COMBUSTION CHAMBER FOR GAS TURBINE ENGINE

FIELD: gas turbine engine engineering. ^ SUBSTANCE: combustion chamber comprises housing provided with inner and outer ring shells, device for graduate change of the ratio of areas of the cross-sections of primary and secondary passages, and collector stabilizer. The reaction zone has shutters and i...

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Bibliographische Detailangaben
Hauptverfasser:	PERESLAVTSEV ANDREJ VIKTOROVICH, MAJATSKIJ SERGEJ ALEKSANDROVICH, PRONIN ALEKSEJ JUR'EVICH, SHAPKO IVAN VITAL'EVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION APPARATUS COMBUSTION PROCESSES GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	FIELD: gas turbine engine engineering. ^ SUBSTANCE: combustion chamber comprises housing provided with inner and outer ring shells, device for graduate change of the ratio of areas of the cross-sections of primary and secondary passages, and collector stabilizer. The reaction zone has shutters and inserts that define inner and outer rings. The shutters and inserts are pivotally interconnected for permitting change of the area of the cross-section in radial direction. The collector stabilizer is unmovable. ^ EFFECT: enhanced reliability. ^ 4 dwg