This application claims priority under the Paris Convention to French Patent Application No. FR 09 56140, filed on Sep. 9, 2009.
This invention relates to the mechanisms for adjusting the tilt of an automobile vehicle seat, the vehicle seats equipped with such mechanisms, and the manufacturing methods of such mechanisms.
More particularly, the invention concerns a mechanism for adjusting the tilt of an automobile vehicle seat comprising:
The document FR 2 578 601 describes an example of such a tilting adjustment mechanism. In this document, a ring is used, attached to one of the flanges, and crimped onto the other, to hold the two flanges together to prevent a relative movement thereof along the pivot direction.
However, it is still sought to improve such systems, and in particular to simplify them whilst maintaining their operational functions intact.
Consequently, a mechanism of the type in question is characterised in that the internal face of the first flange is opposite the external face of the second flange to guide a relative rotational movement of the first and second flanges around the pivot axis,
Thanks to these measures, the additional ring is no longer required, which reduces the supply and logistics problems for the parts, and reduces the number of assembly operations.
In certain embodiments, the following measures may also possibly be used:
According to another aspect, the invention concerns an automobile vehicle seat comprising a first element, a second element, and such a mechanism, wherein the first flange is fixed to the first element and the second flange is fixed to the second element.
According to another aspect, the invention concerns a manufacturing method for a mechanism for adjusting the tilt of an automobile vehicle seat in which:
In certain embodiments, it may be necessary to use one and/or the other of the following measures:
Other features and advantages of the invention will become clearer in the following description of one of its embodiments, provided by way of non-restrictive example, in reference to the attached drawings.
In the drawings:
a and 5b are two identical plane views at two successive steps of an assembly method, and
a and 6b are two cross sectional views according to the VI-VI line respectively in
In the different figures, the same references are used to designate identical or similar elements.
As shown diagrammatically in
The articulation mechanism 5 has for example a single level and may be commanded for example by means of a handle 6 which may be actuated in the direction 6a to release the pivoting of the seat back 4 around the main axis of rotation Y.
As illustrated in
The general form of the first flange 10 is a rigid disc, formed by stamping, which is fixed for example to the chair 2 of the seat. It features a bore extending along the main axis of rotation Y and forms a passage 18 for the command rod, and is connected to the handle 6.
It further comprises three circular shaped guiding elements 14, 15, 16 which are identical and are distributed on the periphery around the main axis of rotation, for example at 120°.
The first flange 10 further features three additional retaining elements 34, 35, 36 which are each respectively positioned circumferentially between two grains 11, 12, 13. These three elements are for example identical, only the element 34 will be described below: it features a first surface opposite a complementary surface of the grain 11 and a second surface opposite a complementary surface of the grain 12 (all cylindrical with a generating line parallel to the Y axis).
The first flange 10 thus has a central plate 50 that is substantially flat normal to the Y axis, featuring a front face 39 and a rear face 51 opposite. The guiding elements 14, 15, 16 and the retaining elements 34, 35, 36 are formed by stamping, so that they protrude with respect to the plane of the front face 39. Similarly, holding patterns may be formed, either protruding or depressed, in the rear face 51, for example to help attach the flange on an element frame of an automobile vehicle seat.
The first flange 10 also features a peripheral crown 9 featuring a cylindrical internal face 52 revolving around the Y axis, orientated towards this axis, and an opposite cylindrical external face 53 revolving around the Y axis, orientated opposite to this axis, and positioned further away from the axis than the internal face 52.
The peripheral crown 9 also features a front face 54 parallel to the front face 39 of the central plate 50, and which joins the inside 52 and external 53 faces.
As may be seen in
In the example presented, a through opening 58 is provided in a proximal region of the crown (i.e. close to the central plate). It extends radially in the crown 9, and is positioned longitudinally between the retaining element 42 and the central plate 50. Consequently, in certain angular sectors of the flange, the crown features an internal face that is purely cylindrical in the proximal and distal regions. In other angular sectors, they feature an opening in the proximal region then a retaining element in the distal region, positioned one after the other in the longitudinal direction when moving from the central plate to the front face.
However, such openings are not essential to the implementation of the invention.
The second flange 20 has the general form of a rigid disc, formed by stamping, which is fixed in this case to the seat back 4. It comprises a central plate 59 extending substantially in a plane that is normal to the Y axis, and which has a front face 60 and a rear face 61 opposite. The latter may feature attachment patterns, for example formed by stamping, to attach it to the seat back 4.
The second flange also features a peripheral crown 22 comprising an internal face 62 that is globally circumferential around the Y axis, and has a toothed segment equipped with teeth 24. An external face 63 is opposite the internal face, and has a smooth cylindrical geometry revolving around the Y axis, and with a radius that is substantially equal, slightly less than that of the internal face 52 of the crown 9 of the first flange. A front face 64 joins the internal 62 and external 63 faces, and extends for example normally to the Y axis.
The second flange also features a cylindrical bore with a circular section extending along the main axis of rotation Y and forming a passage 28 for the command rod.
The retaining elements 42 of the peripheral crown 9 of the first flange 10, which protrude radially towards the centre, retain the second flange 20 in the first flange 10, preventing relative translation of these two flanges along the Y axis whilst permitting their relative rotation around this axis.
In the assembled position, the front face 64 of the crown 22 of the second flange 20 is opposite the front face 50 of the first flange. The peripheral part of the rear face 61 of the second flange is opposite the retaining face 57 of the first flange 10. They are consequently situated directly opposite one another, with no intermediate parts or elements between them. The external face 63 of the crown 22 of the second flange 20 is opposite the internal face 52 and, where applicable, the openings 58 of the crown 9 of the first flange 10.
