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Relevant bibliographies by topics / Turboprop engines

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Academic literature on the topic 'Turboprop engines'

Author: Grafiati

Published: 4 June 2021

Last updated: 7 February 2022

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Journal articles on the topic "Turboprop engines"

1

Filippone, A., and Z. Mohamed-Kassim. "Multi-disciplinary simulation of propeller-turboprop aircraft flight." Aeronautical Journal 116, no. 1184 (2012): 985–1014. http://dx.doi.org/10.1017/s0001924000007454.

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Abstract This contribution presents a novel simulation for a fixed-wing aircraft powered by gas turbine engines and advanced propellers (turboprops). The work is part of a large framework for the simulation of aircraft flight through a multi-disciplinary approach. Novel numerical methods are presented for flight mechanics, turboprop engine simulation (in direct and inverse mode), and propeller dynamics. We present in detail the integration of the propeller with the airframe, aircraft and tonal noise model. At the basic level, we address a shortfall in multi-disciplinary integration in turbopro

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Saravanamuttoo, H. I. H. "Modern turboprop engines." Progress in Aerospace Sciences 24, no. 3 (1987): 225–48. http://dx.doi.org/10.1016/0376-0421(87)90008-x.

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Nicolosi, Fabrizio, Salvatore Corcione, Vittorio Trifari, and Agostino De Marco. "Design and Optimization of a Large Turboprop Aircraft." Aerospace 8, no. 5 (2021): 132. http://dx.doi.org/10.3390/aerospace8050132.

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This paper proposes a feasibility study concerning a large turboprop aircraft to be used as a lower environmental impact solution to current regional jets operated on short/medium hauls. An overview of this market scenario highlights that this segment is evenly shared between regional turboprop and jet aircraft. Although regional jets ensure a large operative flexibility, they are usually not optimized for short missions with a negative effect on block fuel and environmental impact. Conversely, turboprops represent a greener solution but with reduced passenger capacity and speed. Those aspects

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Skliros, Christos. "A CASE STUDY OF VIBRATION FAULT DIAGNOSIS APPLIED AT ROLLS-ROYCE T-56 TURBOPROP ENGINE." Aviation 23, no. 3 (2020): 78–82. http://dx.doi.org/10.3846/aviation.2019.11900.

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Gas turbine engines include a plethora of rotating modules, and each module consists of numerous components. A component’s mechanical fault can result in excessive engine vibrations. Identification of the root cause of a vibration fault is a significant challenge for both engine manufacturers and operators. This paper presents a case study of vibration fault detection and isolation applied at a Rolls-Royce T-56 turboprop engine. In this paper, the end-to-end fault diagnosis process from starting system faults to the isolation of the engine’s shaft that caused excessive vibrations is described.

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GĘCA, Michał, Zbigniew CZYŻ, and Mariusz SUŁEK. "Diesel engine for aircraft propulsion system." Combustion Engines 169, no. 2 (2017): 7–13. http://dx.doi.org/10.19206/ce-2017-202.

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Stricter requirements for power in engines and difficulties in fueling gasoline engines at the airport make aircraft engine manufac-turers design new engines capable of combusting fuel derived from JET-A1. New materials used in compression-ignition engines enable weight reduction, whereas the technologies of a Common Rail system, supercharging and 2-stroke working cycle enable us to increasethe power generated by an engine of a given displacement. The paper discusses the parameters of about 40 types of aircraft compression ignition engines. The parameters of these engines are compared to the s

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Rabeta, Bismil, Mohammad A.F Ulhaq, Aswan Tajuddin, and Agus Sugiharto. "Simulasi Graphical User Interface Analisis Termodinamika Mesin Turboprop Menggunakan Perangkat Lunak Matlab R2020a." Jurnal Teknologi Kedirgantaraan 6, no. 2 (2021): 31–50. http://dx.doi.org/10.35894/jtk.v6i2.44.

