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INTERRELATION OF ENGINE DESIGN AND BURNER CONFIGURATION WITH SELECTION AND PERFORMANCE OF ELECTRICAL IGNITION SYSTEMS FOR GAS TURBINE ENGINES
- Aerospace Standard
- AIR784C
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine.
To describe those parameters in gas turbine engine design and, in particular, burner configurations that influence the type selection and performance of the ignition system.
To indicate the areas where future work may uncover important effects having a direct bearing on certain interrelated parameters, with resultant benefits to both the engine and ignition designers.
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Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 |
Issuing Committee
E-30 Propulsion Ignition Systems Committee
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