Multi-material joint
AssigneeAirbus Operations GmbH
InventorMartin MUIR
Life of this patent
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AssigneeAirbus Operations GmbH
InventorMartin MUIR
Estimating the term…
A multi-material component is provided including two members formed of different materials joined together at a multi-material join. The two members have complementary protrusions that form a multi-material join with a zig-zag interface, such that a tension between them is experienced in at least part as a shear force at the interface between the protrusions. The component further includes a third member connected to the first member by a lattice, which is capable of elastic deformation so as to substantially isolate the interface between the complementary protrusions from deformation of the third member such as that caused by thermal expansion. Methods of designing and constructing such a component in a single piece via additive manufacturing are provided. The component is particularly suitable for use in pylons connecting jet engines to aircraft wings.
A multi material component comprising:
A method of designing a multi-material component for use in coupling a heat source to a vehicle, the multi-material component comprising a first member formed of a first material and a second member formed of a second material, the first and second members each comprising complementary protrusions that form a multi-material join and define a interface between the first and second members;
A method of creating a multi-material component, the component comprising a multi-material join where two different materials are joined together, the method comprising:
A method of creating a multi-material component, the component comprising a multi-material join where two different material are joined together, the method comprising:
Dependencies are inferred from the claim text.