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AIRCRAFT GAS TURBINE ENGINE CONTROLLER WITH REMOVABLE MEMORY AND DIAGNOSTIC SYSTEM AND METHOD THEREFOR

  • US 20090326782A1
  • Filed: 04/21/2008
  • Published: 12/31/2009
  • Est. Priority Date: 04/21/2008
  • Status: Abandoned Application
First Claim
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1. An aircraft gas turbine engine controller, comprising:

  • a processor coupled to receive engine performance data representative of a plurality of aircraft gas turbine engine parameters, the processor configured to (i) generate and supply engine control signals based, at least in part, on the engine performance data and (ii) selectively transmit at least a portion of the engine performance data for storage;

    a fixed memory device in operable communication with the processor to receive and store the engine performance data selectively transmitted by the processor, the fixed memory device fixedly coupled to a fixed-memory mount; and

    a removable memory device in operable communication with the processor to receive and store the engine performance data selectively transmitted by the processor, the removable memory device non-fixedly coupled to a removable memory mount in a manner that allows the removable memory device to be hand-removable from the removable memory mount.

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