Experimental development of a plasma spark plug for GTE altitude start

Experimental development of a plasma spark plug for GTE altitude start

A working process of a plasma spark plug is described and its improved structure that meets the requirements for start and operation stability limits is given. Also presented are the results of the plug tests under conditions of rarefaction to confirm its normal operation at the GTE altitude start.

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Veröffentlicht in:Russian aeronautics 2010-06, Vol.53 (2), p.235-241
Hauptverfasser: Mikhailov, V. V., Lebedev, V. V., Mukhin, A. N.
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft and Rocket Engine Design and Development
Altitude
Automotive Engineering
Engineering
Rarefaction
Spark plugs
Stability
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Beschreibung
Zusammenfassung:A working process of a plasma spark plug is described and its improved structure that meets the requirements for start and operation stability limits is given. Also presented are the results of the plug tests under conditions of rarefaction to confirm its normal operation at the GTE altitude start.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799810020194