Accession Number : AD0783683
Title : Integrated Engine Instrument System.
Descriptive Note : Final technical rept. 29 Aug 72-30 Nov 73 on Phase 3,
Corporate Author : GENERAL ELECTRIC CO WILMINGTON MASS AEROSPACE INSTRUMENTS AND PRODUCT SUPPORT DEPT
Personal Author(s) : Skovholt,R. L. ; Berglund,D. E. ; Doerle,W. A. ; Hiatt,W. R. ; Johnson,F. P.
Report Date : DEC 1973
Pagination or Media Count : 228
Abstract : A two-volume report documents the Phase 3 effort for the integrated engine instrument system (IEIS). IEIS is a computer-driven display and processing instrumentation system concerned with monitoring the aircraft engine's conditions in response to the anticipated needs of flight crew and maintenance personnel in the 1980-85 timeframe. Volume 1 covers engine analysis, including such topics as assumptions, subsonic missions, gas path, mechanical measurement, airborne computer operations, diagnostics, data recording, maintenance indication, fault isolation, gross thrust factor, airborne display, recommendations, and long term trending. Next, system design is discussed, involving requirements, vibration and temperature monitoring, data transmission, software and hardware, costs, program time and routines, reliability, recording, and an introduction to functions performed.
Descriptors : *Aircraft engines, *Monitoring, *Computer applications, *Display systems, Instrumentation, Integrated systems, Human factors engineering, Engine components, Diagnostic equipment, Computer programming, Vertical takeoff aircraft, Short takeoff aircraft, Naval aircraft, Mission profiles, Recording systems, Faults, Maintenance, Airborne, Mechanical engineering, Costs, Data processing
Subject Categories : V/STOL
Distribution Statement : APPROVED FOR PUBLIC RELEASE