Lifting spindle arrangement for a retractable thruster unit of a marine vessel
11427292 · 2022-08-30
Assignee
Inventors
Cpc classification
F16H25/2015
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16H2025/2037
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B63H2025/425
PERFORMING OPERATIONS; TRANSPORTING
F16H2025/2031
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B63H5/125
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A lifting spindle arrangement is disclosed for a retractable thruster unit of a marine vessel, the lifting spindle having a lower end and an upper end and being supported at its lower end to a lower support structure by a lower support assembly and at its upper end to an upper support structure by an upper support assembly. The lifting spindle is provided at its both ends with a locking member for such a connection to the support structures such that each end of the lifting spindle may freely move in an axial direction away from the opposite end of the lifting spindle.
Claims
1. A retractable thruster unit for a marine vessel having a hull, the retractable thruster unit comprising: a lifting spindle arrangement, the lifting spindle arrangement having a lifting spindle, a lifting nut, and a motor, and having a lower end and an upper end and being supported at its lower end to a lower support structure by a lower support assembly and at its upper end to an upper support structure by an upper support assembly, wherein one of the lifting spindle and the lifting nut is fixed and the other one is rotatable for moving the retractable thruster unit and the lifting nut is arranged in cooperation with the lifting spindle vertically between the upper support structure and the lower support structure; and a lower locking member provided at the lower end of the lifting spindle and an upper locking member provided at the upper end of the lifting spindle, the lower locking member being configured to freely move in an axial direction downwards from the lower support structure, and the upper locking member being configured to freely move upwards from the upper support structure, resulting in that in all operating conditions a load subjected to the lifting spindle is tensile stress.
2. The retractable thruster unit as recited in claim 1, comprising: a lower axially resilient member arranged at the lower end of the lifting spindle between the lower locking member and the lower support structure; and an upper axially resilient member arranged at the upper end of the lifting spindle between the upper locking member and the upper support structure.
3. The retractable thruster unit as recited in claim 2, comprising: at least one lower bearing arranged between the lower locking member and the lower axially resilient member; and at least one upper bearing arranged between the upper locking member and the upper axially resilient member.
4. The retractable thruster unit as recited in claim 3, wherein the at least one lower bearing or the at least one upper bearing is a tapered roller bearing or a thrust ball bearing.
5. The retractable thruster unit as recited in claim 2, comprising: a lower casing arranged in connection with the lower support structure, and an upper casing arranged in connection with the upper support structure.
6. The retractable thruster unit as recited in claim 5, wherein the lower casing houses the lower axially resilient member, and the upper casing houses the upper axially resilient member.
7. The retractable thruster unit as recited in claim 6, comprising: at least one lower bearing arranged in the lower casing between the lower locking member and the lower axially resilient member; and at least one upper bearing arranged in the upper casing between the upper locking member and the upper axially resilient member.
8. The retractable thruster unit as recited in claim 7, wherein the at least one lower bearing or the at least one upper bearing is a tapered roller bearing or a thrust ball bearing.
9. The retractable thruster unit as recited in claim 7, wherein: the lower casing includes a top; the upper casing includes a bottom; the lower axially resilient member is arranged on the top of the lower casing, the at least one lower bearing being provided on the lower axially resilient member, the lower locking member being provided on a threaded section of the spindle, the threaded section being against the at least one lower bearing; and the upper axially resilient member is arranged on the bottom of the upper casing, the at least one upper bearing being provided on the upper axially resilient member, the upper locking member being provided on a threaded section of the spindle, the threaded section being against the at least one upper bearing.
10. The retractable thruster unit as recited in claim 9, wherein the lower locking member or the upper locking member is a nut.
11. A marine vessel comprising: a hull; and at least one retractable thruster unit according to claim 9, wherein at least one of the lower support structure and the upper support structure is the hull of the marine vessel.
12. The retractable thruster unit as recited in claim 1, comprising: at least one lower bearing arranged at the lower end of the lifting spindle between the lower locking member and the lower support structure; and at least one upper bearing arranged at the upper end of the lifting spindle between the upper locking member and the upper support structure.
13. The retractable thruster unit as recited in claim 12, wherein the at least one lower bearing or the at least one upper bearing is a tapered roller bearing or a thrust ball bearing.
14. The retractable thruster unit as recited in claim 1, wherein at least one of the lower locking member and the upper locking member is a nut.
15. A marine vessel comprising: a hull; and at least one retractable thruster unit according to claim 1, wherein at least one of the lower support structure and the upper support structure is the hull of the marine vessel.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) In the following, exemplary retractable thruster units of the present disclosure are explained in more detail in reference to the accompanying Figures, of which:
(2)
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DETAILED DESCRIPTION
(8) Exemplary embodiments as disclosed herein include a lifting spindle arrangement for a retractable thruster that has no or reduced risk of buckling.
