| 摘要 |
The rotorcraft has a communication cable fitted to a man-machine interface instrument (2) and a front avionics rack (3) so as to power the instrument and the rack and to put the instrument and the rack in communication with a set of remote units (5-7) distributed aboard the aircraft. A mounting structure (1) is utilized for jointly mounting the interface instrument and the rack on a fuselage structure (4). A unitary cabling assembly provides connection for the interface instrument and for a calculation unit with the set of remote units via a set of separate connectors (14). An independent claim is also included for a method for application of assembly structure of a rotorcraft. |
