Concorde Thrust Management

700817

2/1/1970

Authors
Abstract
Content
The Rolls-Royce/S.N.E.C.M.A. Olympus 593 employs a variable area primary nozzle and has a reheat system - both novelties to civil aviation. The main purpose of this paper is to show that these innovations are accommodated without generating crew work load problems. Consequently the paper is aimed primarily at the airline user rather than the control system specialist. A brief description is given of the basic engine electrical control and its interface with the intake system. The flight deck mounted thrust management controls and indicators are identified and their use described during the course of a typical flight. The subject of engine mechanical condition monitoring is also examined.
Meta TagsDetails
DOI
https://doi.org/10.4271/700817
Citation
Payne, C. and Lewis, A., "Concorde Thrust Management," National Aeronautic and Space Engineering and Manufacturing Meeting, Los Angeles, California, United States, October 5, 1970, https://doi.org/10.4271/700817.
Additional Details
Publisher
Published
2/1/1970
Product Code
700817
Content Type
Technical Paper
Language
English