METHOD FOR PRODUCING A RAIL-SHAPED HYBRID COMPONENT, AND SUCH A HYBRID COMPONENT

In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component(20) made of a titanium material is positioned on a first bar of a first profile rail(10) that is made of a carbon-fiber reinforced plastic material and moved in an advancing...

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Bibliographische Detailangaben
Hauptverfasser:	BORN JOHANNES, GILLESSEN ALEXANDER, ROWEDDER CARSTEN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING CLADDING OR PLATING BY SOLDERING OR WELDING CONSTRUCTIONAL ELEMENTS IN GENERAL CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING LIGHTING MACHINE TOOLS MECHANICAL ENGINEERING METAL-WORKING NOT OTHERWISE PROVIDED FOR PERFORMING OPERATIONS SOLDERING OR UNSOLDERING STRUCTURES BUILT-UP FROM SUCH ELEMENTS, IN GENERAL THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS WELDING WORKING BY LASER BEAM
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Beschreibung
Zusammenfassung:	In a method for producing a rail-shaped hybrid component, in particular for an aircraft or spacecraft, a second rail component(20) made of a titanium material is positioned on a first bar of a first profile rail(10) that is made of a carbon-fiber reinforced plastic material and moved in an advancing direction(R1), in a fixed position relative to the first profile rail(10), such that a bar portion of the first bar(11) is arranged between a first connecting portion(21) of the second rail component(20) and a second connecting portion(22) of the second rail component(20), and the second rail component(20) is cohesively connected to the first profile rail(10). Furthermore, the hybrid component(1) has a first profile rail made of a carbon-fiber reinforced plastic material and a second rail component made of a titanium material.In addition, an aircraft or spacecraft (100) with the mixing element (1) is described. 本发明描述了种用于制造特别是用于航空器或航天器的轨道形混合构件的方法，其中在相对于第型材轨道(10)的固定位置，将由钛材料制成的第二轨道构件(20)定位在由碳-纤维增强塑料材料制成的并沿前进方向(R1)移动的