction zones, thereby inhibiting a flow of the lubricant through the bearing gap in each obstruction zone, and a plurality of non-obstruction zones in which the flow of the lubricant is not inhibited, wherein in a direction of relative movement between the first and second bearing surface the obstruction zones and non-obstruction zone are provided in turns, each non-obstruction zone being located upstream of an associated obstruction zone, wherein each obstruction zone has a curved or angular shape, wherein the curved or angular shape defines a top being directed downstream, wherein the obstruction zone is configured to cause, when the first and second surfaces move relative to one another, a local rise of a pressure of the lubricant within the bearing gap in the non-obstruction zone which is located upstream of each obstruction zone and in particular in a peak zone which is located directly upstream of each top by locally increasing the viscosity or locally decreasing the slip velocity in the obstruction zone and inhibiting the flow of the lubricant across each obstruction zone.
2. The hydrodynamic bearing device according to claim 1, wherein each obstruction zone comprises a left section and a right section which extend at an angle to a radial direction, wherein the left and right section direct the lubricant towards the peak zone.
3. The hydrodynamic bearing device according to claim 1, wherein each top is located in a central region of the first or second surface, wherein the tops are in particular located at a distance from an inner bearing end of the first or second surface, wherein the distance is 30-70 percent of a width of the first or second surface.
4. The hydrodynamic bearing device according to claim 1, being a thrust bearing device, wherein the first and second surface are flat and extend orthogonal to said main rotation axis, wherein the obstruction zones extend over a radial distance.
5. The hydrodynamic bearing device according to claim 1, wherein the first and second surface are annular and wherein the bearing gap is annular.
6. The hydrodynamic bearing device according to claim 1, wherein the obstructions zones have a V-shape or a U-shape.
7. The hydrodynamic bearing device according to claim 1, wherein the bearing device is a tilting pad bearing device and comprises a plurality of tilting pads which are tiltable, wherein the first surface comprises a plurality of first surface sections, each first surface section being associated with a tilting pad, and wherein the bearing gap comprises a plurality of bearing gap sections, each bearing gap section associated with a tilting pad, wherein each first surface section is smooth and free of any surface texturing, and each individual bearing gap section between a tilting pad and the opposed second surface is free of any abrupt changes in the height of the bearing gap, wherein each first surface section comprises an obstruction zone having a curved or angular shape, wherein the curved or angular shape defines a top being directed downstream, wherein the obstruction zone is configured to cause, when the first and second surfaces move relative to one another, a local rise of a pressure of the lubricant within the bearing gap in the non-obstruction zone which is located upstream of each obstruction zone and in particular in a peak zone which is located directly upstream of each top by locally increasing the viscosity or locally decreasing the slip velocity in the obstruction zone and inhibiting the flow of the lubricant across each obstruction zone.
8. A drive assembly, comprising: a shaft, wherein the shaft is supported by at least one bearing device according to claim 1.
9. The drive assembly according to claim 8, wherein the at least one bearing device further comprises a first bearing device, a second bearing device, and a third bearing device, wherein the shaft is supported by the first and second bearing devices as journal bearings, the first and second journal bearing devices positioning the shaft and providing support for the shaft in two independent radial directions, and the third device is a thrust bearing, the third thrust bearing device positioning the shaft and providing support for the shaft in an axial direction.
10. A vessel, comprising: a hull, an engine, a propeller, and a drive assembly of claim 8 which connects the engine with the propeller.
