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Fixing device

A fastening device and fastening technology, which is applied in the direction of seat arrangement, transportation and packaging, thin plate connection, etc., can solve the problem of no integrated vibration damping device, etc., and achieve the effect of light weight and low cost

Active Publication Date: 2013-05-08
FACC
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there is no integrated vibration damping device

Method used

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Examples

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Embodiment Construction

[0029] figure 1 and figure 2 An embodiment of a fastening device 1 is shown for fastening a fitting 2 in the form of a floor element 3 to a structure 4 at a distance d, for example in an aircraft. figure 1 Transversely to the longitudinal direction of the aircraft, the fastening device 1 arranged on the fitting 2 is shown, figure 2 The fastening device 1 is shown viewed in the longitudinal direction of the aircraft. The fastening device 1 comprises a fastening element 5 with an end 6 configured as a leg 6' for bearing on a structure 4. The end 7 of the fastening element 5 opposite said end 6 or the leg 6' is correspondingly configured for receiving the fitting 2, in particular the floor element 3. For the adjustability of the fastening device 1 in the horizontal direction, that is to say in the plane of the structure 4 , the feet 6 ′ of the fastening element 5 are mounted movably in rail profiles 14 arranged on said structure 4 . A rough movement of the fastening device...

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PUM

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Abstract

The invention relates to a device (1) for fixing fittings (2), in particular wall or floor elements (3) in airplanes, to a structure (4) such that no vibrations are generated, comprising a fixing element (5) which is designed on one end (6) for fixing to the structure (4) and on the opposite end for receiving the fittings (2). The opposite end (7) of the fixing element (5) is movably mounted in a spacer sleeve (21) which can be connected to the fittings (2) to be received and which comprises an elongated hole-shaped cross-section, and said opposite end is designed for fixing to the fittings. At least one damping element (8) is provided for arranging between the structure (4) and the fittings (2). The spacer sleeve (21) has an elongated hole-shaped cross-section, and the one end (6) of the fixing element (5) is formed by a stand (6') or can be connected to a stand (6'), said stand (6') being designed for movably mounting in a rail section (14) that lies on the structure (4).

Description

technical field [0001] The invention relates to a device for the vibration-free fastening of fittings, in particular wall or floor elements in an aircraft, to a structure, having a fastening element which is formed at one end for fastening On said structure, while on the opposite end for receiving said fitting, wherein said opposite end of the fastening element is movably supported on a spacer bush which can be connected with said fitting to be housed and is configured for fastening to the fitting, and at least one damping element is provided for the arrangement between the structure and the fitting. [0002] In particular in aircraft it is necessary to connect various fittings, such as wall or floor elements, to the load-bearing structure of the aircraft in a vibration-free or vibration-decoupled manner. However, it is also conceivable to use such a fastening element in applications other than aircraft where various accessories are to be connected in a vibration-decoupled ma...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D11/00B64D11/04B64D11/06
CPCF16B5/0241F16F1/3835B62D27/04Y02T50/46B64D11/0696B64D11/00F16F1/3863Y02T50/40F16B5/0225F16B43/001F16B43/00
Inventor B·克梅雷尔
Owner FACC
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