The invention relates to a test device, in particular a test structure for dynamic seat tests in the aeronautics industry.
Due to increased seat weight, locally increased loads occur that need to be determined in an approval test with original seat rails by means of dynamic tests. In particular, the CS 25.562/FAR 25.562 conditions must be met.
The increase in the seat weight as a result of improved comfort for the passengers has resulted in a requirement for a significant improvement in the local load transfer.
There may be a need to provide a seating device for dynamic seat tests meeting the CS 25.562/FAR 25.562 conditions.
The achievement of the need is described in claim 1. Further developments of the invention are disclosed in the subordinate claims.
The test device according to the invention contains a load cell, a seat rail with a bar and an upper chord, a load transfer means which comes into contact with opposite sides of the bar of the seat rail and is fixed to the load cell, and a floor plate which is fixed to the upper chord of the seat rail and to the load transfer means.
According to a further development of the invention, the load transfer means comprises two profiles arranged on the opposite sides along the bar of the seat rail and fixed to these.
According to a further development of the invention, the profiles are U-profiles with limbs running parallel to the floor plate and extending outward away from the bar of the seat rail.
According to another further development of the invention, the aforementioned components, i.e., the upper chord, load transfer means, floor plate and load cell are each fixed by means of a screw, a clip and/or a groove.
For the local load transfer, according to the invention, in addition to the seat rail crown, the surrounding of the seat rail (floor plate) is also integrated in the test structure. This involves in particular the adaptation of floor plates, which are fixed with original fixing elements. The aim and result of the test device according to the invention is to increase the local load transfer into the seat rail by utilising the existing installation situation. This corresponds to the actual installation situation and results in a relatively higher load bearing capacity compared to known test structures.
In particular, the invention meets the so-called 10° roll (torsion) requirement in full.
The following describes an example of an embodiment of the test device according to the invention with reference to the attached diagram.
As shown in
According to the preferred example of an embodiment, one frontal face 10 of the bar 7 comes into contact with the surface of the load cell 2, which is the same as that with which the limbs 4a, 4b of the U-profiles 3a, 3b come into contact.
The seat rail 8 is substantially T-shaped and comprises, on an end lying opposite to the frontal face 10 of the bar 7, an upper chord 11 extending substantially perpendicularly to the bar 7 and parallel to the surface of the load cell 2.
The seat rail 8 also comprises a crown 12, which is arranged substantially in the middle of the upper chord 11 symmetrical to the bar 7 in order to accommodate correspondingly designed components of a passenger seat (not shown). The crown 12, the upper chord 11 and the bar 7 of the seat rail 8 are preferably embodied in one piece but alternatively could also be embodied separately and welded to each other, for example.
As shown in
As shown in
The connecting elements 16a, 16b extend substantially parallel to the bar 7 from the floor plate 13a, 13b in the direction of the load cell 2.
As shown in
The connecting elements 16a, 16b come into contact with the respective faces of the limbs 4a, 4b, 17a, 17b of the U-profiles 3a, 3b.
The connecting elements 16a, 16b are also fixed by fixing elements 19a, 19b via the respective faces to the limbs 4a, 4b of the U-profiles 3a, 3b. The fixing elements 19a, 19b are for example a screw, a clip, a groove, etc.
Although the above describes the invention with reference to a preferred example of an embodiment, it should be understood that that different modifications of the test structure are possible without leaving the scope of the invention as long as it is guaranteed that the local aircraft structure is integrated in the test structure.
In addition, the test device for dynamic seat tests is not restricted to the aeronautics industry but can also be used in other fields, for example the railway or shipping industries, etc.
Number | Date | Country | Kind |
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10 2006 025 145.8 | May 2006 | DE | national |
This application claims the benefit of the filing date of German Patent Application No. 10 2006 025 145.8 filed May 30, 2006 and of U.S. Provisional Patent Application No. 60/809,289 filed May 30, 2006, the disclosures of which applications are hereby incorporated herein by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/EP2007/004730 | 5/29/2007 | WO | 00 | 11/25/2008 |
Number | Date | Country | |
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60809289 | May 2006 | US |