An aircraft fluid tank module (10) comprises a pressure-free tank shell (12) having an outer surface (18), a contour of which is adjusted to a contour of an installation space provided on board an aircraft for installation of the aircraft fluid tank module (10), and at least one fastening device (34) adapted to fasten the aircraft fluid tank module (10) to a primary structure element of an aircraft.
AIRCRAFT PROVIDED WITH A FLUID TANK MODULE
FLUGZEUG UMFASSEND EIN FLÜSSIGKEITSBEHÄLTERMODUL
AÉRONEF COMPRENANT UN MODULE DE RÉSERVOIR DE FLUIDE
2018-10-24
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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