The JT9D Engine Control System

690405

02/01/1969

Event
National Air Transportation Meeting
Authors Abstract
Content
The JT9D turbofan engine, soon to be in airline service on the next generation of advanced jet aircraft, will incorporate the Hamilton Standard JFC 68 main fuel control and EVC 3 engine vane control. Now in production, this control system embodies advanced control technology while retaining the basic advantages of present operational systems. Its specific advantages are improvements in weight, performance, reliability, and durability over present commercial jet engine control systems. This paper presents a discussion of the design philosophy used in creating the system, a description of the system and some advanced techniques used in its development.
Meta TagsDetails
DOI
https://doi.org/10.4271/690405
Pages
13
Citation
Bussolari, R., "The JT9D Engine Control System," SAE Technical Paper 690405, 1969, https://doi.org/10.4271/690405.
Additional Details
Publisher
Published
Feb 1, 1969
Product Code
690405
Content Type
Technical Paper
Language
English