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A turboprop engine is a hybrid engine that delivers thrust or jet thrust and also drives the propeller. This is basically similar to a turbojet except the turbine works through the main shaft which is connected to the reduction gear to rotate the propeller in front of the engine. This research was conducted to determine the development of engine performance in thermodynamic analysis so as to know the value of each parameter on a engine that has been developing for 20 to 50 years with different engine manufacturing. So that in this study a comparison of the thermodynamic analysis of the TPE-331

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Spychała, Jarosław, Paweł Majewski, and Mariusz Żokowski. "The Use of the Vibroacoustic Method for Monitoring the Technical Condition of Aero Engines with Extended Time between Overhauls." Solid State Phenomena 220-221 (January 2015): 283–88. http://dx.doi.org/10.4028/www.scientific.net/ssp.220-221.283.

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The article presents some aspects of several years of work on the use of the vibroacoustic method (Non-Destructive Testing) for assessing a turboprop engine from a trainer aircraft. The functioning engine does not have an operating system for measuring vibration, and therefore the current levels of vibrations and its changes in trends are not known. In order to extend its service life, performing a number of works was required. On the basis of assessing the current state of the engine, opportunities for further exploitation were identified thus developing methodology for evaluating technical c

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Langston, Lee S. "Not So Simple Machines." Mechanical Engineering 135, no. 01 (2013): 30–35. http://dx.doi.org/10.1115/1.2013-jan-3.

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This article talks about evolving technologies in making efficient gears for different auto engines. Gears are integral to a new engine that has the potential to change commercial aviation. Pratt & Whitney’s geared turbofan (GTF) jet engine will have significantly better fuel economy and much quieter operation. The P&W GTF combines existing jet engine technology with the well-established mechanical engineering technology of gears. Due to its high bypass ratio, the geared turbofan engine is 16% more efficient than standard jet engines. A key facility for developing the GTF gearbox has b

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Wandini, Ratna Ayu, Taufiq Mulyanto, and Hari Muhammad. "Estimation of Lateral/Directional Static Stability Characteristics of a Turboprop Aircraft at one Engine Inoperative Condition." Applied Mechanics and Materials 842 (June 2016): 208–16. http://dx.doi.org/10.4028/www.scientific.net/amm.842.208.

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Twin engines turboprop aircraft provides the most beneficial solution to meet the needs of short distance flight due to high fuel efficiency [1]. One of the emergency conditions which has to be considered for this type of the aircraft when one engine is out operating or one engine inoperative because it involves the safety of flight. Furthermore, a safe flight with one engine inoperative is regulated by FAR/CASR Part 25 and has to be complied during certification .Stability and control characteristics of a turboprop aircraft will change significantly if one engine inoperative condition occurs

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Ранченко, Геннадий Степанович, Анна Григорьевна Буряченко, Вячеслав Михайлович Грудинкин та Всеволод Владимирович Данилов. "БАЗОВОЕ ИСПОЛНЕНИЕ РЕГУЛЯТОРА АВИАДВИГАТЕЛЯ И ЕГО МОДИФИКАЦИИ". Aerospace technic and technology, № 8 (31 серпня 2020): 160–65. http://dx.doi.org/10.32620/aktt.2020.8.21.

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It is shown that the creation of a unified electronic control and control equipment for aircraft gas turbine engines is one of the determining trends in the experimental design work of enterprises developing components of aircraft equipment. The results of the creation of some helicopter and aircraft engine controllers (turboshaft and turboprops) in JSC Element are presented. The basic model for them was the regulator RDC-450М (category A component product according to AP-21 classification), which was developed for the AI-450M family of turboshaft engines of Мi-2M and Mi-2MSB and in 2014 recei

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Dissertations / Theses on the topic "Turboprop engines"

1

Jamonet, Laurent 1978. "Testing of a microrocket engine turbopump." Thesis, Massachusetts Institute of Technology, 2002. http://hdl.handle.net/1721.1/8129.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.<br>Includes bibliographical references (p. 191-194).<br>Advances in microfabrication suggest its application to rocket engines. A MEMS thrust chamber producing 50 N of thrust at design point was previously developed that requires propellants pressurized as high as 300 atmospheres. Hence the need for turbopumps at the MEMS scale. A demonstration microturbopump approximately 20x20x6mm in size was designed and built using silicon microfabrication technology. Nitrogen and deionized water are used as

