Aircraft with an engine control device in the engine compartment and method to obtain such aircraft

    公开(公告)号:US11691749B2

    公开(公告)日:2023-07-04

    申请号:US17175003

    申请日:2021-02-12

    CPC classification number: B64D31/14 B64F5/40 B64D2041/002 F02D2001/0095

    Abstract: A method to modify an aircraft including: disconnecting a first engine control device from command cables and transmission cables, wherein the first engine control device is in a fuselage section forward of a pressure bulkhead; replacing the engine control device with a jumper connector positioned in the fuselage section, wherein the jumper connector electrically connects the command cables to the transmission cables; installing a second engine control device in the fuselage aft of the pressure bulkhead, wherein the second engine control device is in an engine compartment of the fuselage; connecting the second engine control device to transmission cables at a location at or near the pressure bulkhead; connecting sensor cabling directly to the second engine control device, and connecting the engine control device directly to the engine.

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