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Tytuł artykułu

Oveview of modern and advanced techniques in jet engine testing

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Warianty tytułu
PL
Przegląd nowoczesnych i zaawansowanych technik w testowaniu silników odrzutowych
Języki publikacji
EN
Abstrakty
EN
Presented work describes an overview of techniques, probes and sensors as well as methods used in modern and advanced jet engine testing. The main goal of the article is to present complexity of the subject and to obtain knowledge and survey about future undertaken research. Paper is based on broadly considered bibliography and describes various methods of measurement. Within the first chapter temperature measurement methods are shown. Usage of the most popular technique, which considers thermocouples, is described in contrary to noncontact temperature acquisition using pyrometer. Both traditional and alternatives noncontact pressure measurement techniques are mentioned in the next part. Author underlined following chapter showing few different ways of stress and vibration measurement. Conventional, using strain gauges; modern, using Fiber Optic Bragg Sensor, as an example of intrusive techniques are shown. Additionally noncontact stress and vibration measurement examples are described using eddy current, capacitive and optical probes.
PL
Prezentowana praca przedstawia przegląd technik oraz czujników pomiarowych użytych w nowoczesnych metodach do testowania silników odrzutowych. Głównym celem pracy jest przedstawienie złożoności zagadnienia oraz zdobycie wiedzy na prezentowany temat. Praca oparta jest na rozbudowanej konferencyjnej bibliografii oraz dziennikach branżowych z ostatnich lat. W pierwszej części artykułu zostały opisane metody pomiaru temperatury. Przedstawiono charakterystykę najpopularniejszej z metod - wykorzystującą użycie termopary i porównano ją z wybraną techniką bezkontaktową - wykorzystującą pyrometr. Omówiono tradycyjne i alternatywne oraz bezkontaktowe sposoby pomiaru ciśnienia i zachowania się przepływu wewnątrz silnika. Przedstawiono również kilka metod pomiaru naprężeń i drgań w silniku lotniczym. Metody inwazyjne, konwencjonalne, wykorzystujące do pomiaru zarówno tensometry, jak i nowoczesne czujniki Bragga, zostały porównane z metodami nieinwazyjnymi. Dodatkowo opisano przykłady technik wykorzystujących czujniki prądów błądzących, pojemnościowe i optyczne.
Rocznik
Strony
65--74
Opis fizyczny
Bibliogr. 36 poz.
Twórcy
autor
  • Politechnika Rzeszowska
Bibliografia
  • [1] Abdullahi H., Kotulla M., Staudacher S.: A new method for online monitoring and trimming of pyrometer measurements in high performance turbo engines, AIAA, 2003-1195.
  • [2] Andersen H., Hartman T., Pen-Chung C.: Advanced gas turbine monitoring and diagnostics technology for modern power plants, International Joint Power Generation Conference, Atlanta, Georgia, USA 2003.
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  • [4] Brouckaert J.-F., Mersinligil M., Pau M.: A conceptual design study for a new high temperature fast response cooled total pressure probe, ASME Turbo Expo: Power for Land, Sea and Air, Berlin, Germany 2008.
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  • [6] Cradwell D.N., Ghana K.S., Russhard P.: The use of eddy current sensors for the measurement of rotor blade tip timing - sensor development and engine testing, ASME Turbo Expo: Power for Land, Sea and Air, Berlin, Germany, 2008.
  • [7] Dudzinski T. J., Krause L.N.: Effect of inlet geometry on flow-angle characteristics of miniature total-pressure tubes, National Aeronautics and Space Administration Technical Note, Washington D.C., USA 1971.
  • [8] Frank S.L.F., Lechner C., Mertens B., Warnack D.: Testing the latest model V84.3A gas turbine in the Siemens test facility in Berlin, ASME Turbo Expo, New Orleans, Louisiana, USA 2001.
  • [9] Goettlich E., Malzacher F., Heitmeier F., Marn A.: Adaptation of a transonic test turbine facility for experimental investigation of aggressive intermediate turbine duct flows, AIAA, 2005.
  • [10] Gregory J.W., Sullivan J.P.: Effect of quenching kinetics on unsteady response of pressure-sensitive paint, AIAA Journal, vol. 44, no 3, 2006.
  • [11] Knoell H., Ding K.: Tip clearance measurement in modern compressor components, Advanced Instrumentation for Aero Engines Components Conference, Philadelphia, Pennsylvania, USA 1986.
  • [12] Kolhe P.S., Agrawal A.K.: Density measurement in a supersonic microjet using miniature rainbow schlieren deflectometry, AIAA Journal, vol. 47, no 4, 2009.