11. A bearing device, comprising: a first surface and a second surface which are moveable relative to one another and which face one another, wherein the first surface and second surface are separated by a bearing gap filled with a lubricant, wherein the lubricant is a magnetorheological liquid or a lubricant having a controllable slip velocity, one or more supply inlets in the first or second surface, each supply inlet configured to supply the lubricant from a pressurized liquid source to the bearing gap, and one or more activators embedded in the first or second surface and configured to locally increase the viscosity of the lubricant or locally decrease the slip velocity of the lubricant in at least one obstruction zone in the bearing gap, thereby locally inhibiting a flow of the lubricant through the bearing gap in the obstruction zone, wherein the bearing gap comprises at least one non-obstruction zone in which the flow of the lubricant is not inhibited, wherein each non-obstruction zone surrounds the associated supply inlet, wherein a flow path of the lubricant through the bearing gap is defined, which flow path starts at the at least one supply inlet, extends along the at least one non-obstruction zone, traverses the obstruction zone and ends at a bearing gap end, wherein the first surface and the second surface are free of surface texturing, in particular in the form of a land and pad, and are smooth and continuous and are without any abrupt changes in a height of the bearing gap, wherein the at least one obstruction zone either by itself or in cooperation with other obstruction zones encloses the at least one non-obstruction zone, wherein the lubricant having an increased viscosity or decreased slip velocity in the obstruction zone acts as an obstruction of the flow path and either by itself or in cooperation with lubricant with increased viscosity or decreased slip velocity in other obstruction zones inhibits the lubricant from flowing out of the non-obstruction zone and flowing out of the bearing gap through the bearing gap end, thereby increasing a pressure of the lubricant in the non-obstruction zone to a level which is sufficient to carry a load on the bearing device while preventing contact between the first and second surface.
12. The bearing device according to claim 11, wherein the activators are electromagnets or permanent magnets which create a magnetic field or are electric activators which can be electrically charged to create an electric field in the at least one obstruction zone.
13. The bearing device according to claim 11, comprising a plurality of non-obstruction zones, in particular thrcc non obstruction zones, each non-obstruction zone having a respective inlet, and a plurality of obstructions zones wherein each obstruction zone surrounds a non-obstruction zone with which it is associated and inhibits the lubricant from flowing out of the associated non-obstruction zone.
14. The bearing device according to claim 11, wherein the first and second surfaces are cylindrical or conical, the bearing device comprising multiple non-obstruction zones, each non-obstruction zone being surrounded by an obstruction zone, wherein each obstruction zone comprises a first axial part and a second axial part which extend over an axial distance, and a first circumferential part and a second circumferential part which extend over a circumferential distance, each obstruction zone comprising four corners which interconnect the first and second axial part and the first and second circumferential part.
15. A hydrodynamic bearing device, comprising: a first bearing surface, and a second bearing surface which faces the first bearing surface, wherein the first and second bearing surface are configured to rotate relative to one another about a main rotation axis, a bearing gap defined between the first and second bearing surface, the bearing gap being filled with a lubricant, wherein the lubricant is a magnetorheological liquid or a lubricant having a controllable slip velocity, a plurality of activators embedded in the first or second bearing surface and configured to locally increase a viscosity of the lubricant or locally decrease the slip velocity in a plurality of obstruction zones, thereby inhibiting a flow of the lubricant through the bearing gap in each obstruction zone, and a plurality of non-obstruction zones in which the flow of the lubricant is not inhibited, wherein in a direction of relative movement between the first and second bearing surface the obstruction zones and non-obstruction zone are provided in turns, each non-obstruction zone being located upstream of an associated obstruction zone, wherein each obstruction zone has a curved or angular shape, wherein the curved or angular shape defines a top being directed downstream, wherein the obstruction zone is configured to cause, when the first and second surfaces move relative to one another, a local rise of a pressure of the lubricant within the bearing gap in the non-obstruction zone which is located upstream of each obstruction zone and in particular in a peak zone which is located directly upstream of each top by locally increasing the viscosity or locally decreasing the slip velocity in the obstruction zone and inhibiting the flow of the lubricant across each obstruction zone, wherein the bearing device is a tilting pad bearing device and comprises a plurality of tilting pads which are tiltable, wherein the first surface comprises a plurality of first surface sections, each first surface section being associated with a tilting pad, and wherein the bearing gap comprises a plurality of bearing gap sections, each bearing gap section associated with a tilting pad, wherein each first surface section is smooth and free of any surface texturing, and each individual bearing gap section between a tilting pad and the opposed second surface is free of any abrupt changes in the height of the bearing gap, wherein each first surface section comprises an obstruction zone having a curved or angular shape, wherein the curved or angular shape defines a top being directed downstream, wherein the obstruction zone is configured to cause, when the first and second surfaces move relative to one another, a local rise of a pressure of the lubricant within the bearing gap in the non-obstruction zone which is located upstream of each obstruction zone and in particular in a peak zone which is located directly upstream of each top by locally increasing the viscosity or locally decreasing the slip velocity in the obstruction zone and inhibiting the flow of the lubricant across each obstruction zone.
