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    A New Intermittent Aspirated Probe for the Measurement of Stagnation Quantities in High Temperature Gases

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 004::page 41022
    Author:
    Michela Massini
    ,
    Robert J. Miller
    ,
    Howard P. Hodson
    DOI: 10.1115/1.4002414
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the design, manufacture, and testing of a new probe for the measurement of temperature and pressure in engine environments. The probe consists of a choked nozzle located in the flow and a system downstream including a cooler, a flow measuring device, and a valve. It operates in two modes: In the first mode the valve is open, the probe is aspirated, and the nozzle is choked. The mass flow through the probe is measured using instrumentation placed downstream of the cooler, so that it does not have contact with the hot flow. In the second mode, the valve is closed, and the stagnation pressure is measured using the same instrumentation downstream the cooler. The total temperature is computed as a derived variable from the measurements of stagnation pressure and mass flow rate. There are a number of advantages of the probe over existing methods of temperature measurement. The measurement inaccuracy due to conduction and radiation errors and calibration drift found in thermocouples is significantly reduced; it can measure both stagnation temperature and pressure, halving the instrumentation costs; it has no wiring or transducer in the sensor head; the system can self-calibrate while located within an engine. This paper describes the design of a probe for use in engine environments. The probe prototype is tested up to 900 K and is shown to have an accuracy of ±6 K.
    keyword(s): Temperature , Measurement , Pressure , Calibration , Probes , Flow (Dynamics) , Engines , Nozzles , Errors AND Thermocouples ,
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      A New Intermittent Aspirated Probe for the Measurement of Stagnation Quantities in High Temperature Gases

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    http://yetl.yabesh.ir/yetl1/handle/yetl/147774
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    • Journal of Turbomachinery

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    contributor authorMichela Massini
    contributor authorRobert J. Miller
    contributor authorHoward P. Hodson
    date accessioned2017-05-09T00:47:19Z
    date available2017-05-09T00:47:19Z
    date copyrightOctober, 2011
    date issued2011
    identifier issn0889-504X
    identifier otherJOTUEI-28776#041022_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/147774
    description abstractThis paper presents the design, manufacture, and testing of a new probe for the measurement of temperature and pressure in engine environments. The probe consists of a choked nozzle located in the flow and a system downstream including a cooler, a flow measuring device, and a valve. It operates in two modes: In the first mode the valve is open, the probe is aspirated, and the nozzle is choked. The mass flow through the probe is measured using instrumentation placed downstream of the cooler, so that it does not have contact with the hot flow. In the second mode, the valve is closed, and the stagnation pressure is measured using the same instrumentation downstream the cooler. The total temperature is computed as a derived variable from the measurements of stagnation pressure and mass flow rate. There are a number of advantages of the probe over existing methods of temperature measurement. The measurement inaccuracy due to conduction and radiation errors and calibration drift found in thermocouples is significantly reduced; it can measure both stagnation temperature and pressure, halving the instrumentation costs; it has no wiring or transducer in the sensor head; the system can self-calibrate while located within an engine. This paper describes the design of a probe for use in engine environments. The probe prototype is tested up to 900 K and is shown to have an accuracy of ±6 K.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleA New Intermittent Aspirated Probe for the Measurement of Stagnation Quantities in High Temperature Gases
    typeJournal Paper
    journal volume133
    journal issue4
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4002414
    journal fristpage41022
    identifier eissn1528-8900
    keywordsTemperature
    keywordsMeasurement
    keywordsPressure
    keywordsCalibration
    keywordsProbes
    keywordsFlow (Dynamics)
    keywordsEngines
    keywordsNozzles
    keywordsErrors AND Thermocouples
    treeJournal of Turbomachinery:;2011:;volume( 133 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian