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
2016-04-19
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft/spacecraft fluid cooling system and aircraft/spacecraft fluid cooling method
Europäisches Patentamt | 2016
|Aircraft and spacecraft propulsion
Engineering Index Backfile | 1959
|AIRCRAFT AND SPACECRAFT PROPULSION
NTRS | 1959
|