Description
SHORT DESCRIPTION OF THE FIGURES
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DETAILED DESCRIPTION OF THE FIGURES
(28) Turning to
(29) The lubricant is a liquid. The lubricant is a magnetorheological liquid or an electrorheological liquid or a lubricant having a temperature dependent viscosity or a lubricant having a controllable slip velocity.
(30) The bearing device comprises one or more supply inlets 18 in the first or second surface. In this embodiment, the inlet is provide in the first surface 12, but it may be envisaged that the inlet is provided in the second surface. Each supply inlet is configured to supply lubricant from a pressurized liquid source to the bearing gap. The pressurized source will be present in case of a hydrostatic bearing device but is not considered a part of the present invention.
(31) The bearing device comprises one or more activators 20 embedded in the first surface 12 and configured to locally increase a viscosity of the lubricant in at least one obstruction zone 22 in the bearing gap, thereby inhibiting a flow of the lubricant through the bearing gap in the obstruction zone. The bearing gap comprises a non-obstruction zone 24 in which the flow of the lubricant is not inhibited. The non-obstruction zone comprises non-affected lubricant having a lower viscosity. The non-obstruction zone 24 surrounds the supply inlet 18. In this embodiment the non-obstruction zone 24 has a circular shape.
(32) An obstruction zone may be defined by multiple activators which are arranged adjacent to one another along a line. Each activator 20 and likewise each obstruction zone 24 comprises two radial parts 29A, 29B which extend radially and a circumferential section 33 which extend circumferentially. An outflow zone 35 is defined between each pair of radial parts 29 of adjoining obstruction zones.
(33) A flow path of the lubricant through the bearing gap is defined. The flow path starts at the at least one supply inlet 18, extends along the at least one non-obstruction zone 24, traverses the obstruction zone 22 and ends at a bearing gap end 26.
(34) Contrary to traditional hydrostatic bearing devices, the first surface 12 and the second surface 14 are free of surface texturing in the form of a land and pad and are smooth and continuous and are without any abrupt changes in the height of the bearing gap. An upper side of the activators 20 is flush with the rest of the first surface 12. This makes the bearing device relatively easy to manufacture and relatively robust.
(35) The obstruction zone 22 encloses the at least one non-obstruction zone 26 and inhibits the lubricant from leaving the non-obstruction zone by flowing across the obstruction zone 22 to the bearing gap end 26 and out of the bearing gap via the bearing gap end 26.
(36) Turning to
(37) The bearing gap end 26 is circumferential and extends around the bearing gap 16. In this embodiment, the bearing device only comprises an outer bearing gap end 26 and a non-obstruction zone 24 which is encircled by an annular obstruction zone 22 which inhibits the lubricant from flowing out of the bearing gap through the outer bearing gap end. As will be discussed with reference to other embodiment, the bearing device may also have more than one bearing gap end.
(38) The lubricant having an increased viscosity in the obstruction zone 22 acts as an obstruction of the flow path and either by itself or in cooperation with lubricant with increased viscosity in other obstruction zones inhibits the lubricant from leaving the at least one non-obstruction zone 26, thereby increasing a pressure of the lubricant in the non-obstruction zone to a level which is sufficient to carry a load on the bearing device and to prevent contact between the first and second surface.
