Joining method and assembly for an aircraft
AssigneeAirbus SAS
InventorsUwe Beier, Christian Metzner, Thomas Meer
Life of this patent
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Abstract
A joining method and assembly for an aircraft. To improve the characteristics or permit hitherto impossible connections between thermoplastic and thermoset components, a multi-material joining method is disclosed in which a thermoplastic connecting region is formed on the thermoplastic component. The connecting region is connected to the thermoset component by interdiffusion. For this purpose, the uncured second component is brought into contact with the connecting region and heat is supplied. An interdiffusion layer is formed which fixedly connects the second component and the connecting region to one another and thus joins the first component to the second component.
Claims1
A joining method for joining together fiber-reinforced first and second components, the method comprising:
- forming a connecting region, which comprises one or more thermoplastic polymer materials and is formed with a surface structure region;
- forming, via additive manufacturing, a first fiber-reinforced component, which comprises a first polymer material as matrix, on the connecting region, such that the connecting region and the first component are attached together to provide a joining surface on the first component;
- forming a second fiber-reinforced component, which comprises a curable thermosetting second polymer material as matrix;
- and
- arranging, after the connecting region and the first component are attached together, a region of the second component in contact with the joining surface and supplying heat to fix the connecting region to the second component while curing the second polymer material to join the first component to the second component;
- wherein the surface structure region comprises periodic elevations and indentations in at least one direction and is formed on a side of the connecting region that faces away from the joining surface;
- and
- wherein, in a plane parallel to the joining surface, the elevations and the indentations are of wavelike design and/or a corrugated or serrated pattern.
Dependencies are inferred from the claim text.