Accession Number:

AD0402813

Title:

DESIGN REPORT OF AN ENGINE PERFORMANCE INDICATOR

Descriptive Note:

Corporate Author:

NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AERONAUTICAL INSTRUMENTS LAB

Personal Author(s):

Report Date:

1963-03-01

Pagination or Media Count:

30.0

Abstract:

The development of a simplified version of an Engine Performance Indicator is reported. The instrument is a three-module, servo-driven indi cator which displays information relative to Engine Speed RPM, Exhaust Gas Temperature EGT, and Fuel Flow F.F. utilizing vertical tape type of readout. The compatibility of this indicator with the integrated display system was evaluated.

Subject Categories:

  • Jet and Gas Turbine Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE