This application claims the benefit of priority under 35 U.S.C. ยง 119 to German Patent Application No. 10 2006 014 261 filed Mar. 28, 2006, the disclosure of which is incorporated herein by reference in its entirety.
The invention relates to an air guiding system for a vehicle, particularly for a passenger car, which is arranged in a rear area of the vehicle and comprises at least one central main air guiding element, which can be displaced from a moved-in inoperative position into a moved-out operative position, lateral auxiliary air guiding elements being displaceable together with the or each central main air guiding element.
DE 30 19 150 A1 shows a vehicle air guiding system arranged in an upper rear area of the vehicle and having an air guiding element that can be displaced from an inoperative position, in which it is integrated in the shaping of the rear area flush with the surface, into a moved-out operative position. The air guiding element is constructed as an aerofoil which, by way of an operating device, can be displaced or changed between the inoperative position into the operative position.
DE 43 05 090 A1 also discloses a vehicle air guiding system for a vehicle, arranged in a rear area of the vehicle and having an air guiding element that can be displaced from an inoperative position into a moved-out operative position. The air guiding element is formed by a rear spoiler arranged in a recessed receiving device of the vehicle body and can be displaced by an operating device between the inoperative position and the operative position.
The air guiding systems known from the above-mentioned DE 30 19 150 A1 and DE 43 05 090 A1 increase the rear axle output coefficient (cah-value) of the motor vehicle while maintaining the same or even improving the drag coefficient (cw-value) these known air guiding elements each having the same transverse dimension in the inoperative position and in the operative position.
Yet unpublished DE 10 2005 030 203, discloses a vehicle air guiding system having a central main air guiding element as well as two lateral auxiliary air guiding elements. The auxiliary air guiding elements allow the transverse dimension of the air guiding system to be enlarged in the operative position and particularly the rear axle output coefficient to be further increased. The adjusting movement of the lateral auxiliary air guiding elements with respect to the central main air guiding element takes place when the main air guiding element has been displaced from the inoperative position into the operative position. The adjustment of the auxiliary air guiding elements with respect to the main air guiding element therefore takes place after, and uncoupled from, the displacement of the main air guiding element.
An object of the present invention is to provide a novel vehicle air guiding system in which the auxiliary air guiding elements can essentially be linearly or translatorily adjusted with respect to the at least one main air guiding element in a direction transversely to the longitudinal direction of the vehicle in order to change these from an also moved-in inoperative position into an also moved-out operative position. Each auxiliary air guiding element is guided in a guiding device and is movable along the latter.
According to an advantageous further development of the invention, in the air guiding device according to the invention, the adjustment of the lateral auxiliary air guiding elements is coupled to the displacement of the at least one central main air guiding element during its or their change between the inoperative position and the operative position. Thereby, the lateral auxiliary air guiding elements can be changed isochronously or simultaneously with the displacement of the, or each, central main air guiding element with respect to the, or each, central main air guiding element from the inoperative position into the operative position and from the operative position into the inoperative position, respectively. In this case, the lateral auxiliary air guiding elements are adjusted with respect to the at least one central main air guiding element only linearly or translatorily transversely to the vehicle longitudinal direction. Within a very short time and in a simple manner, the transverse dimension of the air guiding system according to the invention can thereby be adapted.
Preferably, an operating device is associated with the auxiliary air guiding element for the latter's linear displacement with respect to the at least one central main air guiding element. A coupling device is applied to the respective operating device to couple the linear adjustment of the respective auxiliary air guiding element with respect to the at least one central main air guiding element to the displacement of the latter main air guiding element.
Other objects, advantages and novel features of the present invention will become apparent from the following detailed description of the invention when considered in conjunction with the accompanying drawings.
In the illustrated embodiment, the air guiding system 13 according to the invention has a central main air guiding element 14 as well as two lateral auxiliary air guiding elements 15, 16. One of the lateral auxiliary air guiding elements 15, 16, respectively, is arranged on each side of the central main air guiding element 14. The lateral auxiliary air guiding elements 15, 16 are visible only in the operative position (see
During the change or displacement from the inoperative position into the operative position or from the operative position into the inoperative position, the central main air guiding element 14 is swiveled and thereby lifted or lowered. The two auxiliary air guiding elements 15, 16 go along in this movement of the central main air guiding element 14.
