Invention Grant
US09359083B2 Rotorcraft fitted with a mounting structure for jointly mounting a control panel and avionics rack previously fitted with a unitary cabling assembly
有权
旋翼机配有一个安装结构，用于联合安装一个先前装配有一体式布线组件的控制面板和航空电子设备
- Patent Title: Rotorcraft fitted with a mounting structure for jointly mounting a control panel and avionics rack previously fitted with a unitary cabling assembly
- Patent Title (中): 旋翼机配有一个安装结构，用于联合安装一个先前装配有一体式布线组件的控制面板和航空电子设备
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Application No.: US14060833Application Date: 2013-10-23
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Publication No.: US09359083B2Publication Date: 2016-06-07
- Inventor: Richard Olive
- Applicant: AIRBUS HELICOPTERS
- Applicant Address: FR Marignane
- Assignee: Airbus Helicopters
- Current Assignee: Airbus Helicopters
- Current Assignee Address: FR Marignane
- Agency: Brooks Kushman P.C.
- Priority: FR1202839 20121025
- Main IPC: B64D45/00
- IPC: B64D45/00 ; B64D43/00 ; B64C27/04
Abstract:
A rotorcraft fitted with means for mounting at least one front avionics rack (3, 3′) and man-machine interface instruments (2) on board a fuselage structure (4). A mounting structure (1) comprises a slotted body forming compartments for receiving interface instruments (2), the avionics rack (3, 3′), and a unitary cabling assembly (12) suitable for incorporating as a block with the mounting structure (1). The mounting structure (1) is installed as a block on the fuselage structure (4) after its functioning has been verified. The unitary cabling assembly (12) may also include separation connectors (14) segregating communications of the front avionics rack (3, 3′) respectively with remote computers (5) by means of a primary communications bus of the multiplexed, unidirectional, or bidirectional type, and with ancillary equipment (6) and/or with on-board instruments (7) by means of a secondary fieldbus.
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