• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention relates to a load plane element which is intended to be mounted on load bows vehicles, the load plane element comprising a plant bottom portion (1) having at least one upwardly folded edge (3) in the longitudinal direction of the load plane element which generally coincides with the vehicle direction of travel. Characteristic of the loading platform element according to the present invention is that the bottom portion (1) is provided with composite openings (10, 11, 12), (10, 11, 12) comprising at least two sub-openings (10A, 10B, 11A, 11B, 12A, 12B) of different widths. (Bl, B2). and that the composite openings (Fig. 3)
    公开号:SE1000696A1
    申请号:SE1000696
    申请日:2010-06-29
    公开日:2011-12-30
    发明作者:Henrik Nyberg
    申请人:Henrik Nyberg；
    IPC主号:
    专利说明:

    15 20 25 30 35 2 sufficient bearing capacity while having as low a weight as possible. At least the primary object of the present invention is realized by means of a loading platform element which has obtained the features stated in the following independent claim 1. Preferred embodiments of the invention are defined in the dependent claims.
    Brief Description of the Drawings Hereinafter, a preferred embodiment of the invention will be described with reference to the accompanying drawings, in which: Fig. 1 shows a perspective view of a loading platform element according to the present invention; Fig. 2 shows a plan view of the load plane element according to Fig. 1; and Fig. 3 shows a perspective view of a loading platform element according to the present invention, wherein an elongate object is clamped on the loading platform by means of clamps.
    Detailed description of a preferred embodiment of the invention The load plane element shown in Figs. 1 and 2 comprises a flat bottom portion 1, a first longitudinal continuous edge portion 3 and a number of second longitudinal edge portions 5.
    As can be seen most clearly from Fig. 1, the first longitudinal edge portion 3 is folded upwards. The other longitudinal edge portions 5 are folded downwards. As can be seen most clearly from Fig. 1, the other edge portions 5 are three in number and arranged at a distance from each other, whereby spaces 7 are formed, in which load arches (not shown) are intended to be received.
    The loading platform element according to the present invention is preferably made of aluminum with a thickness of the order of 3 ~ 6 mm.
    The flat bottom portion 1 is provided with a number of round or oval holes of different size and configuration, this configuration of holes may vary and is thus not significant for the present invention. These holes are used i.a. to clamp the load plane element to the load arches 10 U and to apply straps or the like to lash the load present on the load plane element.
    The flat bottom portion 1 also has a number 10, 11, 12. of the openings 9 are generally rectangular and located in openings 9. In the embodiment shown, two are connected to the downwardly folded edge portions 5. The other 11, sub-openings of different sizes, the sub-openings the openings 10, 12 are composed of rectangular passages so as to form a continuous opening.
    A first composite opening 10 is located adjacent the intermediate downwardly folded edge portion 5, the first composite opening 10 comprising a central rectangular first sub-opening 10A and two rectangular second sub-openings 10B connecting to the first sub-opening 10A on either side thereof. In general, the first sub-opening 10A is larger than the second sub-openings 10B. According to the embodiment shown, the first sub-opening 10A has a width B1 which according to the invention can be about 3-5 times the width B2 of the second sub-openings 10B, the longitudinal direction of which coincide with each other. According to the embodiment shown, the second sub-openings 10B connect to the first sub-opening 10A in the middle of the opposite short sides of the first sub-opening 10A.
    A second composite opening 11 is located adjacent an intermediate portion of the upwardly folded edge portion 3.
    The second composite opening 11 comprises a third rectangular sub-opening 11A and a fourth rectangular sub-opening 11B, the third sub-opening 11A being generally larger than the fourth sub-opening 11B. According to the embodiment shown, the third sub-opening 11A has a width B1 which according to the invention can be 3-5 times the width B2 of the fourth sub-opening 11B. According to the embodiment shown, the fourth sub-opening 11B connects to the third sub-opening 11A in the middle of one long side of the third sub-opening 11A. In general, the second composite opening has a T-shape.
    Two third composite openings 12 are located in the area of two of the corners of the loading platform element, adjacent to respective ends of the upwardly folded edge portion 3. The third composite openings 12 comprise a fifth rectangular sub-opening 12A and a sixth rectangular sub-opening 12B. , the fifth sub-opening 12A generally being larger than the sixth sub-opening 12B. According to the embodiment shown, the fifth sub-opening 12A has a width B1 which according to the invention can be 3-5 times the width B2 of the sixth sub-opening 12B. According to the embodiment shown, the sixth sub-opening 12B connects with one end portion to an end portion of the fifth sub-opening 12A. Generally, the third composite opening has a 12 L shape.
    Fig. 3 shows how an elongate object F is clamped on the load plane element according to the present invention. The clamping of the elongate object F takes place by means of two clamps T, which are preferably so-called quick clamps. When fitting the quick clamps, one stop of the quick clamp T (not visible) can be transferred to the underside of the load plane element via the fifth partial opening 12A, i.e. the fifth sub-opening 12A is large enough to allow passage for one stop of the quick clamp T. Thereafter, a slide rail G of the high-speed wing T is inserted into the sixth sub-opening 12B, the sixth sub-opening 12B having such a small width B2 that the abutment located on the underside of the load plane element cannot pass through the sixth sub-opening 12B.
