Cabin lifter for a material transfer unit

10894698 ยท 2021-01-19

Assignee

Inventors

Cpc classification

International classification

Abstract

The present disclosure relates to a cabin lifter for a material transfer unit comprising at least one hydraulic cylinder supported in a damped manner. The present disclosure is further directed to a corresponding damping bush for damping the hydraulic cylinder and to a material transfer unit comprising a corresponding cabin lifter.

Claims

1. A cabin lifter for a material transfer unit comprising at least one hydraulic cylinder supported in a clamped manner for adjustment of the cabin lifter, wherein the hydraulic cylinder is extendable and retractable along an axis of operation of the hydraulic cylinder, and the hydraulic cylinder is supported via at least one damping bushing at the cabin lifter or at another section of the material transfer unit, the at least one damping bushing having at least one circular first recess positioned radially outward from a first leadthrough and radially inward from an outer perimeter of the damping bushing, the at least one first recess oriented to extend from a lower portion of the damping bushing to an upper portion of the damping bushing, the lower portion opposite the upper portion with the first leadthrough positioned therebetween, wherein the upper portion, the lower portion, and the first leadthrough are oriented along the axis of operation of the hydraulic cylinder, wherein the lower portion and the upper portion each include a web feature oriented along the axis of operation, wherein the damping bushing comprises at least one second recess radially positioned between the first recess and the first leadthrough, wherein the damping bushing comprises at least two symmetrically opposite recesses of said at least one first recess extending in a peripheral direction of the damping bushing, and wherein the damping bushing further comprises at least two of said second recess symmetrically opposed to one another.

2. The cabin lifter in accordance with claim 1, wherein the damping bushing is a rubber-metal bushing.

3. The cabin lifter in accordance with claim 1, wherein at least one damping bushing is supported at a ground side or at a bar side at the hydraulic cylinder.

4. The cabin lifter in accordance with claim 1, wherein the damping bushing is coupled to the cabin lifter or to another section of the material transfer unit by at least one bearing shell.

5. A damping bushing for a cabin lifter for a material transfer unit, wherein the cabin lifter comprises at least one hydraulic cylinder supported in a damped manner for the adjustment of the cabin lifter, wherein the hydraulic cylinder is extendable and retractable along an axis of operation of the hydraulic cylinder, and the hydraulic cylinder is supported via at least one damping bushing at the cabin lifter or at another section of the material transfer unit, and wherein the damping bushing comprises a first leadthrough arranged radially centrally wherein the at least one leadthrough is at least partly cylindrical, the at least one damping bushing having at least one circular first recess positioned radially outward from the first leadthrough and radially inward from an outer perimeter of the damping bushing, the at least one first recess oriented to extend from a lower portion of the damping bushing to an upper portion of the damping bushing, the lower portion opposite the upper portion with the first leadthrough positioned therebetween, wherein the upper portion, the lower portion, and the first leadthrough are oriented along the axis of operation of the hydraulic cylinder, wherein the lower portion and the upper portion each include, a web feature oriented along the axis of operation, wherein the damping bushing further comprises at least one second recess radially positioned between the first recess and the first leadthrough, wherein the damping bushing comprises at least two symmetrically opposite recesses of said at least one first recess extending in a peripheral direction of the damping bushing, and wherein the damping bushing further comprises at least two of said second recess symmetrically opposed to one another.

6. The damping bushing in accordance with claim 5, wherein the damping bushing comprises at least one second leadthrough disposed radially further outwardly than the first leadthrough.

7. The damping bushing in accordance with claim 6, wherein the at least one second leadthrough is oriented along an axis extending across a diameter of the first leadthrough and substantial parallel to the axis of operation of the hydraulic cylinder.

