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SOCLE DE COCKPIT ET AÉRONEF COMPORTANT UN SOCLE DE COCKPIT

摘要

A cockpit pedestal (100) and an aircraft with a cockpit pedestal. The cockpit pedestal (100) includes an integrally-formed frame (110) including an instrument receiving portion (114) defining a plurality of compartments (120) for receiving instruments (80) therein; and a plurality of legs (140) supporting the instrument receiving portion (114), the plurality of legs (140) being integrally formed with the instrument receiving portion (114), the plurality of legs being adapted for transferring a load of the plurality of instruments from the instrument receiving portion to a floor of the aircraft cockpit (20) when the cockpit pedestal and the instruments are installed in the aircraft cockpit. In some versions the cockpit pedestal includes a conductive layer (150) electrically grounding the instruments in the cockpit.

著录项

  • 公开/公告号EP3659926A1

    专利类型

  • 公开/公告日2020.06.03

    原文格式PDF

  • 申请/专利权人

    申请/专利号EP19209922.4

  • 发明设计人

    申请日2019.11.19

  • 分类号

  • 国家 EP

  • 入库时间 2022-08-21 10:52:35

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