(9) An exemplary retractable thruster unit for a marine vessel having a hull is disclosed with a retractable thruster unit including a lifting spindle arrangement, the lifting spindle arrangement having a lifting spindle, a lifting nut, and a motor, and having a lower end and an upper end and being supported at its lower end to a lower support structure by a lower support assembly and at its upper end to an upper support structure by an upper support assembly, wherein one of the lifting spindle and the lifting nut is fixed and the other one is rotary via the motor provided to rotate one of the lifting spindle and the lifting nut for moving the retractable thruster unit, the lifting spindle being provided at its both ends with locking members such that a lower locking member is able to freely move in an axial direction downwards from the lower support structure, and an upper locking member is able to freely move upwards from the upper support structure.
(10) Exemplary methods of moving a thruster unit in a marine vessel in a vertical direction via one or more lifting spindle arrangements are also disclosed, each lifting spindle arrangement including a lifting spindle, a lifting nut cooperating with the lifting spindle, a lower support assembly at a lower end the lifting spindle for connecting the lifting spindle to a lower support structure, an upper support assembly at an upper end the lifting spindle for connecting the lifting spindle to an upper support structure, one of the spindle and the lifting nut being fixed and the other one being rotary by means for rotating (e.g., a motor) one of the spindle and the lifting nut, the method including: initiating movement of the thruster unit by rotating one of the spindle and the lifting nut; and allowing the lower locking member to move freely in an axial direction downwards from the lower support structure and the upper locking member to move freely upwards from the upper support structure.
(11) Exemplary embodiments can provide a number of advantages, of which a few are listed in the following: Higher loads can be applied to a smaller diameter spindle. Compact build-in space with no parts in underwater area. No external locking required. Driven by electric motor. (Can be converted to hydraulic if requested.) Lower cost compared to other systems. Easy to build into vessel due to lighter, smaller and simpler components. Unlimited movement of the spindle at the ends of the spindle in a direction away from the thruster unit.
(12) However, it should be understood that the listed advantages are exemplary and optional, with varied embodiments offering advantages as desired.
(13)
(14) The thruster unit 10 illustrated in
(15) The motor base 14 is provided, in this exemplary embodiment of the present disclosure, with two arms 18 and 20 extending outwardly on opposite sides of the motor base 14. The arms 18 and 20 are, for example but not necessarily, at their outer ends opposite the motor base 14, each provided with a slide bearing 22 arranged to slide along a vertical guide post 24 when moving the thruster unit 10 up and down. The guide post 24 is fastened at both of its ends to the support structures 2 and 4. The arms 18 and 20 are each provided with a lifting nut 26 for cooperation with a spindle 28 arranged vertically between the support structures 2 and 4. The bearing 22 and the lifting nut 26 may be arranged directly to the arms 18 and 20, or, optionally, the arms may be provided with upper and lower support plates, 30′ and 30″, respectively, between which the bearing 22 and the lifting nut 26 are arranged.
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(19) When installing the spindle 28, or in general the thruster unit, in place, the lower end of the spindle 28 is pushed through the sealing ring 48 inside the lower casing 42, a set of disc springs 50 is positioned on the spindle 28 and against the bottom 44 of the casing 42. Next a bearing 52, such as a tapered roller bearing or a thrust ball bearing is positioned on the spindle 28 for carrying and centering the spindle 28 in relation to the inner wall 54 of the lower casing 42. The threaded end section of the spindle 28 is provided with a locking nut 56 for keeping the bearing and the set of disc springs in place on the spindle. The loosening of the locking nut 56 is prevented by means of one or more locking pins, keys or screws 58 positioned, for instance, at the interface between the spindle 28 and the locking nut 56.
(20) The coupling of the spindle 28 to the shaft 60 of the angular reduction gear (reference numeral 36 in
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(22) When assembling the upper support assembly the upper casing 72 is first provided with the sealing ring 78 in the opening 76 whereafter the upper casing 72 is installed at the upper end of the spindle 28 by pushing the upper casing 72 downwards such that the upper end of the spindle is inside the sealing 78. Thereafter a set of disc springs 80 is positioned on the spindle 28 and against the bottom 74 of the upper casing 72. Next a bearing 82, such as a tapered roller bearing or a thrust ball bearing is positioned on the spindle 28 for carrying and centering the spindle 28 in relation to the inner wall 84 of the upper casing 72. The threaded upper end of the spindle 28 is provided with a locking nut 86 by means of which the sets of cup springs 50 and 80, both at the upper and lower ends of the spindle 28, are compressed to a desired tightness, when installing the thruster unit in place in the hull of a marine vessel. When the desired tightness is reached the loosening of the locking nut 86 is prevented, for instance, by means of one or more locking pins, keys or screws 88 positioned at the interface between the spindle 28 and the locking nut 86. Thereafter, a fastening plate 4 (earlier referred to as a support structure) is provided so that the upper casing 72 and the upper end of the guide post 24 (if used) may be fastened thereto, whereafter the fastening plate may be attached to other support structures of the marine vessel.
