Mechanism for moving a downward folding wing
11603687 · 2023-03-14
Assignee
Inventors
Cpc classification
E05F5/02
FIXED CONSTRUCTIONS
E05Y2800/21
FIXED CONSTRUCTIONS
E05Y2800/22
FIXED CONSTRUCTIONS
International classification
E05F1/08
FIXED CONSTRUCTIONS
E05F5/02
FIXED CONSTRUCTIONS
E05F1/12
FIXED CONSTRUCTIONS
Abstract
Mechanism for the movement of a wing of furniture with a downward folding opening, designed to be placed on one side of the furniture item, the mechanism being contained in a box consisting of two half-shells, and including a hinge including a plurality of levers, articulated one in relation to the other, to the box and to the wing for the movement of the latter, one of the levers being able to slide in a track formed in the box, another of the levers being able to rotate around a fulcrum point provided on the box and acting with one of its ends on the front side of a linear slider, the rear side of which acts on one end of a rocker lever, whose other end acts on.
Claims
1. A mechanism (100) for moving a furniture wing with a downward folding opening, designed to be placed on a side (4) of a piece of furniture (1), said mechanism being contained in a box (10) with two half-shells (11, 12), said mechanism comprising: a hinge (C) comprising a plurality of levers configured to articulate in relation to one another, to the box (10), and to the wing (6) for moving the wing, a first lever (L1) of said plurality of levers being configured to slide in a track (B) formed in the box (10), and a second lever (L2) of said plurality of levers being configured to rotate around a first fulcrum point (P1) provided on the box (10), a first end (22) of the second lever (L2) acting on a front side (31) of a first linear slider (30), a rear side (32) of the first linear slider (30) acting on a first end (33) of a rocker lever (34), and an opposing second end (35) of the rocker lever (34) acting on a second linear slider (40) subjected to an action of springs (42), first and second dampers being mounted on said first linear slider (30), the first damper (50) damping a final part of a descent stroke of the wing (6) during opening of the wing, and the second damper (60) damping a final part of an ascent stroke of the wing (6) during closure of the wing.
2. The mechanism according to claim 1, wherein said hinge (C) has three levers, the first and second levers (L1, L2) of the three levers configured to articulate one in relation to the other in an intermediate second fulcrum point (P2), a second end of the second lever (L2) opposite to said first end (22) of the second lever (L2) being articulated in a third fulcrum point (P3) at a first end of a third lever (L3), an opposing second end of the third lever (L3) being articulated in a fourth fulcrum point (P4) to an attachment (20) fixed to the wing (6), a first end of the first lever (L1) sliding with an end pin (27) in said track (B) formed in the box (10), and the first lever (L1) being articulated with an opposing second end of the first lever (L1) in a fifth fulcrum point (P5) to said attachment (20) fixed to the wing (6).
3. The mechanism according to claim 2, wherein said fourth and fifth fulcrum points (P4, P5) are provided in the attachment (20) fixed to the wing (6).
4. The mechanism according to claim 2, wherein said second lever (L2) carries a beak projection (70) which, during the closure of the wing (6), moves to abut against a pin (28) provided on the first slider (30), such that, in the case of a violent closing of the wing, the wing does not hit an upper shelf (3) of the piece of furniture.
5. The mechanism according to claim 2, wherein said front (31) and rear (32) sides of the first linear slider (30) have cam profiles.
6. The mechanism according to claim 5, wherein said springs (42) are compression springs which can be preloaded by means of a screw (44) acting on a mobile abutment (43).
7. The mechanism according to claim 2, wherein said springs (42) are compression springs which can be preloaded by means of a screw (44) acting on a mobile abutment (43).
8. The mechanism according to claim 2, wherein said track (B) formed on the box (10) is linear or curvilinear.
9. The mechanism according to claim 1, wherein said front (31) and rear (32) sides of the first linear slider (30) have cam profiles.
10. The mechanism according to claim 9, wherein said springs (42) are compression springs which can be preloaded by means of a screw (44) acting on a mobile abutment (43).
11. The mechanism according to claim 9, wherein said track (B) formed on the box (10) is linear or curvilinear.
12. The mechanism according to claim 2, wherein said fourth and fifth fulcrum points (P4, P5) are provided in the attachment (20) fixed to the wing (6).
13. The mechanism according to claim 1, wherein said springs (42) are compression springs which can be preloaded by means of a screw (44) acting on a mobile abutment (43).
14. The mechanism according to claim 13, wherein said damper (50) is actuated by a first end of a small lever (51) pivoted in a seventh point (P7) to said box (10), and a protrusion (52) of said first linear slider (30) acts upon a second end of the small lever (51), said first linear slider (30) moving rearwards during the opening of the wing.
15. The mechanism according to claim 14, wherein said second damper (60) is actuated by a stop (62) provided internally to the half-shells (11, 12) of the box (10), a stem (61) of the second damper (60) impacting against said stop (62) during a phase of advancing the first linear slider (30) during the closing of the wing (6).
