ROTARY BLADE ASSEMBLY THAT CAN BE USED IN TILE-CUTTING MACHINES
20210354330 · 2021-11-18
Inventors
Cpc classification
B28D1/225
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
The invention relates to a rotary blade assembly that can be used in tile-cutting machines, which has an annular blade (1) mounted on a bearing (2) comprising an inner race (21), and outer race (22) and ball bearings (23). A first side of the outer race (22) comprises a perimeter projection (24) that forms a stop for mounting the blade (1) on the bearing. A securing ring (3) that forms a second stop for mounting the blade (1) is mounted and secured on the second side of the outer race (22), the bearing and/or the securing ring comprising projections or recesses (31, 25, 26) which are coupled to complementary recesses or projections (11, 12) defined in the blade and which prevent the relative rotation of the blade (1) with respect to the securing ring (3) and the outer race (22) of the bearing (2).
Claims
1. A rotary blade assembly for use in tile-cutting machines, having an annular blade (1) mounted on a bearing (2) comprising an inner race (21), and outer race (22) and ball bearings (23) arranged between both races, a first side of the outer race (22) comprising a perimeter projection (24) that forms a first side stop for mounting the annular blade (1) on the bearing, the rotary blade assembly comprising: a securing ring (3) of the annular blade (1) mounted on a second side of the outer race (22) of the bearing, secured to said outer race (22) and that forms a second stop for mounting the annular blade (1); wherein the bearing and/or the securing ring comprise on a contact surface with the annular blade projections or recesses (31, 25, 26) which, in a mounting position of the assembly, are coupled to complementary recesses or projections (11, 12) defined in a corresponding contact surface of the annular blade, and prevent relative rotation of the annular blade (1) with respect to the securing ring (3) and the outer race (22) of the bearing (2).
2. The rotary blade assembly, according to claim 1, wherein the securing ring (3) and the outer race (22) of the bearing (2) are secured to each other by means of welding, micro-welding or interference (5).
3. The rotary blade assembly, according to claim 1, wherein the perimeter projection (24) of the outer race (22) of the bearing and the securing ring have thicknesses suitable for a centered arrangement of the annular blade with respect to the bearing.
4. The rotary blade assembly, according to claim 1, wherein the coupling projections (31) and the recesses (11) are defined on opposing side faces of the securing ring (3) and of the annular blade (1).
5. The rotary blade assembly, according to claim 1, wherein the projections (25) configured to be housed in the recesses (11) of the annular blade (1) are defined on the side of the outer race (22) of the bearing corresponding to the perimeter projection (24).
6. The rotary blade assembly, according to claim 1, wherein the recesses (11) defined in the annular blade (1) have a depth less than or equal to a total width of the annular blade (1).
7. The rotary blade assembly, according to claim 1, wherein the complementary projections and recesses in charge of preventing the relative rotation of the annular blade (1) with respect to the outer race (22) of the bearing (2) are arranged on surfaces that are faced in a radial direction of the annular blade (1) and of the outer race; defining complementary non-cylindrical shapes (26, 12).
8. The rotary blade assembly, according to claim 2, wherein the perimeter projection (24) of the outer race (22) of the bearing and the securing ring have thicknesses suitable for a centered arrangement of the annular blade with respect to the bearing.
9. The rotary blade assembly, according to claim 2, wherein the coupling projections (31) and the recesses (11) are defined on opposing side faces of the securing ring (3) and of the annular blade (1).
10. The rotary blade assembly, according to claim 3, wherein the coupling projections (31) and the recesses (11) are defined on opposing side faces of the securing ring (3) and of the annular blade (1).
11. The rotary blade assembly, according to claim 2, wherein the projections (25) configured to be housed in the recesses (11) of the annular blade (1) are defined on the side of the outer race (22) of the bearing corresponding to the perimeter projection (24).
12. The rotary blade assembly, according to claim 3, wherein the projections (25) configured to be housed in the recesses (11) of the annular blade (1) are defined on the side of the outer race (22) of the bearing corresponding to the perimeter projection (24).
13. The rotary blade assembly, according to claim 4, wherein the projections (25) configured to be housed in the recesses (11) of the annular blade (1) are defined on the side of the outer race (22) of the bearing corresponding to the perimeter projection (24).
14. The rotary blade assembly, according to claim 2, wherein the recesses (11) defined in the annular blade (1) have a depth less than or equal to a total width of the annular blade (1).
15. The rotary blade assembly, according to claim 3, wherein the recesses (11) defined in the annular blade (1) have a depth less than or equal to a total width of the annular blade (1).
16. The rotary blade assembly, according to claim 4, wherein the recesses (11) defined in the annular blade (1) have a depth less than or equal to a total width of the annular blade (1).
17. The rotary blade assembly, according to claim 5, wherein the recesses (11) defined in the annular blade (1) have a depth less than or equal to a total width of the annular blade (1).
18. The rotary blade assembly, according to claim 2, wherein the complementary projections and recesses in charge of preventing the relative rotation of the annular blade (1) with respect to the outer race (22) of the bearing (2) are arranged on surfaces that are faced in a radial direction of the annular blade (1) and of the outer race; defining complementary non-cylindrical shapes (26, 12).
19. The rotary blade assembly, according to claim 3, wherein the complementary projections and recesses in charge of preventing the relative rotation of the annular blade (1) with respect to the outer race (22) of the bearing (2) are arranged on surfaces that are faced in a radial direction of the annular blade (1) and of the outer race; defining complementary non-cylindrical shapes (26, 12).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0024] As a complement to the description provided herein, and for the purpose of helping to make the features of the invention more readily understandable, the present specification is accompanied by a set of drawings which, by way of illustration and not limitation, represent the following:
[0025]
[0026]
[0027]
[0028]
[0029]
[0030]
[0031]
DETAILED DESCRIPTION
[0032] In the exemplary embodiment shown in
[0033] In
[0034] The outer race (22) of the bearing has a cylindrical outer surface provided on a first side with a perimeter projection (24), in a radial direction, that forms a first side stop for mounting the blade (1) on the part.
[0035] The securing of the blade (1) in the mounting position represented in
[0036] As shown in
[0037] As can be seen in
[0038] In the variant embodiment shown in
[0039] It should be mentioned that the recesses (11) defined in the cutting disc (1) may have a depth less than the width of the blade (1), as shown in
[0040] In the variant embodiment shown in
[0041] Having sufficiently described the nature of the invention, in addition to a preferred exemplary embodiment, it is hereby stated for the relevant purposes that the materials, shape, size and layout of the described elements may be modified, provided that it does not imply altering the essential features of the invention claimed below.