The present invention provides a composite for an aircraft or spacecraft, comprising: a skin portion; a stringer which is attached to the skin portion; and a former made from fibre composite material, which is attached to the skin portion and forms an opening therewith, through which the stringer extends, substantially transverse to the former.
COMPOSITE, AIRCRAFT OR SPACECRAFT, AND METHOD
VERBUNDSTRUKTUR, FLUGZEUG ODER RAUMFAHRZEUG UND VERFAHREN
COMPOSITE, AÉRONEF OU ENGIN SPATIAL ET PROCÉDÉ
2018-06-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft/spacecraft fluid cooling system and aircraft/spacecraft fluid cooling method
European Patent Office | 2016
|Aircraft and spacecraft propulsion
Engineering Index Backfile | 1959
|AIRCRAFT AND SPACECRAFT PROPULSION
NTRS | 1959
|