8. The damping bushing of claim 5, wherein the damping bushing is a rubber-metal bushing.

9. A material transfer unit for a cabin lifter, wherein the cabin lifter comprises at least one hydraulic cylinder supported in a damped manner for adjustment of the cabin lifter, wherein the hydraulic cylinder is extendable and retractable along an axis of operation of the hydraulic cylinder, and the hydraulic cylinder is supported via at least one damping bushing at the cabin lifter or at another section of the material transfer unit, the at least one damping bushing having at least one circular first recess positioned radially outward from a first leadthrough and radially inward from an outer perimeter of the damping bushing, the at least one first recess oriented to extend from a lower portion of the damping bushing to an upper portion of the damping bushing, the lower portion opposite the upper portion with the first leadthrough positioned therebetween, wherein the upper portion, the lower portion, and the first leadthrough are oriented along the axis of operation of the hydraulic cylinder, wherein the lower portion and the upper portion each include a web feature oriented along the axis of operation, wherein the damping bushing further comprises at least one second recess radially positioned between the first recess and the first leadthrough, wherein the damping bushing comprises at least two symmetrically opposite recesses of said at least one first recess extending in a peripheral direction of the damping bushing, and wherein the damping bushing further comprises at least two of said second recess symmetrically opposed to one another.

10. The cabin lifter of claim 1, wherein the at least two second recesses are separated from one another circumferentially by the web feature of the lower portion and the web feature of the upper portion.

11. The cabin lifter of claim 1, wherein the hydraulic cylinder is supported via two damping bushings, and wherein each damping bushing is coupled via a bearing shell.

12. The material transfer unit of claim 9, wherein the at least two second recesses are separated from one another circumferentially by the web feature of the lower portion and the web feature of the upper portion.

13. The damping bushing of claim 7, wherein the damping bushing comprises at least two symmetrically opposite second leadthroughs oriented along the axis extending across the diameter of the first leadthrough and parallel to the axis of operation of the hydraulic cylinder.

Description

BRIEF DESCRIPTION OF THE FIGURES

(1) FIG. 1 shows a part of a cabin lifter in accordance with the present disclosure with a hydraulic cylinder.

(2) FIGS. 2 and 3 show a cabin lifter in accordance with the present disclosure in a side view and in different pivot states.

(3) FIG. 4 shows a damping bush in accordance with the present disclosure.

DETAILED DESCRIPTION

(4) FIG. 1 shows a cabin lifter in accordance with the present disclosure for a material transfer unit comprising a hydraulic cylinder 1 that is coupled to a lower section of the cabin lifter via two damping bushes 2 in the embodiment of FIG. 1. Said lower section of the cabin lifter can be a connector or a connector section that is configured for coupling the cabin lifter to the remaining structure of a material transfer unit, not shown in more detail, and may comprise leadthroughs for said coupling.

(5) The damping bush 2 or the damping bushes 2 are provided at the ground side at the hydraulic cylinder 1 in the embodiment of the Figure.

(6) Provision can alternatively or additionally be made that one or more damping bushes 2 are provided at a bar-side coupling side of the hydraulic cylinder 1. This bar-side coupling point can, for example, be coupled to the sections of the cabin lifter shown in FIGS. 2 and 3.

(7) An embodiment of the cabin lifter is thus also conceivable in which, for example, four damping bushes 2 are provided for coupling the hydraulic cylinder 1 to the cabin lifter and/or to other structures of the material transfer unit. The damping bush 2 can accordingly be provided at the ground side and/or at the bar side at the hydraulic cylinder 1.

(8) As can be seen from FIG. 1, a bearing shell 3 or a plurality of bearing shells 3 can be provided for coupling the damping bush 2 or the damping bushes 2 to structures of the cabin lifter or to other sections of the material transfer unit.

(9) The bearing shells 3 can here have a depth that is no larger than the depth of the connector section at which the bearing shells 3 are provided.

(10) The bearing shell 3 or the bearing shells 3 may comprise cylindrical recesses or at least partly cylindrical recesses for receiving the damping bush 2. It is possible by means of the bearing shell 3, for example, to screw a damping bush 2 to the further structure of the cabin lifter and/or to the material transfer unit.