In the illustrated preferred embodiment of the invention, the lateral auxiliary air guiding elements 15, 16 can isochronously or simultaneously with the swivel-type displacement of the central main air guiding element 14 from the inoperative position (see
According to
For the linear displacement or movement of the auxiliary air guiding element 15 illustrated in
Adjacent ends of the two operating rods 23, 24 are connected with one another in an articulated manner by a joint 25. The first joint rod 23 is also connected at the end situated opposite the joint 25 by a joint 26 with the lateral auxiliary air guiding element 15, whereas a second joint rod 24 is connected at the end situated opposite the joint 25 by a joint 27 with the central main air guiding element 14 in an articulated manner, particularly with the guide rail 21 of the guiding element arranged on the carrier element 17 of the central main air guiding element 14.
A comparison of
For coupling the linear motion of the lateral auxiliary air guiding element 15 with respect to the central main air guiding element 14 to the displacement of the central main air guiding element 14 from the inoperative position into the operative position or from the operative position into the inoperative position, a coupling device 28 comprised of a coupling element 29 is applied to the operating device 22 of the lateral auxiliary air guiding element 15.
In the following the coupling element 29 will be called a coupling rod, but can also be called a coupling guide rod. By way of a first end, the coupling rod 29 is applied via a joint 30 to one of the two operating rods 23, 24, respectively, and at an opposite second end, is applied via a joint 31 to the receiving device 19 of the vehicle body part 12 of the rear area 10. When the main air guiding element 14 is displaced by swiveling from the inoperative position illustrated in
The operating rods or joint rods 23, 24 provide a translation which is required for generating the path for the moving-out of the auxiliary air guiding elements 15, 16 from the rotating or swinging motion of the main air guiding element 14. If the adjustment of the main air guiding element 14 with respect to the receiving device 19 is large enough, the operating rods or joint rods 23, 24 can be eliminated and the coupling rods 29 can be linked by the joints 30 directly to the auxiliary air guiding elements 15 and 16.
As mentioned above, in the illustrated embodiment, the lateral auxiliary air guiding elements 15, 16 are covered in the inoperative position by the central main air guiding element 14 and are therefore not visible. As an alternative, it is also contemplated that the auxiliary air guiding elements 15, 16 are visible in the inoperative position, by being arranged above a covering element 18 of the main air guiding element 14.
In the illustrated embodiment, the coupling between the displacement of the main air guiding element 14 and the displacement of the auxiliary air guiding elements 15, 16 is implemented mechanically by the coupling device 28. In this case, only a single drive will be required for the air guiding system 13.
As an alternative, it is also contemplated to associate a separate drive to the auxiliary air guiding element for their adjustment. Then, the coupling between the displacement of the main air guiding element and the linear displacement of the auxiliary air guiding elements with respect to the main air guiding element does not take place mechanically as shown in
Furthermore, it is pointed out that the operating device 22 for the linear displacement of the auxiliary air guiding elements 15, 16 with respect to the main air guiding element 14, in contrast to the illustrated embodiment, can also be provided by way of a four-bar linkage.
The foregoing disclosure has been set forth merely to illustrate the invention and is not intended to be limiting. Since modifications of the disclosed embodiments incorporating the spirit and substance of the invention may occur to persons skilled in the art, the invention should be construed to include everything within the scope of the appended claims and equivalents thereof.
Number | Date | Country | Kind |
---|---|---|---|
10 2006 014 261 | Mar 2006 | DE | national |
Number | Name | Date | Kind |
---|---|---|---|
1274986 | Carolin | Aug 1918 | A |
1762002 | Van De Putte | Jun 1930 | A |
3791468 | Bryan, Jr. | Feb 1974 | A |
4773692 | Schleicher et al. | Sep 1988 | A |
4925236 | Itoh et al. | May 1990 | A |
5013081 | Cronce et al. | May 1991 | A |
5074612 | Liese et al. | Dec 1991 | A |
5120105 | Brin et al. | Jun 1992 | A |
5536062 | Spears | Jul 1996 | A |
6382708 | Erdelitsch et al. | May 2002 | B1 |
20020074826 | Presley | Jun 2002 | A1 |
20070001482 | Larson | Jan 2007 | A1 |
20070001485 | Larson | Jan 2007 | A1 |
Number | Date | Country |
---|---|---|
30 19 150 | Nov 1981 | DE |
43 05 090 | Aug 1994 | DE |
10 2004 030 571 | Jan 2006 | DE |
10 2005 030 203 | Jan 2007 | DE |
271757 | Jun 1988 | EP |
0 429 776 | Jun 1991 | EP |
1 118 529 | Jul 2001 | EP |
1 138 582 | Oct 2001 | EP |
1 738 996 | Jan 2007 | EP |
60163773 | Aug 1985 | JP |
03000578 | Jan 1991 | JP |
03281484 | Dec 1991 | JP |
WO9732770 | Sep 1997 | WO |
Number | Date | Country | |
---|---|---|---|
20070236044 A1 | Oct 2007 | US |