The present invention describes an outer fuel access tank cover (FTAC) of an aircraft, a wing comprising such outer FTAC of an aircraft and an aircraft. The invention belongs to the field of designing auxiliary pieces in the wings of aircraft to control the risk of impact against an inner FTAC when an impact occurs against the outer FTAC. This impact can be caused by a tire.
Outer fuel tank access cover, wing and aircraft comprising such a cover
Abdeckung für äußeren Kraftstofftankzugang, Flügel und Flugzeug mit einer solchen Abdeckung
Couvercle d'accès de réservoir de carburant externe, aile et avion comprenant un tel couvercle
2017-05-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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