Advanced Control of Turbofan Engines

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Publisher : Springer Science & Business Media
ISBN 13 : 1461411718
Total Pages : 275 pages
Book Rating : 4.4/5 (614 download)

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Book Synopsis Advanced Control of Turbofan Engines by : Hanz Richter

Download or read book Advanced Control of Turbofan Engines written by Hanz Richter and published by Springer Science & Business Media. This book was released on 2011-10-20 with total page 275 pages. Available in PDF, EPUB and Kindle. Book excerpt: Advanced Control of Turbofan Engines describes the operational performance requirements of turbofan (commercial) engines from a controls systems perspective, covering industry-standard methods and research-edge advances. This book allows the reader to design controllers and produce realistic simulations using public-domain software like CMAPSS: Commercial Modular Aero-Propulsion System Simulation, whose versions are released to the public by NASA. The scope of the book is centered on the design of thrust controllers for both steady flight and transient maneuvers. Classical control theory is not dwelled on, but instead an introduction to general undergraduate control techniques is provided. Advanced Control of Turbofan Engines is ideal for graduate students doing research in aircraft engine control and non-aerospace oriented control engineers who need an introduction to the field.

Systems of Commercial Turbofan Engines

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Publisher : Springer Science & Business Media
ISBN 13 : 3540736190
Total Pages : 239 pages
Book Rating : 4.5/5 (47 download)

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Book Synopsis Systems of Commercial Turbofan Engines by : Andreas Linke-Diesinger

Download or read book Systems of Commercial Turbofan Engines written by Andreas Linke-Diesinger and published by Springer Science & Business Media. This book was released on 2008-05-21 with total page 239 pages. Available in PDF, EPUB and Kindle. Book excerpt: To understand the operation of aircraft gas turbine engines, it is not enough to know the basic operation of a gas turbine. It is also necessary to understand the operation and the design of its auxiliary systems. This book fills that need by providing an introduction to the operating principles underlying systems of modern commercial turbofan engines and bringing readers up to date with the latest technology. It also offers a basic overview of the tubes, lines, and system components installed on a complex turbofan engine. Readers can follow detailed examples that describe engines from different manufacturers. The text is recommended for aircraft engineers and mechanics, aeronautical engineering students, and pilots.

Aircraft Engine Controls

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Publisher : AIAA Education
ISBN 13 : 9781600867057
Total Pages : 0 pages
Book Rating : 4.8/5 (67 download)

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Book Synopsis Aircraft Engine Controls by : Link C. Jaw

Download or read book Aircraft Engine Controls written by Link C. Jaw and published by AIAA Education. This book was released on 2009 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Overview of engine control systems -- Engine modeling and simulation -- Model reduction and dynamic analysis -- Design of set-point controllers -- Design of transient and limit controllers -- Control system integration -- Advanced control concepts -- Engine monitoring and health management -- Integrated control and health monitoring -- Appendix A. Fundamentals of automatic control systems -- Appendix B. Gas turbine engine performance and operability.

Advanced Control System for Turbofan Engine: Multivariable Control and Fuzzy Logic. (Applicatoin to the M88-2 Engine)

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Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)

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Book Synopsis Advanced Control System for Turbofan Engine: Multivariable Control and Fuzzy Logic. (Applicatoin to the M88-2 Engine) by : Alain Garassino

Download or read book Advanced Control System for Turbofan Engine: Multivariable Control and Fuzzy Logic. (Applicatoin to the M88-2 Engine) written by Alain Garassino and published by . This book was released on 1995 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine and Aeroengine Congress and Exposition, Houston, Texas - June 5-8, 1995.

Advanced Control for Airbreathing Engines, Volume 1: Pratt and Whitney

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Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Advanced Control for Airbreathing Engines, Volume 1: Pratt and Whitney by :

Download or read book Advanced Control for Airbreathing Engines, Volume 1: Pratt and Whitney written by and published by . This book was released on 1993 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Control Design for an Advanced Geared Turbofan Engine

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Publisher :
ISBN 13 :
Total Pages : 14 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Control Design for an Advanced Geared Turbofan Engine by : Jeffryes Chapman (W.)

