Hall et al., 2001 - Google Patents
F/A-18E/F F414 advanced inflight engine condition monitoring system (IECMS)Hall et al., 2001
- Document ID
- 11599541201698894235
- Author
- Hall C
- Leary S
- Lapierre L
- Hess A
- Bladen K
- Publication year
- Publication venue
- 2001 IEEE Aerospace Conference Proceedings (Cat. No. 01TH8542)
External Links
Snippet
The IECMS proven on the F/A-18C/D aircraft has been further developed with expanded capabilities for the F414-GE-400 engine installed in the F/A-18E/F Super Hornet. IECMS combines diagnostic algorithms, engine control system computer/sensors, and airframe …
- 241000256856 Vespidae 0 abstract description 4
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0259—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterized by the response to fault detection
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B23/00—Testing or monitoring of control systems or parts thereof
- G05B23/02—Electric testing or monitoring
- G05B23/0205—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults
- G05B23/0218—Electric testing or monitoring by means of a monitoring system capable of detecting and responding to faults characterised by the fault detection method dealing with either existing or incipient faults
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