The structure of distributing between FADEC and avionic component

The structure of distributing between FADEC and avionic component

  • CN 101,808,900 B
  • Filed: 08/20/2008
  • Issued: 11/25/2015
  • Est. Priority Date: 09/03/2007
  • Status: Active Grant
First Claim
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1. , for the device of motor-powered aircraft, described device comprises at least one avionic component of being arranged in described aircraft and is arranged in the driving engine of described aircraft or at least one engine controller near it,The feature of this device is, described device also comprises at least one the driving engine interface being arranged in described aircraft, at least one driving engine interface described is for obtaining the reliability of different source datas and confirmation data, at least one driving engine interface described is suitable for obtaining, select and merge the numerous data deriving from avionics system, and transmit necessary data with the form of synthesis after verification, at least one driving engine interface described is suitable for merging the data that derive from least one engine controller described and sends it at least one avionic component described, at least one driving engine interface described is monitored at least one avionic component described independent of at least one engine controller described,At least one driving engine interface described is suitable for the swapping data at least one avionic component described and at least one engine controller described, at least one driving engine interface described is standard and is suitable for and can be arranged on described carry-on dissimilar engine controller and gets in touch with, at least one engine controller described is exclusively used in the driving engine of a typeBe further characterized in that, at least one driving engine interface described comprises at least two redundant channels.

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