(11) As can further be seen from FIG. 1, the bearing shell 3 can, for example, comprise leadthroughs for fixing means such as screws. In the embodiment of FIG. 1, each bearing shell 3 or each component of the bearing shells 3 comprises exactly four leadthroughs for corresponding fixing means. Embodiments of the bearing shell 3 having a number of leadthroughs differing therefor are, however, also conceivable.

(12) The bearing shell 3 or the bearing shells 3 can be provided at the hydraulic cylinder 1 at both sides and may be arranged symmetrically to one another. The bearing shells 3 can furthermore be retrofitted to existing material transfer units and cabin lifters in accordance with the present disclosure can thus be simply retrofitted as required.

(13) It is also conceivable that the bearing shells 3 or parts of the bearing shells 3 are formed in one piece with components of the cabin lifter. At least a lower part of a bearing shell 3 may be produced in one piece with a lower section of the cabin lifter or can be welded to a lower section of the cabin lifter.

(14) FIGS. 2 and 3 show the cabin lifter in a position pivoted to the bottom (FIG. 2) and in a position pivoted substantially horizontally (FIG. 3). The cabin lifter can comprise a pedestal section 4 that is connected to a unit section 5 via, for example, a four-bar linkage 6 such that the pedestal section 4 is aligned horizontally in all pivot positions.

(15) FIG. 4 shows an enlarged plan view of a damping bush 2 that may be formed as a rubber-metal bush having at least two different lower sections. A lower section of the damping bush 2 can here be a rubber section consisting of rubber and another section can be a metal section.

(16) In one aspect, the rubber section of the damping bush 2 is supported within the metal section. The damping bush 2 can further comprise a leadthrough 21 that may be arranged radially centrally or also asymmetrically and that is at least partly cylindrical, through which leadthrough a coupling device can be led to couple the damping bush 2 to the hydraulic cylinder 1. At least one radial leadthrough 22 or 22 can be provided spaced apart radially outwardly therefrom that can be dimensioned in dependence on the desired damping properties of the damping bush.

(17) The upper second leadthrough 22 shown in the embodiment of FIG. 4 can have regions with radial extents of different amounts. A small radial extent of the leadthrough 22 may be provided in a middle region in the peripheral direction of the leadthrough 22. The outer regions of the leadthroughs 22 viewed in the peripheral direction can in contrast have larger radial extents, or vice versa.

(18) As can be recognized by the example of the lower second leadthrough 22, the second leadthrough 22 can also have a constant radial extent viewed in the peripheral direction. It is furthermore conceivable to provide differently dimensioned second leadthroughs 22, 22 and also different numbers of said second leadthroughs 22, 22 at a damping bush 2, depending on the desired elastic behavior of the damping bush 2.

(19) At least one first recess 23 extending substantially in the peripheral direction can be provided in a radially outer region, for example, in the rubber section of the damping bush 2, said first recess, for example, being able to be provided at the same radial spacing from the center axis of the damping bush 2 as the second leadthroughs 22, 22. The depth of the first recess 23 can be selected to influence the elastic behavior of the damping bush 2.

(20) A second recess 24 can furthermore be provided that at least partly extends in the peripheral direction and that can be arranged radially further inwardly than the first recess 23. Two or more second recesses 24 can furthermore be provided that can be separated from one another by means of webs 25. The webs 25 and the second recesses 24 can be differently dimensioned in dependence on the desired damping behaviors and can, for example, have different depths or widths.

(21) The damping bush 2 can be produced without parts movable relative to one another or with parts only movable elastically relative to one another. It is further conceivable that the damping bush 2 comprises two metal sections of which one is provided radially outwardly and one is provided radially inwardly, in the region of the first leadthrough 21. In one aspect, a metal section limits the first leadthrough 21 and/or is hollow cylindrical.

(22) The diameter of the first leadthrough 21 of the damping bush 2 can approximately correspond to the axial extent of the damping bush 2 and may be formed at least partly as hollow cylindrical. The difference between the diameter of the first leadthrough 21 and the axial extent of the damping bush 2 may comprise less than 50% of the respective longer dimension.