Device and method for producing a component and component

The invention relates to a device for producing an angle bracket 56 for attaching a fuselage cabin skin 3 to an annular gap 1 and/or a stringer 2, 66 within a fuselage cabin structure of an aircraft, wherein the angle bracket 56 is made by a single deformation of an originally flat blank 6 along at...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	LANGE THOMAS, TSCHAKROW EUGEN, MENKEN TANJA, BOCHINGER MARC, SPERLING SVEN, WIRTZ TOBIAS, EDELMANN KLAUS
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	The invention relates to a device for producing an angle bracket 56 for attaching a fuselage cabin skin 3 to an annular gap 1 and/or a stringer 2, 66 within a fuselage cabin structure of an aircraft, wherein the angle bracket 56 is made by a single deformation of an originally flat blank 6 along at least three fold lines 11-13 in a single-axis press fixture having a top and bottom die 34, 50, and the blank 6 is formed by a fiber-reinforced thermoplastic material. According to the invention, a clamping frame 18 having hinges 23-25 is disposed between the lower 34 and upper dies 50, wherein the blank 6 to be formed is received in the clamping frame 18 preferably by means of a plurality of circumferentially disposed (tension) springs 27 at the edge thereof. The invention further relates to a method for producing such a component, particularly an autostabilized angle bracket 56, by means of the device in a simple, single-stroke press device, and such a component.