The invention is directed to an installation system (1) for installing at least one auxiliary device (2a-f) overhead and/or at a sidewall area in a fuselage (3) of an aircraft (4). The installation system includes at least one in principle two-dimensional carrier (5a, 5b, 5c, 5a′, 5b′, 5c′) with fastening points (6) and at least one tie rod (7) interconnected to a fastening point (6) and suited to be mechanically interconnected to a predefined fastening point (8) of the fuselage (3). The at least one auxiliary device (2) is attached to the carrier (5).
INSTALLATION SYSTEM FOR AN AIRCRAFT
2018-08-16
Patent
Electronic Resource
English
Emerald Group Publishing | 1972