(39) The activators may comprise electromagnets or permanent magnets which create a magnetic field. In another embodiment, the activators may comprise electric activators which can be electrically charged to create an electric field. In another embodiment, the activators are cooling elements configured to cool the lubricant in the at least one obstruction zone 22. In another embodiment used with a lubricant having a controllable slip velocity, the activators are electric activators which create an electric field, thereby orienting dipoles in the lubricant and controlling the slip velocity of the lubricant.
(40) Turning to
(41) In the shown embodiments of
(42) The bearing device of
(43) The bearing device may be free of any roller elements such as balls or cylindrical roller elements.
(44) Turning to
(45) The non-obstruction zones in the embodiment of
(46) The obstruction zones are spaced at regular angular intervals about a centre 31 and/or about a central axis 30, in particular at an angular interval of about 120 degrees.
(47) The embodiment of
(48) The source of pressure may be configured to provide independent pressures to the different non-obstruction zones. A control unit 101 may be provided to control the different pressures. Sensors 102 may also be provided. The sensors may include pressure sensors for the different non-obstruction zones. The sensors 102 may be located in or at the inlet openings 18. In case of pressure differences, the control unit 101 may increase the flow to one of the inlet openings 18 in order to restore the pressure equilibrium. Also, position sensors or orientation sensors may be provided. In case of tilting of the second surface, the tilting may be sensed by the sensors and an increase in pressure in or more of the non-obstruction zones may be provided by the control unit 101, resulting in a reversal of the tilting and in a re-alignment of the first and second surfaces.
(49) The bearing device may allow movement in two independent directions X, Y and provide support in a third direction Z. The bearing device may allow rotation about the Z-axis and prevent rotation about the X and Y axis.
(50) The skilled person will understand that this embodiment may be enlarged and comprise a multitude of non-obstruction zones surrounded by obstruction zones. Although the bearing device of
(51) Turning to
(52) The non-obstruction zones 24 have a square or rectangular shape, but different shapes are possible.
(53) Turning to
(54) Turning to
(55) Journal Bearing
(56) Turning to
(57) In another embodiment, the bearing device may be conical and in such a variant, the first and second surfaces are also conical.
(58) The bearing device comprises multiple non-obstruction zones 24A, 24B, 24C, 24D, 24E, in particular five. Five has an advantage in that tilting of the axis about the radial axes Y,Z can be supported by independent control of the pressure in the different non-obstruction zones. However, a different number than five is also possible. Each non-obstruction zone is surrounded by an obstruction zone 22A, 22B, 22C, 22D, 22E.
(59) Each obstruction zone comprises a first axial part A1 and a second axial part A2 which extend over an axial distance D1 and a first circumferential part C1 and a second circumferential part C2 which extend over a circumferential distance D2. Each obstruction zone comprises four corners 32 which interconnect the first and second axial part and the first and second circumferential part. This is indicated for the obstruction zone 22D only, but it will be clear that this is the same for the other obstruction zones.
(60) If the bearing device is conical, a similar configuration may be applied with a difference that the obstruction zones and non-obstruction zones will taper.
(61) In an embodiment, a control unit 101 may be provided and sensors 102 may be provided to sense a tilting of the axis about the radial axes Y,Z. The control unit may be coupled to the source of pressurized fluid or to control valves in conduits extending from the source of pressurized fluid to the inlets for individually controlling the pressure inside the non-obstruction zones. Additionally or alternatively, sensors may be provided which measure the position and/or orientation of the shaft relative to the inner surface and the control unit may be configured to control the pressures in the individual non-obstruction zones to control the position and/or orientation of the shaft relative to the inner surface.
(62) Thrust Bearing
(63) Turning to
(64) The first surface 12 and second surface are annular and extend around a main rotation axis 30 of the bearing. The main rotation axis 30 extends orthogonal to the first surface 12 and second surface.