16. The mechanism according to claim 14, wherein said track (B) formed on the box (10) is linear or curvilinear.
17. The mechanism according to claim 13, wherein said second damper (60) is actuated by a stop (62) provided internally to the half-shells (11, 12) of the box (10), a stem (61) of the second damper (60) impacting against said stop (62) during a phase of advancing the first linear slider (30) during the closing of the wing (6).
18. The mechanism according to claim 17, wherein said track (B) formed on the box (10) is linear or curvilinear.
19. The mechanism according to claim 13, wherein said track (B) formed on the box (10) is linear or curvilinear.
20. The mechanism according to claim 1, wherein said track (B) formed on the box (10) is linear or curvilinear.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Further features of the invention will be made clearer by the detailed description that follows, referred to one of its embodiments purely by way of a non-limiting example, illustrated in the accompanying drawings, in which:
(2)
(3)
(4)
(5)
DESCRIPTION OF THE PREFERRED EMBODIMENTS
(6)
(7) The movement mechanism according to the invention is denoted overall by reference numeral 100, and is attached on a side 4 of the furniture item. In
(8) Referring now to
(9) Hinge C consists of three levers L1, L2, L3.
(10) Levers L1 and L2 are articulated one in relation to the other in the fulcrum point P2, placed in an intermediate zone. Lever L2 is articulated at one end in the fulcrum point P3 at one end of lever L3, the other end of which is articulated in fulcrum point P4 to attachment 20, which is then fixed to the wing. One end of the lever L1 is also articulated at the attachment 20 fixed to the wing 6 in the fulcrum point P5, while the other end of the lever L1 carries a pin 27 sliding in a track B formed in box 10.
(11) Lever L2 is articulated in the fulcrum point P1 also restrained to box 10.
(12) The end of the lever L2 opposite the fulcrum point P3 carries a roller 22 that acts on a cam profile 31 of a slider 30 housed in the box 10 between the half-shells 11 and 12.
(13) The hinge C thus structured is forced, during the movement of the wing 6, to rotate around the fulcrum point P1 and to slide in the track B, formed in the two half-shells 11, 12 of box 10.
(14) Track B is shown as the linear type in the accompanying drawings, but it can also have a curved profile. In fact, by varying the position of the fulcrum point P1 and the shape of track B, it is possible to obtain different rotations of the wing 6, for example on the basis of the thickness of the latter.
(15) The functioning of the mechanism is now described, introducing on each occasion the essential elements that compose it.
(16) Referring to
(17) The rear part of slider 30, i.e. the part distal from hinge C, also has a cam profile 32, which acts on a roller 33 provided at one end of a rocker lever 34 hinged in a point P6 to box 10. The other end 35 of the rocker lever 34 acts on a slider 40 through a roller 41 carried by the latter.
(18) The slider 40 moves linearly and is under the action of springs 42 that abut against a striker 43, whose position is adjustable by means of a screw 44 in order to vary the compression of the springs and therefore the force that they develop, in order to adapt to wings of different height and weight, within a certain operating range.
(19) When the wing 6, under the action of its own weight, falls downwards, the springs 42, compressing themselves, contrast the fall thereof, reducing the speed of descent.
(20) The final part of the fall of the wing 6 is also cushioned through the action of a damper 50, integral with the slider 30. The damper 50 is operated by a small lever 51, which is hinged to box 10 in one of its intermediate points P7. During the backward stroke, slider 30 hits one end of small lever 51 with one of its rear projections 52 which, rotating around the fulcrum point P7, goes to compress with its other end the damper 50, thus obtaining the cushioned effect. The damping force of the damper 50 can be varied by varying the lever arms of small lever 51.
(21) During closure of the wing, the opposite effect is obtained.
(22) When, in fact, the wing 6 is raised, the springs 42 that had previously been compressed exert a thrust force on the rocker lever 34, which transmits it to the wing through the slider 30, which moves to the right. This allows a reduction in the lifting force that has to be applied to the wing in order to make it close. When wing 6 reaches about 22° of complete closure (
(23) During this closing phase, a second damper 60 intervenes, also carried integrally by the slider 30, so as to have a cushioned effect even during closure. In particular, when slider 30 slides forwards, to the right with reference to the drawings, it drags with it the damper 60, whose stem 61 impacts against a stop 62 provided on the half-shells 11 and 12 of box 10, thus compressing the damper 60.
(24) The slider 30 is guided by a slot 36 provided therein, in which is inserted a pin 37 integral with the box 10.
(25) The lever L2 has a beak protrusion 70 which, during closure of the wing (
(26) From what is disclosed the advantages of the mechanism for moving wings with downward folding according to the invention appear clear, which allows a gradual movement of the wing both during opening and closing and a damping of the same in the final phases of opening and closing.
(27) Naturally the invention is not limited to the particular embodiment previously described and illustrated in the accompanying drawings, but numerous detailed changes may be made thereto within reach of the person skilled in the art, without thereby departing from the scope of the invention itself, defined by the appended claims.