A high-pressure, blow-down type turbine combustor test facility is reported that has a capacity of up to 30 atm of air from ambient temperature to 720 K. The test section can supply an airflow rate of either 10 kg/s in weight or 0.6 cu m/s in volume at the maximum. The combustor inlet temperature and pressure are independently regulated. Test duration is limited to between 60 and 100 seconds depending on the experimental condition. Control of the facility and experimental measurements are conducted by a minicomputer.


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    Title :

    A High-Pressure, Sector-Shaped Model Combustor Test Facility for Development of Turbofan Engines


    Contributors:
    K. Suzuki (author) / K. Nishio (author) / S. Horiuchi (author) / M. Koshinuma (author) / Y. Kabe (author)

    Publication date :

    1977


    Size :

    32 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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