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E-30 Propulsion Ignition Systems Committee
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INTERRELATION OF ENGINE DESIGN AND BURNER CONFIGURATION WITH SELECTION AND PERFORMANCE OF ELECTRICAL IGNITION SYSTEMS FOR GAS TURBINE ENGINES

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • AIR784B
  • Current
Published 2011-08-10 by SAE International in United States
To describe typical ignition systems in general usage and their parameters that warrant consideration during the development of a gas turbine engine.
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Spark Igniter Outline - .500-20 Threaded Mounting

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • AS815
  • Current
Published 2002-12-16 by SAE International in United States
No Abstract Available.
 

Terminal, High Altitude, Socket Contact

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • ARP296
  • Current
Published 2002-07-23 by SAE International in United States
No Abstract Available.
 

Spark Energy Measurements Using Oscilloscopic Methods

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • AIR77
  • Current
Published 1998-12-01 by SAE International in United States
No Abstract Available.
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Spark Energy Measurement, Alternative Methods

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • AIR951A
  • Current
Published 1998-08-01 by SAE International in United States
Parameters to consider and various methods of measuring spark energy of aviation ignition systems.
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Spark Plug Rating Calibration

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • ARP890A
  • Current
Published 1998-08-01 by SAE International in United States
Procedure for obtaining the corrected heat-rating values (indicated mean effective pressure, IMEP) of spark plugs rated in the SAE 17.6 cubic inch rating engine (SAE AS840).
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Magnetos, Aircraft, Mountings For

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • AS12
  • Current
Published 1997-04-01 by SAE International in United States
This specification covers three types of flanges for magneto mountings as follows: 1. Two-bolt Flange, 2. Three-bolt Flange, and 3. Four-bolt Flange.
 

IGNITION SHIELDING, AIRCRAFT

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • AS29
  • Current
Published 1996-11-01 by SAE International in United States
This standard covers two basic types of ignition shielding as follows: Type I - Unfilled Type II - Filled
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TERMINALS, AIRCRAFT IGNITION

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • ARP670B
  • Current
Published 1995-11-01 by SAE International in United States
No Abstract Available.
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INTERRELATION OF ENGINE DESIGN AND BURNER CONFIGURATION WITH SELECTION AND PERFORMANCE OF ELECTRICAL IGNITION SYSTEMS FOR GAS TURBINE ENGINES

E-30 Propulsion Ignition Systems Committee
  • Aerospace Standard
  • AIR784C
  • Historical
Published 1995-06-01 by SAE International in United States
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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