    The abutment of the high-speed wing T located on the underside of the loading platform element can thus be brought into abutment against the underside of the loading platform element, in the area of the sixth sub-opening 12B, without the abutment being able to pass through the sixth sub-opening 12B. The second abutment A present on the upper side of the load-bearing element A of the quick-release wing T can be applied for abutment against the elongate object F to be clamped on the load-bearing element according to the present invention. Then the quick clamps are activated so that a clamping of the object F takes place.
    Of course, the other composite openings 10 and 11 can also be used in a corresponding manner to clamp objects on the load plane element.
    Possible modifications of the invention The above-described embodiment of a loading platform element constitutes half of a loading platform which is mounted on the load arches of a vehicle, i.e. two loading platform elements as described above are mounted together, the assembly taking place along the normally abutting downwardly folded edge portions 5 of the respective loading platform elements. However, it is not necessary for the edge portions 5 to abut each other if it is desirable for the load plane to define a larger width.
    Within the scope of the present invention, it is not necessary for the loading platform to consist of two loading platform elements, but it is also conceivable for one loading platform element to constitute the entire loading platform. In that case, however, the edge portions will have a different design than that described above.
    In the above-described embodiments of the composite openings, these comprise rectangular sub-openings. Within the scope of the present invention, however, the sub-openings do not have to have a rectangular shape, this being especially true of the larger sub-openings of the composite openings. Since the larger sub-openings only 10A, 11A, 12A have only the task of allowing passage for stops of clamps, it will be appreciated that the shape of these openings can in principle be arbitrary as long as they allow said passage. In the case of the smaller partial openings of a composite opening, these should generally be in the form of a slot which allows the slide rail G to be received by the quick wing and also that the slide rail G can be displaced in the longitudinal direction of the slot. However, it is not necessary for the smaller sub-openings / slots to have a constant width, but it can be varied within certain limits as long as the slide rail G can be displaced and the passage of the abutment on the underside of the load plane element is not permitted.
    With regard to the number of composite openings 10, 11, 12 and the location of the same, the number and the location shown in Figs. 1-3 are only exemplary. Thus, a loading platform element according to the present invention can have both fewer and more composite openings than the number shown in Figs. 1-3. Of course, the location of the composite openings may also deviate from the location shown in Figs. 1-3.
    权利要求:
    Claims (9)
    [1]
    A loading platform element intended to be mounted on load arches for vehicles, the loading platform element comprising a flat bottom portion (1) characterized as being provided with openings, in that the bottom portion (1) is provided with composite openings (10, 11, 12), and that the composite openings (10, 11, 12) comprise at least two sub-openings (10A, 10B, 11A, 11B, 12A, 12B) of different widths (B1, B2).
    [2]
    Cargo plane element according to Claim 1, characterized in that at least one of the composite openings (11) has an L-shape.
    [3]
    Load plane element according to claim 1 or 2, characterized in that at least one of the composite openings (12) has a T-shape.
    [4]
    Load plane element according to one of the preceding claims, in that at least one partial opening (10A, (10, 11, k e n k e n k e a k l a t l 10 B, 11A, 11B, 12A, 12B) 12) has a rectangular shape. at a composite opening
    [5]
    Load plan element according to claim 4, characterized in that all sub-openings (10A, 10B, 11A, 11B, 12A, 12B) of a composite opening (10, 11, 12) have a rectangular shape.
    [6]
    Load plane element according to one of the preceding claims, in that the sub-openings (11A, 11B, 12A, 12B) of a composite opening (11, 12) have extensions in their longitudinal direction which are perpendicular to each other.
    [7]
    Load plane element according to one of the preceding claims, in that the widths (B1, B2) of 11A, 11B, 12A, 12B) are characterized by the sub-openings (10A, 10B) such that B1> B2.
    [8]
    Load plane elements according to claim 7, characterized in that the widths (B1, B2) relate to each other according to: 3B2 S B1 S 5B2.
    [9]
    Load element element according to one of the preceding claims, in that the bottom portion (1) has the characteristic of at least one folded-up edge (3) in the longitudinal direction of the load plane element, the longitudinal direction generally coinciding with the direction of travel of the vehicle.
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    同族专利:
    公开号 | 公开日
    EP2402215A1|2012-01-04|
    SE534929C2|2012-02-21|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    AT341351B|1976-07-30|1978-02-10|Knoblich Camillo|ROOF RACK FOR MOTOR VEHICLES|
    DE29520547U1|1995-12-27|1996-02-29|Oris Fahrzeugteile Riehle H|Loading platform for arrangement on the roof of a motor vehicle|
    法律状态:
    2013-01-29| NUG| Patent has lapsed|
    优先权:
    申请号 | 申请日 | 专利标题
    SE1000696A|SE534929C2|2010-06-29|2010-06-29|Load Plan Element|SE1000696A| SE534929C2|2010-06-29|2010-06-29|Load Plan Element|
    EP11445003A| EP2402215A1|2010-06-29|2011-06-28|Load surface element|
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