(65) The bearing device 10 comprising an outer circumferential bearing end 26A and an inner circumferential bearing end 26B. The bearing device comprises at least one outer activator 20A which extends circumferentially and defines an outer obstruction zone 22A which inhibits the flow of lubricant from the at least one non-obstruction zone 24 to the outer circumferential bearing end 26A.
(66) The bearing device comprises at least one inner activator 20B which extend circumferentially and defines an inner obstruction zone 22B which inhibits the flow of lubricant from the at least one non-obstruction zone 24 to the inner circumferential bearing end 26B.
(67) The at least one non-obstruction zone 24 is annular and is located between the inner and outer obstruction zone.
(68) The bearing device comprises multiple supply inlets 18 in the first surface 12. This embodiment is a hydrostatic bearing device in that the pressure required to carry the load and prevent contact between the first and second surface is created by hydrostatic pressure.
(69) The circumferential obstruction zones 22A, 22B inhibit the lubricant from leaving the annular non-obstruction zone via the bearing gap ends 26A, 26B.
(70) Thrust Bearing Having a Plurality of Non-Obstruction Zones
(71) Turning to
(72) In this embodiment, the non-obstruction zones have the shape of an annulus segment. This embodiment allows individual pressure control in the different non-obstruction zones 24.
(73) Hydrodynamic Bearing
(74) Turning to
(75) A bearing gap is defined between the first and second bearing surface. The first and second bearing surface are smooth and free of any surface texturing. The bearing gap 16 is free of any abrupt changes in the height of the bearing gap. The bearing gap is filled with a lubricant, wherein the lubricant is a magnetorheological liquid or an electrorheological liquid or a lubricant having a temperature dependent viscosity.
(76) A plurality of activators 20 are embedded in the first (or second) bearing surface 12 and are configured to locally increase a viscosity of the lubricant in a plurality of obstruction zones 22. The effect of this is that a flow of the lubricant through the bearing gap is inhibited in each obstruction zone 22.
(77) The bearing device comprises a plurality of non-obstruction zones 24 in which the flow of the lubricant is not inhibited. In a circumferential direction the obstruction zones and non-obstruction zone are provided in turns, wherein each non-obstruction zone 24 is located between two obstruction zones 22.
(78) The effect of an obstruction zone is noticeable in the non-obstruction zone 24 which is upstream of the obstruction zone when considering the flow direction 34 (indicated with an arrow) of the lubricant relative to the obstruction zones 22. For instance the effect of obstruction zone 22J is felt in the non-obstruction zone 24J which is located upstream of the obstruction zone 22J.
(79) Each obstruction zone has a curved or angular shape. Each obstruction zone extends over a radial distance Dr which may be equal to a width W1 of the annular first or second surface.
(80) In case of an angular shape, the herringbone pattern shown in
(81) The curved or angular shape defines a top 36 which is directed downstream. The obstruction zone is configured to cause, when the first and second surfaces move relative to one another, a local rise of a pressure of the lubricant within the bearing gap in the non-obstruction zone 24 which is located upstream of each obstruction zone and in particular in a peak zone 38 of each obstruction zone 24 which is located directly upstream of each top 36 by locally increasing the viscosity in the obstruction zone and inhibiting the flow of the lubricant across each obstruction zone.
(82) Because of the curved or angular shape of the obstruction zones 24, the lubricant will be urged in a radial direction toward the peak zone, as indicated by arrows 40 in
(83) Each top 36 is located in a central region of the first surface 12, wherein the tops 38 are in particular located at a distance (A1) from an inner bearing end 26B, wherein the distance (A1) is 30-70 percent, more in particular 40-60 percent of a width (W1) of the first surface 12 or second surface.
(84) The obstruction zones may have a V-shape (herringbone arrangement) as shown in
(85) Turning to
(86) Turning to
(87) Turning to
(88) The hydrodynamic journal bearing device has a bearing length (L1). The bearing device has a bearing gap and has a first bearing gap end 26A and an opposite second bearing gap end 26B. The first bearing gap end 26A and the second bearing gap end 26B are located at opposite first and second bearing ends 40A, 40B.
