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Attachment structure for affixing interior equipment components of an aircraft passenger cabin

A technology of attachment structure and internal equipment, applied in the field of aircraft, can solve the problems of extended downtime economic expenses, inflexible cabin configuration, etc., and achieve the effect of simple and convenient installation

Inactive Publication Date: 2008-11-19
AIRBUS OPERATIONS GMBH
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Thus, the advantages provided by the consistent hole spacing or attachment device spacing of the seat rails in the cabin floor, or the equivalent structure on the fuselage side, cannot be used for internal equipment components attached at the top end
[0006] Therefore, the conventional attachment of internal equipment components makes the nacelle configuration rather inflexible, which can only be changed with considerable construction effort
Thus, any change to the configuration of the passenger compa

Method used

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  • Attachment structure for affixing interior equipment components of an aircraft passenger cabin
  • Attachment structure for affixing interior equipment components of an aircraft passenger cabin
  • Attachment structure for affixing interior equipment components of an aircraft passenger cabin

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Embodiment Construction

[0029] FIG. 1 shows a sectional view of an interior equipment component 9 , in this case a central coat rack in the passenger cabin of an aircraft. Correspondingly, FIG. 2 shows a section through another interior equipment component 9 , which may be, for example, a kitchen. Both the central coat rack 9 shown in FIG. 1 and the galley 9 shown in FIG. 2 are attached to an aircraft structure 5, 6, 7 using an attachment structure according to the invention, which in the example includes a Frame elements 5 spaced apart from each other in the longitudinal direction of the fuselage, stringers 6 in the longitudinal direction of the fuselage structure, and an outer skin 7 (see also FIG. 3 ).

[0030]The attachment structure shown in Figures 1 to 3 according to a typical embodiment of the invention essentially comprises two system supports 1 extending parallel to the fuselage structure, attached in each case in pairs to frame elements 5 Two suspension devices 2, and a reinforcing bar 3 ...

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Abstract

The application describes an attachment structure, by means of which interior equipment components (9) of an aircraft passenger cabin can conveniently be affixed. The attachment structure comprises at least one system support (1) that above the cabin floor (12) extends at least along the spacing of two frame elements (12). The system support (1) has a longitudinal extension along which it comprises a plurality of attachment means (19), evenly spaced apart from each other, for affixing interior equipment components (9), wherein the spacing of the attachment means (9) is smaller than the spacing of the frame elements (5).

Description

[0001] This application claims priority from German Patent Application No. 10 2005 054890.3 filed on November 17, 2005, the disclosure content of which is hereby incorporated by reference. technical field [0002] The present invention relates generally to the technical field of equipment installation in aircraft. In particular, the present invention relates to an attachment structure by which internal equipment components of an aircraft cabin can be easily fixed. Furthermore, the invention relates to an aircraft whose fuselage structure includes a passenger cabin provided with such an attachment structure. Background technique [0003] In general, interior equipment components in the aircraft cabin are attached at the bottom end to or in the cabin floor and / or at the top end in the ceiling region of the cabin. These interior equipment components include, for example, coat racks, galleys, luggage racks, purser workstations, entertainment control centers or class dividers, a...

Claims

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Application Information

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IPC IPC(8): B64D11/00B61D37/00
CPCB64C1/066B64D11/003B61D37/003B61D17/18
Inventor 马库斯·福肯鲁迪·希森贝赫约翰内斯·贡森乌韦·约翰森黑尔格·蒂德
Owner AIRBUS OPERATIONS GMBH
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