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Fastening arrangement for fastening a component on a fuselage

A technology for fixing devices and structural units, applied in the direction of equipment, fuselage, aircraft parts, etc. for loading and unloading goods, which can solve the problems of trouble, high total weight of the aircraft, deburring manpower and time consumption.

Inactive Publication Date: 2015-04-01
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] This is relatively cumbersome since the manufacture of the holes, the deburring of the holes, the assembly of the overhead luggage rack and its alignment are associated with high labor and time expenditure
Besides that, the different brackets and fixing elements necessary for joining to the stiffening elements may lead to a higher overall weight of the aircraft

Method used

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  • Fastening arrangement for fastening a component on a fuselage
  • Fastening arrangement for fastening a component on a fuselage
  • Fastening arrangement for fastening a component on a fuselage

Examples

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Embodiment Construction

[0046] figure 1 A part of an aircraft fuselage 2 is shown, on which a fastening device 4 according to the invention is arranged. The fastening device 4 according to the invention consists of a base element 6 , an exemplary holding rail 8 with a double T-shaped cross-section and a connecting element 10 arranged therebetween. base element 6 and retaining rail 8 in the figure 1 In the example shown in , they extend parallel to each other and are spaced apart by connecting elements 10 and are mechanically connected to each other. The base element 6 has a receiving means 12 realized in the form of a receiving hole. The holding rail 8 likewise has a receptacle 14 , which is configured as a receptacle, for example.

[0047] Furthermore, a bulkhead 16 can be seen on the fuselage 2 , which has an essentially ring-shaped configuration and is arranged transversely to the longitudinal axis of the fuselage 2 . In order to fasten the fastening device 4 according to the invention, the fr...

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PUM

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Abstract

A mounting assembly for the mounting of components in a body of a vehicle comprises at least one base element, at least one holding rail and connecting elements. The base element is designed to be arranged on the body of the vehicle. The holding rail is designed for mounting the components, and the base element and the holding rail are connected by the connecting elements so as to be spaced apart from each other.

Description

[0001] Related application reference [0002] This application claims that the filing date is October 27, 2009, the application number is the U.S. patent application No. 61 / 255,396 and the filing date is October 27, 2009, the application number is the German patent application No. 10 2009 050 736.1 priority, the contents of which are hereby incorporated by reference. technical field [0003] The present application relates to a fastening device for fastening a structural unit to an aircraft fuselage, an aircraft equipped with such a fastening device, and a method for producing such a fastening device. Background technique [0004] In the aircraft, a plurality of structural elements contributing to the shape of the aircraft cabin are arranged on stiffening elements of the aircraft fuselage. In this case, the stiffening elements are generally formed as so-called bulkheads and by so-called stringers, wherein the bulkheads are arranged at regular intervals transversely to the l...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D11/00
CPCB64C1/406B64D9/003Y02T50/46B64D11/003B64D11/0696Y02T50/40
Inventor 亨德里克·温策尔塞巴斯蒂安·乌姆劳夫特
Owner AIRBUS OPERATIONS GMBH