GAS TURBINE COMBUSTOR

GAS TURBINE COMBUSTOR

PURPOSE:To make it possible to provide a certain allowance for the combustion range of the combustor by connecting a combustion compartment to an exhaust compartment via a bypass pipe provided with a control valve for adjusting the amount of air within the combustion compartment, and exhausting bypa...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SAEKI HIROBUMI, IKEGAMI YASUHIKO, SASAMOTO FUJIO
Format: Patent
Sprache:eng
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:PURPOSE:To make it possible to provide a certain allowance for the combustion range of the combustor by connecting a combustion compartment to an exhaust compartment via a bypass pipe provided with a control valve for adjusting the amount of air within the combustion compartment, and exhausting bypass air into the exhaust compartment. CONSTITUTION:The amount of air within a combustion compartment 108 which has been exhausted out of a compressor 101 is controlled from the outside by means of a bypass pipe 112 provided with a control valve 113. Thus, the amount of air which is optimum for continuing to ignite or burn two burners 104 and 106 is secured. As a result, it is possible to reduce the unignition phenomena and load variations to be burdened on the gas turbine at the time of changing a single movement over to a combined operation.