  • [13] Kreuzer M.: Strain measurement with fiber optic Bragg sensor, Hottinger Baldwin Messtechnik, Darmstadt, Germany 2006.
  • [14] Lempert W.R.: Introduction to aerodynamic measurement technology special section, AIAA Journal, vol. 40, no 6, 2002.
  • [15] Long D.F., Pipkin J.: Optical measurement of flow conditions on model scale engine exhaust system, 39th AIAA/ASME/SEA/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, USA 2003.
  • [16] Massini M., Miller R.J., Hodson H.P.: A new intermitten aspirated probe for the measurement of stagnation quantities in high temperature gases, ASME Turbo Expo: Power for Land, Sea and Air, Berlin, Germany 2008.
  • [17] Mckenzie R.L.: Three-dimensional planar Doppler velocity measurement in a full-scale rotor wake, AIAA Journal, vol. 43, no 3, 2005.
  • [18] Melcher K.J., Kypuros J.: Toward a fast-response active turbine tip clearance control, AIAA, 2003.
  • [19] Mielke A.F., Elam K. A., Sung C.-J.: Multiproperty measurements at high sampling rates using Rayleigh scattering, AIAA Journal, vol. 47, no 4, 2009.
  • [20] Mueller M.W., Schiffer H.P., Viges M., Ascherp C.: Experimental investigation of the rotor/casing treatment interaction in axial single-stage transonic compressor, Technische Universitaet Darmstad, Dept. of Gas Turbines and Aerospace propulsion; German Aerospace Center (DLR), Institute for Propulsion Technology, Cologne, MTU Aero Engines, Munich, Germany.
  • [21] Naik S.V., Kulatilaka W.D., Venkatesan K.K., Lucht R.P.: Pressure, temperature, and velocity measurement in underexpanded jets using laser induced fluorescence imaging, AIAA Journal, vol. 47, no 4, 2009.
  • [22] Pisasale A.J., Ahmed N.A.: Examining the effect of flow reversal on seven-hole probe measurements, AIAA Journal, vol. 41, no 12, 2003.
  • [23] Porreca L., Hollenstein M., Kalfas A.I., Abhari R.S.: Turbulence measurements and analysis in a multistage axial turbine, Turbomachinery Laboratory, Swiss Federal Institute of Technology, Zurich, Switzerland.
  • [24] Pulliam W., Russler P.: High-temperature, high bandwidth, fiber-optic, MEMS pressure sensor technology for turbine engine component testing, Instrumentation, Systems and Automation Conference, Houston, TX, USA 2001.
  • [25] Ramakrishnan V., Rediniotis O.K.: Development of a 12-hole omnidifferectional flow-velocity measurement probe, AIAA Journal, vol. 45, no 6, 2007.
  • [26] Ruyten W.: Sensitivity analysis of three-gate lifetime pressure- and temperature-sensitive paint measurements, AIAA Journal, vol. 45, no 1, 2007.
  • [27] Smith V.K., Albro J.R., More M.: New aeropropulsion ground test tools for accelerated engine life assessment, 37th AIAA/ASME/SEA/ASEE Joint Propulsion Conference and Exhibit, Salt Lake City, USA 2001.
  • [28] Turco D.P., D’Ercole M., Gamberi F., De Prosperis R., Pieroni N., Mariotti M.: Modelling and measuring experiences to evaluate the modal behavior of an industrial gas turbine high pressure bucket, ASME Turbo Expo: Power for the Land, Sea and Air, Montreal, Canada 2007.
  • [29] Vacher F., Alves F., Gilles-Pascaud C.: Eddy current nondestructive testing with giant magneto-impedance sensor, NDT&E International, 2007.
  • [30] Watkins A.N., Nuck G.M., Leighty B.D., Lipford W.E.: Using pressure- and temperature-sensitive paint on the aftbody of a capsule vehicle, AIAA Journal, vol. 47, no 4, 2009.
  • [31] Weiss J., Chokani N., Comte-Bellot G.: Constant-temperature and constant=voltage anemometer use in a Mach 2.5 flow, AIAA Journal, vol. 43, no 5, 2005.
  • [32] Woodmansee M.A., Iyer V., Dutton J.C., Lucht R.P.: Nonintrusive pressure and temperature measurements in a underexpanded sonic jet flowfield, AIAA Journal, vol. 42, no 6, 2004.
  • [33] www.wikipedia.pl
  • [34] Zeisberger A.: Total temperature probes for turbine and combustor applications. AIAA, 2007.
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  • [36] Zieliński M., Ziller G.: Noncontact vibration measurements on compressor rotor blades, Measurement Science Technology, no 11, 2000.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-PWA9-0055-0018
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