(89) The bearing gap exists between the inward facing first bearing surface and the outward facing second surface. The first surface 12 and the second surface are smooth and continuous. The bearing gap is filled with a lubricant. The lubricant is a magnetorheological liquid or a electrorheological liquid or a lubricant having a temperature dependent viscosity.
(90) At least a first activator 20A and a second activator 20B are embedded in the first or second surface and are configured to locally increase a viscosity of the lubricant in a first and second obstruction zone 22A,22B in the bearing gap. When activated the first and second activator increase the viscosity of the lubricant in the first and second obstruction zone and inhibit the lubricant from flowing across the first and second obstruction zone.
(91) The first surface 12 and the second surface are free of surface texturing in the form of a land and pad and are smooth and continuous and are without any abrupt changes in the height of the bearing gap. The bearing gap comprises at least one non-obstruction zone 24 in which the flow of lubricant is not inhibited,
(92) The first and second bearing gap end 26A, 26B are annular and extend around the shaft and extend in a plane which is orthogonal to the longitudinal bearing axis 30.
(93) The first and second obstruction zones 22A, 22B are ring-shaped and are located at the opposite ends 40A, 40B of the journal bearing. The non-obstruction zone 24 is located between the first and second obstruction zone 22A, 22B.
(94) The first obstruction zone 22A inhibits the lubricant from reaching the first bearing gap end 26A and the second obstruction zone 22B inhibits the lubricant from reaching the second bearing gap end 26B. The first obstruction zone 22A and the second obstruction zone 22B together inhibit the lubricant from flowing out of the non-obstruction zone 24 and flowing out of the bearing gap through the bearing gap ends 26A, 26B.
(95) As in most hydrodynamic journal bearings, a height of the bearing gap may vary in a circumferential direction. If the axle is aligned with the cylindrical bearing member 13, a height of the bearing gap will be constant in an axial direction. However in practice a small misalignments may occur as a result of the loads on the axis.
(96) The bearing has a length L1 each obstruction zones has a width Woz. The width Woz of each obstruction zone is less than 10 percent of the length L1 of the bearing. This results in the non-obstruction zone 24 forming at least 80 percent of the length of the bearing.
(97) Turning to
(98) The shaft is supported by a first journal bearing device 10A and a second journal bearing device 10B, the first and second bearing device being a journal bearing device and providing support in a radial direction Y,Z, and a third, thrust bearing device 100 providing support in an axial direction X.
(99) The drive assembly may be used in various applications.
(100) Turning to
(101) The shaft is supported by the first journal bearing device 10A, the second journal bearing device 10B, the first and second journal bearing device providing support in two independent radial directions Y,Z, and by the third thrust bearing device providing support in an axial direction X.
(102) The engine further comprises a gear box 112, an outboard seal 114, an inboard seal 115. The seals 114, 115 prevent ingress of seawater 116. The engine 108 and the gear box 112 are positioned in an engine room 118, which may be separated from the rest of the inner volume of the vessel by one or more bullheads 120. The shaft 50 is generally located within a stern tube 122. The annular space 124 between the stern tube 122 and the shaft 50 may be filled with oil.
Further Embodiment
(103) Turning to
(104) In this embodiment, the primary activator 20 is a coil which extends around the inlet 18. The coil has a main axis 30. The anti-activator 44 also is a coil which extends around the inlet 18, the coil having a same main axis 30. When viewed in the X-direction (which extends parallel to the axes 30 of the coils), the primary activator 20 and the anti-activator 44 form concentric circles.
(105) The anti-actuators 44 have effect in a part of the non-obstruction zone, wherein said part is called an anti-obstruction zone 46. The non-obstruction zone 24 further comprises a non-influence zone 48 which is not under the influence of the primary activators or anti-activators, wherein at least one anti-obstruction zone is located adjacent an obstruction zone and between said obstruction and a non-influence zone.