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Deux, Antoine 1975. "Design of a silicon microfabricated rocket engine turbopump." Thesis, Massachusetts Institute of Technology, 2001. http://hdl.handle.net/1721.1/8714.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.<br>Includes bibliographical references (p. 175-178).<br>The advances in silicon microfabrication technology suggest the feasibility of high-precision mechanical devices for power conversion. This thesis describes the design of a silicon demonstration turbopump for a micro-rocket engine, and the analysis and experimental investigation of liquid bearings that may be implemented in a future turbopump. Liquid micro-scale lubrication is investigated. Models are developed to predict the performance of

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Wang, Vincent S. M. Massachusetts Institute of Technology. "Characterization of cavitation instabilities in rocket engine turbopump inducers." Thesis, Massachusetts Institute of Technology, 2016. http://hdl.handle.net/1721.1/107057.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2016.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 135-138).<br>Characterized by super-synchronous rotation of cavities around the periphery of rocket engine turbopump inducers, rotating cavitation is the primary cavitation instability considered in this thesis. A recently developed hypothesis for rotating cavitation onset is assessed through novel experimental analysis and a previously developed body force modeling approach using the MIT inducer, represent

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Kline, Sara E. "Investigation of the Fluid Flow Through the Oil Transfer Sleeve of the PT-06 Turboprop Engine." University of Akron / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=akron1341577847.

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Rutkowski, Richard J. "Cold flow simulation of the alternate turbopump development turbine of the space shuttle main engine high pressure fuel turbopump." Thesis, Monterey, California. Naval Postgraduate School, 1994. http://hdl.handle.net/10945/28034.

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Approved for public release; distribution is unlimited<br>Completion of the installation at the Naval Postgraduate School of a cold-flow test facility for the turbine of the Space Shuttle Main Engine High Pressure Fuel Turbopump is reported. The article to be tested is the first stage of the Alternate Turbopump Development model designed and manufactured by Pratt & Whitney. The purpose of the facility is to enable the development of non- intrusive flow measurements and comparison of those measurements with numerical simulations. Flow field characteristics of the turbine stator were predicted u

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Brown, Joseph R. "Model Identification for the Space Shuttle Main Engine High Pressure Oxidizer Turbopump." Ohio University / OhioLINK, 1992. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1239733713.

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Southward, James D. "Laser doppler velocimetry in the space-shuttle main engine high-pressure fuel turbopump." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA342224.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, March 1998.<br>Thesis advisor(s): Garth V. Hobson. "March 1998." Includes bibliographical references (p. 145-147). Also available online.

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Greco, Philip Andrew. "Turbine performance mapping of the space-shuttle main engine high-pressure fuel turbopump." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1995. http://handle.dtic.mil/100.2/ADA306473.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, September 1995.<br>Thesis advisor(s): Garth V. Hobson. "September 1995." Includes bibliographical references. Also available online.

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Cunha, Marco Antonio Hidalgo. "A computational tool for the design and optimization of supersonic turbines with application on turbopump rocket engines." Instituto Tecnológico de Aeronáutica, 2012. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3218.

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Turbo-machinery design is clearly about making many decisions often under uncertainty and with multiple conflicting objectives. In this work, a computational tool has been developed to assist in the preliminary design optimization of supersonic turbines with application on turbopump rocket engines. It was proposed an evolutive approach based on genetic algorithm to automatize the process of selecting values, based on hands-on experience, for decision variables and fulfill simultaneously decisive compromises faced by the designer. At design point, exploring multiple optima solutions, the tool a

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Yoshida, Brian Richard. "Compuational analysis of boundary layer control by suction in a space transfer vehicle engine turbopump diffuser /." Online version of thesis, 1992. http://hdl.handle.net/1850/11058.

