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Frame element, storage bin and method for installing a storage bin in an aircraft

A technology for aircraft and storage boxes, which is applied to aircraft parts, vehicle parts, transportation and packaging, etc. It can solve the problems of time-consuming and difficult installation of storage boxes, and achieve the effect of simple installation

Inactive Publication Date: 2012-04-04
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Storage bin installation is often time consuming as each bin must be individually positioned and secured to the aircraft structure
In addition, changes to location and / or design are often very difficult to achieve, since such changes usually require modification of the mounts on the aircraft structure side and / or at least for the mounting of storage boxes on the aircraft structure The fastening point is modified

Method used

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  • Frame element, storage bin and method for installing a storage bin in an aircraft
  • Frame element, storage bin and method for installing a storage bin in an aircraft
  • Frame element, storage bin and method for installing a storage bin in an aircraft

Examples

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Embodiment Construction

[0038] figure 1 and figure 2 Shown is a frame element 10 made of aluminum comprising two curved longitudinal struts 12 , 14 arranged in parallel to each other and between said longitudinal struts 12 , 14 in parallel to each other. Extended three connecting struts 16, 18, 20. At a first end of each longitudinal strut 12 , 14 of the frame element 10 a force application device 22 , 24 is formed. The frame element 10 includes storage box fastening means, not shown, for fastening the storage box 26 at various positions on the frame element 10 . A retaining device, a clamping device or a latching device may serve as storage box fastening means for fastening the storage box 26 to the frame element 10 . Alternatively, however, the storage box 26 can also be screwed or riveted to the frame element 10, in which case corresponding holes are then provided in the storage box 26 and / or the frame element 10, if necessary. If so, the holes can be threaded and placed at different position...

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PUM

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Abstract

A frame component (10) which is used in an aircraft component installation system (46) can be connected to an aircraft structure (36) and comprises a storage box fastening device. The storage box fastening device is designed to fasten a storage box (26) to a different position on the frame component (10). The storage box (26) used in the aircraft comprises a device which is complementary to the storage box fastening device of frame component (10) so as to fasten the storage box (26) to the different position on the frame component (10). In a method for installing the storage box (26) in the aircraft, the frame component (10) is provided. The storage box (26) is fastened to an anticipated position on the frame component (10). The frame component (10) is connected to an aircraft structure (36).

Description

technical field [0001] The invention relates to a frame element for use in an aircraft component mounting system, a storage box and a method for installing a storage box in an aircraft. Background technique [0002] Currently, when installing storage boxes in an aircraft, the storage boxes are usually connected separately to the aircraft structure. Wherein, the storage boxes are respectively fixed at a certain height corresponding to the geometric shape of the fuselage (aircraft main body). Installation of the storage bins is often time consuming because each storage bin must be individually positioned and secured to the aircraft structure. In addition, changes to location and / or design are often very difficult to achieve, since such changes usually require modification of the mounts on the aircraft structure side and / or at least for the mounting of storage boxes on the aircraft structure The fastening point is modified. Contents of the invention [0003] The object of ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D11/00B60R5/00
CPCB64C1/066B64D11/003B64C1/40Y10T29/49826
Inventor 克里斯蒂安·克芬格约阿希姆·梅茨格迈克尔·奥布格尔
Owner AIRBUS OPERATIONS GMBH