The actuation transfer element 30, or “cam”, has three hooks 31, 32, 33 and three actuation surfaces designed to engage with each of the respective locking elements 11, 12, 13. Each hook 31, 32, 33, is provided to release the grains.
The cam 30 is stationary to the rod and mobile in rotation around the main axis of rotation Y between a locked position and an unlocked position.
The cam 30 engages with the locking elements 11, 12, 13 in a plane extending perpendicularly to the main axis of rotation Y, such that the cam 30 does not extend in the direction of the main axis of rotation Y between the locking element 11, 12, 13 and the first flange 10, nor between the locking elements 11, 12, 13 and the second flange 20, but engages radially to the main axis of rotation Y with the locking elements 11, 12, 13.
A spring 7 tends to bring the cam 30 back to the locked position.
The locking elements 11, 12, 13 are positioned regularly (at 120°) in the first flange 10. They each comprise a toothed segment 11a, 12a, 13a, a guide portion 11b, 12b, 13b, a release pin 11c, 12c, 13c, and an actuation portion 11d, 12d, 13d.
Each guide portion features a guide surface that is complementary to an external face of the respective guide element 14, 15, 16.
In the active position, the cam presses against the actuation surface 11d, 12d, 13d of each of the locking elements 11, 12, 13, via the thrust surfaces, in order to maintain the locking elements in the active position.
In the active position of the locking elements, the toothed segments 11a, 12a, 13a engage with the teeth 24 of the toothed crown 22, in order to prevent the rotation between the first flange 10 and the second flange 20 around the main axis of rotation Y.
The engagement between the guide portions 11b, 12b, 13b and the guiding elements 14, 15, 16 enables a movement of the locking elements 11, 12, 13 in a plane that is normal to the Y axis between an active position and an inactive position. The faces of the locking elements 11, 12, 13 which are normal to the Y direction are in contact and slide on parallel front faces of the first and second flanges (Front face 39 of the first flange 10 and front face 60 of the second flange 12 as may be seen in
When the cam pivots from its locked position to its unlocked position from the action of the command rod (from the action of a user wishing to unlock the mechanism to adjust the relative orientation of the two flanges), the actuation surfaces disengage from the respective actuation surfaces 11d, 12d, 13d of the grains. Each of the retaining surfaces of the hooks 31, 32, 33 engage with the pin 11c, 12c, 13c of a respective grain 11, 12, 13 to bring said respective grain to the inactive position progressively as the pin is inserted 11c, 12c, 13c inside the hook.
When the user releases the handle, thus releasing the command rod 8, the spring 7 moves the cam 30 towards its active position. The hooks 31, 32, 33 of the cam disengage again from the pins 11c, 12c, 13c of the respective grains, then the actuation surface of the cam solicits the respective grains from their inactive position to their active position previously described. During this movement, the grains are guided by the engagement of the guide surfaces, until they reach the locked position previously described.
Even though this embodiment has been described in the context of a discontinuous adjustment mechanism with rotary grains, other embodiments may be envisaged by a person skilled in the art, provided that the two flanges are retained with one another in the Y direction, and are free to turn around this Y direction. For example, discontinuous mechanisms with sliding grains, or even continuous mechanisms with epicycloidal trains.
One example of an embodiment of a manufacturing method will now be provided in references to
Next, the two flanges are placed opposite one another, the front face 62 of the crown of the second flange 20 is opposite the front face 39 of the central plate of the first flange, and the external face 63 of the crown 22 of the second flange 20 is opposite the internal face 52. The insertion of the second flange in the first one is possible due to the fact that the retaining elements at this stage do not protrude. Beforehand, care has been taken to place all of the active elements of the system (cam, grains, spring, and others where applicable) between the flanges.
Next, as shown by the arrow A in
Where applicable, a deformation is made as shown by the arrow B in
Number | Date | Country | Kind |
---|---|---|---|
09 56140 | Sep 2009 | FR | national |
Number | Name | Date | Kind |
---|---|---|---|
4505515 | Wilking et al. | Mar 1985 | A |
5451096 | Droulon | Sep 1995 | A |
6112370 | Blanchard et al. | Sep 2000 | A |
7100986 | Uramichi et al. | Sep 2006 | B2 |
7140686 | Rohee | Nov 2006 | B2 |
7354109 | Oki | Apr 2008 | B2 |
7380882 | Oki | Jun 2008 | B2 |
7416255 | Yamada et al. | Aug 2008 | B2 |
20070040436 | Oki | Feb 2007 | A1 |
20100033004 | Reubeuze | Feb 2010 | A1 |
Number | Date | Country |
---|---|---|
2 153 751 | Nov 2008 | EP |
2 578 601 | Mar 1985 | FR |
2 872 105 | Jun 2004 | FR |
2 878 196 | Nov 2004 | FR |
2 890 913 | Sep 2005 | FR |
2 927 027 | Feb 2008 | FR |
WO-2008139851 | Nov 2008 | WO |
Entry |
---|
French Preliminary Search Report from priority application No. FR 09 56140; Report dated Apr. 23, 2010. |
Written Opinion from priority application No. FR. 09 56140. |
Japanese Office Action issued in related Japanese Application No. JP 2010-200799; action dated Sep. 12, 2012. |
Number | Date | Country | |
---|---|---|---|
20110057494 A1 | Mar 2011 | US |