초록 ▼

The invention relates to a fuselage cell structure of an aircraft for the simplified installation and attachment of at least one fastener for at least one conduit, the fuselage cell structure having a large number of reinforcing elements formed in particular using an aluminum alloy material. Accordi

The invention relates to a fuselage cell structure of an aircraft for the simplified installation and attachment of at least one fastener for at least one conduit, the fuselage cell structure having a large number of reinforcing elements formed in particular using an aluminum alloy material. According to the invention, the reinforcing elements within the fuselage cell structure are provided with at least one groove in which the fasteners can be secured by producing a combined pressing and clamping fit creating a positive fit at least in certain regions. For this purpose, the fasteners can have at the lower face thereof, for example, two retaining feet which can be spread apart and attached by driving a fixing element into the groove. The reinforcing elements are continuous stringers preferably produced by extrusion and cross-bars, the required grooves being simultaneously extruded during the production process.

대표청구항 ▼

1. A fuselage cell structure of an aircraft for simplified installation and attachment of at least one fastener for at least one conduit, the fuselage cell structure having a large number of reinforcing elements and the reinforcing elements having at least in certain regions at least one groove, cha

1. A fuselage cell structure of an aircraft for simplified installation and attachment of at least one fastener for at least one conduit, the fuselage cell structure having a large number of reinforcing elements and the reinforcing elements having at least in certain regions at least one groove, characterised in that the reinforcing elements are formed using an aluminum alloy material, the reinforcing elements are embodied as stringers having a substantially Z-shaped cross-sectional geometry, the at least one groove running in a head region of the stringer, or as crossbars arranged in the region of a floor frame, the at least one groove running in head flanges and/or foot flanges of the crossbars, wherein at least one fastener for positionally fixing at least one conduit can be is attached in the at least one groove, and wherein the at least one fastener has at least two retaining feet which can be locked into the at least one groove, the at least two retaining feet each having a vertical portion extending from a common linkage element and each having a horizontal portion adapted to be locked into the at least one groove, wherein the retaining feet can be spread apart by at least one fixing element to produce a pressing and friction fit with the at least one groove. 2. The fuselage cell structure according to claim 1, wherein the at least one groove has a substantially inverted T-shaped cross-sectional geometry. 3. The fuselage cell structure according to claim 1, wherein the at least one fixing element is protected from accidental detachment by interlocking with the at least one fastener. 4. The fuselage cell structure according to claim 1, wherein the at least one conduit can be attached directly to the at least one fastener. 5. The fuselage cell structure according to claim 1, further comprising at least one support member for accommodating the at least one conduit, the at least one support member being securely attached to, in particular locked onto, the at least one fastener. 6. The fuselage cell structure according to claim 1, wherein the at least one groove is interrupted by at least one recess for arranging further functional elements, in particular seat rail profiled parts, therein extending transverse to the reinforcing elements.