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Books on the topic "Turboprop engines"

1

Hager, Roy D. Advanced turboprop project. Scientific and Technical Information Division, National Aeronautics and Space Administration, 1988.

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Hager, Roy D. Advanced turboprop project. Scientific and Technical Information Division, National Aeronautics and Space Administration, 1988.

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Pant, Rajkumar. GENENG: A generic turboprop engine model. Cranfield University, College of Aeronautics, 1996.

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Gentry, Garl L. Effect of solidity and inclination on propeller-nacelle force coefficients. Langley Research Center, 1991.

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Whitlow, John B. NASA advanced turboprop research and concept validation program. National Aeronautics and Space Administration, 1988.

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6

Heathcote, Roy. The Rolls-Royce Dart: Pioneering turboprop. Rolls-Royce Heritage Trust, 1992.

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7

Warsi, Saif A. User's guide to PMESH - a grid-generation program for single-rotation and counterrotation advanced turboprops. Lewis Research Center, 1989.

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Hanson, Donald B. Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise. Lewis Research Center, 1991.

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Gentry, Garl L. Aerodynamic characteristics of a propeller-powered high-lift semispan wing. Langley Research Center, 1994.

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Metzger, F. B. Benefits of blade sweep for advanced turboprops. AIAA, 1985.

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Book chapters on the topic "Turboprop engines"

1

Greatrix, David R. "Turboprop and Turboshaft Engines." In Powered Flight. Springer London, 2012. http://dx.doi.org/10.1007/978-1-4471-2485-6_8.

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El-Sayed, Ahmed F. "Shaft Engines Turboprop, Turboshaft, and Propfan." In Fundamentals of Aircraft and Rocket Propulsion. Springer London, 2016. http://dx.doi.org/10.1007/978-1-4471-6796-9_7.

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Greatrix, David R. "Erratum to: Turboprop and Turboshaft Engines." In Powered Flight. Springer London, 2012. http://dx.doi.org/10.1007/978-1-4471-2485-6_15.

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Le Brun, Christophe, Emmanuel Godoy, Dominique Beauvois, Bogdan Liacu, and Ricardo Noguera. "Decentralized Control: Application to a Turboprop Engine." In Informatics in Control, Automation and Robotics 12th International Conference, ICINCO 2015 Colmar, France, July 21-23, 2015 Revised Selected Papers. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-31898-1_22.

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Şöhret, Yasin, M. Ziya Sogut, Onder Turan, and T. Hikmet Karakoc. "Sustainability Assessment of a Turboprop Engine: Exergy-Based Method." In Lecture Notes in Energy. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-26950-4_22.

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Coban, Kahraman, Yasin Şöhret, M. Ziya Sogut, Onder Turan, and T. Hikmet Karakoc. "Exergy Approach to Evaluate Performance of a Mini Class Turboprop Engine." In Lecture Notes in Energy. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-26950-4_23.

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Vinay, C. A., and S. Bhaskar Chakravarthy. "Validation of Numerical Analysis Results for Pusher Configured Turboprop Engine Air Intake." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-9601-8_3.

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Atilgan, Ramazan, Onder Turan, and Hakan Aydin. "Exergo-Economic Analysis of an Experimental Aircraft Turboprop Engine Under Low Torque Condition." In Springer Proceedings in Physics. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-05521-3_42.

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Li, Cheng, Chen Lishun, Liang Tao, Guo Li, Cheng Ming, and Zeng Lin. "Features of Singular Value Decomposition and Its Application to the Vibration Monitoring of Turboprop Engine." In Lecture Notes in Electrical Engineering. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-6571-2_181.

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"Appendix K: Turboprop Engine Cycle Analysis." In Aircraft Engine Design, Second Edition. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/5.9781600861444.0589.0608.

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Conference papers on the topic "Turboprop engines"

1

Pegors, Douglas E. "Advanced Allison Small Turboprop Engines." In General Aviation Aircraft Meeting and Exposition. SAE International, 1987. http://dx.doi.org/10.4271/871055.

