A structural arrangement for an aircraft or spacecraft, in particular a fuselage structural arrangement, is disclosed. The structural arrangement includes: a former; a metal skin; and a fibre composite layer which is uniformly structured in a direction running transversely to the former and is arranged between the former and the metal skin. Further, an aircraft or spacecraft having a fuselage which has such a structural arrangement, and a method for producing such a structural arrangement are disclosed.
Structural Arrangement, Aircraft Or Spacecraft, And Method For Producing A Structural Arrangement
2017-04-27
Patent
Electronic Resource
English
European Patent Office | 2022
|Structural arrangement, aircraft or spacecraft and method
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