The subject of the present invention is a mechanism for moving a wing of a piece of furniture, in particular a wing with a downward folding opening.
The mechanisms for operating wings with downward folding, to which the present invention specifically relates, comprise a lever mechanism for operating a spring assembly, which is loaded when the wing is opened and discharged when it is closed, exerting a thrust that assists in the phase of rising of the wing.
The mechanisms for the above purposes available on the market are not completely satisfactory, either because they do not allow a gradual movement of the wing in the opening and closing phase, or because they cause knocks at the end of the opening and/or closing strokes of the wing.
Moreover, most of the time, these known mechanisms are of a rather complex design, and therefore expensive.
A lifting system for leaves of furniture that oscillate about at least one horizontal axis comprises a supporting body which can be connected to a fixed portion of the piece of furniture, a system of articulated levers with a first lever and a second lever which connect the supporting body to a leaf of the piece of furniture, and elastic actuation means which are functionally connected to the system of articulated levers in order to generate a rotation torque for the system of levers; the lifting system further comprises means which cooperate with the elastic actuation means in order to increase the rotation torque at least along a portion of the oscillation in the direction for opening the leaf.
The object of the invention is to eliminate the disadvantages of the prior art described above.
In particular, one of the objects of the invention is to provide a mechanism for moving a wing with a downward folding opening that allows a gradual movement of the wing, both in opening and in closing, with minimum effort by the user.
Another object of the invention is to provide such a mechanism that prevents the wing from slamming at the end of the opening and closing strokes.
Another object of the invention is to provide such a mechanism that is simple and economical to manufacture.
These and other objects of the invention are achieved by the mechanism of movement of downward folding herein disclosed and claimed.
Substantially, the mechanism for moving a furniture wing with a downward folding opening, designed to be placed on one side of the furniture item, is contained in a box consisting of two half-shells, and comprises a hinge comprising 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 said levers being able to slide in a track formed in the box, another of said levers being able to rotate around a point of fulcrum provided on the box and acting with one of its ends on the front side of a linear slider, whose rear side acts on one end of a rocker lever, whose other end acts on a second linear slider subjected to the action of springs, two dampers being mounted on said linear slider (30), one damper (50) damping the final part of the descent stroke of the wing (6) during opening, and one damper (60) damping the final part of the ascent stroke of the wing (6) during closure.
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:
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
Referring now to
Hinge C consists of three levers L1, L2, L3.
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.
Lever L2 is articulated in the fulcrum point P1 also restrained to box 10.
The end of the lever L2 opposite the fulcrum point P3 carries a roll 22 that acts on a cam profile 31 of a slider 30 housed in the box 10 between the half-shells 11 and 12.
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.
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.
The functioning of the mechanism is now described, introducing on each occasion the essential elements that compose it.
Referring to
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.
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.
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.
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.
During closure of the wing, the opposite effect is obtained.
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 (
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.
The slider 30 is guided by a slot 36 provided therein, in which is inserted a pin 37 integral with the box 10.
The lever L2 has a beak protrusion 70 which, during closure of the wing (
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.
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.
Number | Date | Country | Kind |
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102018000009883 | Oct 2018 | IT | national |
This application is the U.S. national phase of International Application No. PCT/EP2019/079077 filed Oct. 24, 2019 which designated the U.S. and claims priority to IT 102018000009883 filed Oct. 30, 2018, the entire contents of each of which are hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind |
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PCT/EP2019/079077 | 10/24/2019 | WO | 00 |