(106) The activators 20 are electromagnets The bearing device further comprises at least one passive ferromagnetic member 60 configured for increasing the electromagnetic field.
(107) The coils 20, 44 are located underneath the first surface 12 and underneath a layer of material 28. An end 62 of said coil is located at a distance (Dc) from the first surface 12 underneath which the coil is located. The at least one ferromagnetic member comprises an inner member 64 located within the coil and an outer member 66 located outside the coil. The inner and outer member 64, 66 comprise respectively an inner projection 65 and an outer projection 67 which extend beyond the end 62 of the coil towards said first surface 12, An opening 70 is provided between said inner and outer projection. The area in the bearing gap 16 above said opening 70 is the obstruction area 22. The at least one obstruction zone 22 fully surrounds the at least one non-obstruction zone 24.
(108) Embodiment with Obstruction Zone within Non-Obstruction Zone
(109) Turning to
(110) The inner obstruction zone 22M has a beneficial effect of damping of possible vibrations (or resonance) of two bearing surfaces moving relative to one another in a direction orthogonal to the first surface 12. When the bearing surfaces move toward one another, a so called “squeeze flow” is created. The squeeze flow is a flow of lubricant from the inner obstruction zone 22M to the non-obstruction zone 24 and from the non-obstruction zone 24 through the obstruction zone 22 to the bearing gap end 26 and out of the bearing gap.
(111) The squeeze flow in itself is known in the field of bearing devices. However, with this embodiment, the lubricant in the bearing gap at the central obstruction zone 22M has an increased viscosity (or increased slip angle). As a result the squeeze flow will be obstructed and less lubricant will be squeezed out of the bearing gap. As a result better damping of the vibration or resonance will occur.
(112) Turning to
(113) In this embodiment, the direction of flow of the lubricant relative to the first surface 12 is indicated with arrow 34. The shape of the obstruction zone 22 is the same as discussed for the embodiment of
(114) The arrow 34 not only indicates the direction of flow of the lubricant relative to the first surface, but also indicates the direction of movement of the second surface relative to the first surface.
(115) The obstruction zone 22 has a top 36 which is “bottom” of the U-shape. Directly upstream of the top 36, a peak zone 38 is formed in the non-obstruction zone. In the peak zone 38, the pressure of the lubricant reaches a maximum.
(116) Although only one tilting pad 80 is shown, it will be clear that in a complete bearing device, there will be a plurality of tilting pads spaced about the axis of rotation. For instance there may be 3, 4, 6 or 8 tilting pads, but a different number is also possible. The first surface 12 of the tilting pad may be flat but may also be curved, in particular concave, as is known for tilting pads.
(117) In case of a thrust bearing, the tilting pads may also have the shape of a part of a ring shape. Together, the tilting pads form the ring shape.
(118) The skilled person will understand that between two adjoining tilting pads there is generally a non-supporting zone (or non-supporting gap). For the purpose of this document, these non-supporting zones are not considered part of the bearing gap. The feature evenness of the first and second surface applies to the individual first surface sections of the tilting pads. The feature of “free of any surface texturing” and “free of any abrupt changes in the height of the bearing gap” also applies to the individual sections formed by the tilting pads.
(119) The tilting pads need not be exactly square or rectangular. A trapezoid shape is also possible. The tilting pads 80 may have rounded corners.
(120) As required, detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention, which can be embodied in various forms. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a basis for the claims and as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriately detailed structure. Further, the terms and phrases used herein are not intended to be limiting, but rather, to provide an understandable description of the invention.
(121) The terms “a” or “an”, as used herein, are defined as one or more than one. The term plurality, as used herein, is defined as two or more than two. The term another, as used herein, is defined as at least a second or more. The terms including and/or having, as used herein, are defined as comprising (i.e., open language, not excluding other elements or steps). Any reference signs in the claims should not be construed as limiting the scope of the claims or the invention.
(122) The mere fact that certain measures are recited in mutually different dependent claims does not indicate that a combination of these measures cannot be used to advantage.