Aircraft engine monitoring process
An aircraft engine and engine technology, applied in the direction of engine testing, measuring devices, testing/monitoring control systems, etc.
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[0025] With reference to Figures 1 and 2, the illustrated architecture takes a four-engine aircraft as an example to give a detailed description. The monitoring and control system 10 of the engines m1, m2, m3, and m4 of the aircraft (not shown in the figure) is composed of FADEC computers 1, 2, 3, 4. Each computer monitors and controls the designated engine m(1), m(2), m(3), m(4), or, as shown in the figure, m1, m2, m3, m4.
[0026] FADEC, here are 4 units, which are connected to each other via an aircraft through the AFDX (Aviation Electronic Equipment Full Duplex) digital communication network. This digital communication network can be determined, for example, according to the ARINC (Aviation Radio Company) standard. A dedicated link for communication as described below, or through an existing link dedicated to other communications on the aircraft, to send data and parameters from the engine that it monitors and controls. FADEC is a two-way computer, which can enhance the inform...
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