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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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