The present invention relates to a lift.
An object of the invention is to provide a lift able to compensate deformations and misalignments, and hence prevent internal overloads on the various structural components.
Another object of the invention is to provide a lift able to assume a deformed geometry and/or to absorb unbalanced load s, while always remaining in equilibrium and without generating structural overloads.
These objects are attained according to the invention by a lift for motor vehicles as described hereinafter
The present invention is described in detail hereinafter with reference to the accompanying drawings, in which:
As can be seen from the figures, the lift of the invention comprises substantially a pair of runways 2 raisable from the floor by elevators indicated overall by 4, which in the illustrated embodiment are two in number.
Each elevator comprises a first upright 6, hinged to a hinging bracket 8 fixed to the workshop floor or to a base longitudinal member, the upright being hinged at its other end to a second upright 10 of the same length, which at its other end is hinged to a lug 12 provided on the runway 2.
Also hinged to the first upright 6 there is a first arm 14 hinged at its other end to a second arm 16, the other end of which is provided with rollers or slide blocks 18 slidable along guides 20 provided on the longitudinal members of the runways.
The second arm 16 is also hinged to the second upright 10 on a pin 22, such that the distance of the pin 22 from the lug 12 corresponds to the distance of the pin 22 from the roller 18.
Also hinged on the pin 22 is the end of a piston rod 24 of a cylinder-piston unit, of which the cylinder 26 is hinged on the pin 28 on which the first arm 14 is hinged to the first upright 6.
The first arm 14 is formed in two separate portions 14′, 14″ connected together by a compensation hydraulic cylinder-piston unit 30.
The cylinders 36 are fed via a flow synchronizer 32, which simultaneously ensures an equal movement of the piston rods 24 within the cylinders 26 and hence guarantees synchronism of movement of the runways 2 during lifting and descent.
The flow synchronizer 32 comprises substantially a base 34 on which four double acting cylinders 36 are mounted with their longitudinal axes parallel.
Each cylinder 36 is hinged at its bottom 38 to lugs 40 rigid with the base, the piston rod 42 of each cylinder having its free end hinged to a crank 44 rigid with a torsion bar 46 perpendicular to the longitudinal axis of the cylinders and hinged at its ends to brackets 48.
Each cylinder is provided with an entry conduit 50 for hydraulic fluid originating from a control center 52, and with an exit conduit 54 for feeding the hydraulic cylinder-piston units for raising the lift runways 2.
The lift of the invention operates in the following manner: when in its lowered condition, the hydraulic cylinder-piston units are in their condition of minimum elongation. Under these conditions, the vehicle (not shown in the drawings) can be driven onto the runways.
Operating fluid is then fed into the hydraulic cylinder-piston units via the synchronizer 32.
The hydraulic fluid fed by the control center 52 is distributed into the cylinders 36 from the bottom 38, to hence move the piston heads 56 and cause oil to leave through the conduits 54, to feed the hydraulic cylinder-piston units, with consequent rotation of the torsion bar 46 via the crank 44.
As the cylinder-piston units gradually lengthen, and by virtue of the particular choice of hinge points:
the uprights 6, 10, which when the lift is in its lowered configuration are practically coplanar, are rotated relative to each other, such that the angle formed between them increases,
the arms 14, 16 are also rotated relative to each other, such that the angle formed between them increases, and while the arm 14 rotates about the pin on which it is hinged to the arm 16, its other end slides with the roller 18 along the guide 20 in the sense of approaching the hinge 12.
The result is an upward translation of the runways 2 from the floor, while remaining parallel to this latter.
When the lift is subjected to an unbalanced load, the hydraulic cylinder-piston unit enables the two portions 14′, 14″ of the arm 14 to assume a deformed geometry and consequently absorb this unbalance.
It is apparent that if there is a non-uniform load distribution on the lift runways, the effect of the different pressure on the hydraulic cylinder-piston unit concerned will be to move the rod 42 of the corresponding piston, but as all the piston rods are connected together by the torsion bar 46, this movement will result in the synchronized movement of all the pistons of the bank.
In a different embodiment, the elastic element can be provided at the end of the second arm 24 supporting the roller 18.
In a further embodiment, the elastic element can consist of a slotted hole in which the end of the first upright 6 engages.
In a variant, not shown on the drawings, the uprights are hinged to longitudinal members resting on the floor.
In other variants, the elastic element, which can be of adjustable type, can consist of a wheel positioned at the end of the first upright or be inserted into the hinge pins of the first and/or second arm.
Number | Date | Country | Kind |
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VE2009A0051 | Sep 2009 | IT | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/EP2010/063182 | 9/8/2010 | WO | 00 | 3/13/2012 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2011/032872 | 3/24/2011 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
2471901 | Ross | May 1949 | A |
3246876 | Larson | Apr 1966 | A |
3891108 | Traficant | Jun 1975 | A |
4130178 | Smith, Jr. | Dec 1978 | A |
4815712 | Kawada | Mar 1989 | A |
5322143 | Curran | Jun 1994 | A |
5636711 | Nussbaum | Jun 1997 | A |
5695173 | Ochoa et al. | Dec 1997 | A |
6286629 | Saunders | Sep 2001 | B1 |
8052122 | Rossato et al. | Nov 2011 | B2 |
20010025952 | Wanner | Oct 2001 | A1 |
20100270523 | Schmitt et al. | Oct 2010 | A1 |
20120168701 | Rossato et al. | Jul 2012 | A1 |
Number | Date | Country |
---|---|---|
9414456 | Oct 1994 | DE |
19744519 | Dec 1998 | DE |
29916254 | Mar 2000 | DE |
453168 | Jun 1913 | FR |
2385638 | Oct 1978 | FR |
2503119 | Oct 1982 | FR |
2084543 | Apr 1982 | GB |
Number | Date | Country | |
---|---|---|---|
20120168701 A1 | Jul 2012 | US |