(23) As may be understood in
(24) Referring to
(25) When dimensioning the spindle 28 and/or the shaft 60 of the angular reduction gear 36 care has to be taken to leave a sufficient gap between the ends of the spindle 28 and the shaft 36 such that the spindle 28 may move downwards until the upper set of disc springs 80 is fully compressed. A similar free area for a longitudinal or axial movement has to be reserved in connection with the coupling sleeve 62 or bushing and the lower end of the spindle 26 and the end of the shaft 60 of the angular reduction gear 36, too. By providing the opening shown in
(26) Via the discussed support assemblies and by providing free area in longitudinal or axial direction at both longitudinal or axial ends of the spindle, the spindle is arranged to “float” on the support of the sets of disc springs such that the spindle is always pre-tensioned and no matter from which direction the spindle is subjected to a load the spindle is never subjected to the risk of buckling but a tensile stress. In other words, even if the locking nuts 56 and 86 at the ends of the spindle 28 are, in the embodiment illustrated in
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(31) It is thus clear that in exemplary embodiments the spindles are always under tensile stress irrespective of the direction of the load. In case of positive load due to gravity the lower support assembly allows the lower end of the spindle to move freely axially downwardly until the disc springs in the upper casing are fully compressed, in other words the load is hanging in the support of the upper support assembly and has induced tensile stress in the spindle. Here, the word ‘freely’ means a situation where the end of the spindle is free to move in a certain direction, i.e. the end of the spindle is not provided with any means preventing its movement in that particular direction. In other words, the opposite end of the spindle may have, and in this case has, means for limiting the movement of the end in question, but not the end itself. In case of negative loads due to external forces such as the motion of the marine vessel or buoyancy the upper support assembly allows the spindle to move freely axially upwardly until the disc springs in the lower casing are fully compressed. In other words, in all above discussed operating conditions the load subjected to the spindles results in tensile stress and there is not the slightest risk of buckling.
(32) In view of the above it should also be understood that either the spindles may be driven with the lifting nuts fixed to the arms or support plates used for lifting the thruster unit, or the lifting nuts may be driven with the spindles fixed to the upper and lower support structures.
(33) With regard to the locking nuts it should be understood that they may not only be threaded nuts screwed onto threaded end sections of a spindle but they may be locking members provided with some kind of bayonet-fastening cooperating with a corresponding fastening means at the end sections of the spindle. Additionally, the locking members may be locked in place with different types of wedge and (possibly circumferential) groove connections or by arranging a pin running radially through appropriate openings provided in both the locking member and the end section of the spindle.
(34) As to the sets of disc springs they may be replaced with any such member that is resilient in the direction of the axis of the spindle including a set of coil springs or an annular ring of appropriate resilient material or a set of pads of appropriate resilient material like, for instance, rubber.
(35) With regard to the coupling of the ends of the spindle to the lower and upper support structures, it is possible, as another exemplary embodiment of the present disclosure, that the ends of the spindle are brought through holes in the support structures, resilient members are positioned on the support round the ends of the spindle and locking members provided at the ends of the spindle to keep the resilient members between the locking members and the support structures. If desired bearings may be arranged between the locking members and the resilient members.
(36) The lifting arrangement can include one or more spindles. In case of using more than 1 spindle, the synchronization between the spindles or lifting nuts may be achieved by various means and/or techniques, for example using synchronizing driveshaft or synchronizing chain, or using synchronous electric motors, using drive encoders and electronic compensation, etc. In a similar manner, various kinds of threaded rods and/or spindles may be used. For example, trapezoidal or other types of sliding threads, or ball & screw types of threads, which use a rolling connection instead of a sliding one can be used.
(37) It should be understood that exemplary descriptions of novel and inventive retractable thruster units have been disclosed. It should be understood that though the specification discusses a certain type of a retractable thruster unit, the type of the retractable thruster unit does not limit the invention to the types discussed. The above explanation should not be understood as limiting the invention as the entire scope of the invention is defined by the appended claims only. From the description herein it should be understood that separate features may be used in connection with other separate features even if such a combination has not been specifically shown in the description or in the drawings.
(38) Thus, it will be appreciated by those skilled in the art that the present invention can be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The presently disclosed embodiments are therefore considered in all respects to be illustrative and not restricted. The scope of the invention is indicated by the appended claims rather than the foregoing description and all changes that come within the meaning and range and equivalence thereof are intended to be embraced therein.