Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

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: 2013-01-30
AIRBUS OPERATIONS GMBH
View PDF0 Cites 0 Cited by
  • Summary
  • 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 compartment results in a particularly large number of components having to be replaced as the interior equipment components are only structurally attached by means of specially designed frame components and corresponding milled structures
Moreover, such large-scale changes in the cabin configuration can only be carried out by specially authorized development companies and the relevant approval bodies, which in the case of cabin reconfiguration entails considerable economic costs due to prolonged downtime

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • 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

Examples

Experimental program
Comparison scheme
Effect test

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 comprises 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...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

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 extends at least along the spacing of two frame elements (5). The system support (1) has a longitudinal extension along which it comprises a plurality of attachment means (10), evenly spaced apart from each other, for affixing interior equipment components (9), wherein the spacing of the attachment means (10) is smaller than the spacing of the frame elements (5).

Description

[0001] This application claims priority from German Patent Application No. 102005054890.3 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, all...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Patents(China)
IPC IPC(8): B64D11/00B61D37/00
CPCB64C1/066B64D11/003B61D17/18B61D37/003
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
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com