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Agrawal, Rishabh, Deepanshu Singh, and PMV Subbarao. "Regenerative System for Turboprop Engines." In 15th International Energy Conversion Engineering Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4806.

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Cook, David L. "Development of the PW100 Turboprop Engines." In General Aviation Aircraft Meeting and Exposition. SAE International, 1985. http://dx.doi.org/10.4271/850909.

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Vogt, Robert L., and Arun Sehra. "Next Generation 2 MW Turboshaft and Turboprop Engines." In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/93-gt-046.

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Textron Lycoming of Stratford, Connecticut is incorporating the latest in advanced technology into turboshaft and turboprop engines for near term commercial service. The level of cold section technology being incorporated is the already demonstrated next generation of axi-centrifugal compressor beyond that which was developed for the U.S. Army T800, 0.9 MW turboshaft engine in the late 1980s. The compressor evolution is given special emphasis. The hot section technology is a robust, simplified, low cost, commercial endurance derate of the tri-service; US Army, US Navy, US Air Force and Textron

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Prevallet, L. C. "Single Lever Power Management of Turboprop Engines." In Aerospace Technology Conference and Exposition. SAE International, 1991. http://dx.doi.org/10.4271/912200.

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Rodgers, C. "High Pressure Ratio Intercooled Turboprop Study." In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-405.

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High altitude long endurance unmanned aircraft impose unique contraints on candidate engine propulsion systems and types. Piston, rotary and gas turbine engines have been proposed for such special applications. Of prime importance is the requirement for maximum thermal efficiency (minimum specific fuel consumption) with minimum waste heat rejection. Engine weight, although secondary to fuel economy, must be evaluated when comparing various engine candidates. Weight can be minimized by either high degrees of turbocharging with the piston and rotary engines, or by the high power density capabili

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Marcellan, A., W. P. J. Visser, and P. Colonna. "Potential of Micro Turbine Based Propulsion Systems for Civil UAVs: A Case Study." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-57719.

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There is a high potential for civil applications of Unmanned Aerial Vehicles (UAV) in areas such as goods transport, telecommunication, remote monitoring and sensing, surveillance, search and rescue, and disaster management. Developments in areas such as telecommunication, control and information technology offer opportunities for long range remotely or automatically piloted missions. This requires efficient and light-weight small propulsion systems. The potential of turboprop propulsion for civil UAVs using micro turbine technology has been explored and compared with existing concepts, such a

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Mainville, D., D. Melfi, and M. Whiting. "A Universal Turboprop Engine Dynamometer Test Cell." In ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1991. http://dx.doi.org/10.1115/91-gt-343.

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Pratt & Whitney Canada produces a wide range of aircraft engines and this has led to a concerted effort to standardize and streamline its production engine test facilities. P&WC produce two very different series of turboprop engines, the PW100 with a conventional intake and exhaust arrangement and the PT6 with its reverse flow arrangement. A dynamometer test cell capable of testing both these engine series has been designed and built at Longueuil and is now in operation. The changeover from one model to the other can be carried out by an operator in less than two hours and requires no

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Lopez-Diez, Alfredo, Luis Ruiz-Calavera, Javier Castillo-Calvo, and Raul Prieto-Ibañez. "Front End Optimization of High Speed Turboprop Engines." In 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-4204.

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Faltot, Pierre-Jean, Daniela Pitel Welnitz, Philippe Vertenoeuil, Tomas Vlach, Luca Lombardi, and Michele D’Ercole. "Analysis and Testing of Aerobatic Turboprop Aircraft Inlet." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-76398.

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Aerobatic aircraft have become popular for the training of military pilots, and nowadays an increasing number of such airframes are being developed. Modern turboprop engines provide high performance allowing the pilots to get similar handling characteristics to military jet aircraft engines. Prior to the availability of high performance turboprops, the basic pilot training was conducted using jet aircraft. Furthermore, the introduction of electronic control systems on last-generation turboprop engines enables single lever control, making it an ideal candidate for this type of aerobatic and tra

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