Download or read book Control Design for an Advanced Geared Turbofan Engine written by Jeffryes Chapman (W.) and published by . This book was released on 2017 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Commercial Aircraft Propulsion and Energy Systems Research

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Publisher : National Academies Press
ISBN 13 : 0309440998
Total Pages : 123 pages
Book Rating : 4.3/5 (94 download)

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Book Synopsis Commercial Aircraft Propulsion and Energy Systems Research by : National Academies of Sciences, Engineering, and Medicine

Download or read book Commercial Aircraft Propulsion and Energy Systems Research written by National Academies of Sciences, Engineering, and Medicine and published by National Academies Press. This book was released on 2016-08-09 with total page 123 pages. Available in PDF, EPUB and Kindle. Book excerpt: The primary human activities that release carbon dioxide (CO2) into the atmosphere are the combustion of fossil fuels (coal, natural gas, and oil) to generate electricity, the provision of energy for transportation, and as a consequence of some industrial processes. Although aviation CO2 emissions only make up approximately 2.0 to 2.5 percent of total global annual CO2 emissions, research to reduce CO2 emissions is urgent because (1) such reductions may be legislated even as commercial air travel grows, (2) because it takes new technology a long time to propagate into and through the aviation fleet, and (3) because of the ongoing impact of global CO2 emissions. Commercial Aircraft Propulsion and Energy Systems Research develops a national research agenda for reducing CO2 emissions from commercial aviation. This report focuses on propulsion and energy technologies for reducing carbon emissions from large, commercial aircraftâ€" single-aisle and twin-aisle aircraft that carry 100 or more passengersâ€"because such aircraft account for more than 90 percent of global emissions from commercial aircraft. Moreover, while smaller aircraft also emit CO2, they make only a minor contribution to global emissions, and many technologies that reduce CO2 emissions for large aircraft also apply to smaller aircraft. As commercial aviation continues to grow in terms of revenue-passenger miles and cargo ton miles, CO2 emissions are expected to increase. To reduce the contribution of aviation to climate change, it is essential to improve the effectiveness of ongoing efforts to reduce emissions and initiate research into new approaches.

Aircraft Turbine Engine Control Research at NASA Glenn Research Center

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Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.6/5 (72 download)

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Book Synopsis Aircraft Turbine Engine Control Research at NASA Glenn Research Center by : National Aeronaut Administration (Nasa)

Download or read book Aircraft Turbine Engine Control Research at NASA Glenn Research Center written by National Aeronaut Administration (Nasa) and published by . This book was released on 2020-08-05 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper provides an overview of the aircraft turbine engine control research at the NASA Glenn Research Center (GRC). A brief introduction to the engine control problem is first provided with a description of the state-of-the-art control law structure. A historical aspect of engine control development since the 1940s is then provided with a special emphasis on the contributions of GRC. With the increased emphasis on aircraft safety, enhanced performance, and affordability, as well as the need to reduce the environmental impact of aircraft, there are many new challenges being faced by the designers of aircraft propulsion systems. The Controls and Dynamics Branch (CDB) at GRC is leading and participating in various projects to develop advanced propulsion controls and diagnostics technologies that will help meet the challenging goals of NASA Aeronautics Research Mission programs. The rest of the paper provides an overview of the various CDB technology development activities in aircraft engine control and diagnostics, both current and some accomplished in the recent past. The motivation for each of the research efforts, the research approach, technical challenges, and the key progress to date are summarized. Garg, Sanjay Glenn Research Center NASA/TM-2013-217821, E-18277-1 WBS 432938.11.01.03.02.02.15 AIRCRAFT ENGINES; TURBINE ENGINES; ENGINE CONTROL; PROPULSION SYSTEM PERFORMANCE; PROPULSION SYSTEM CONFIGURATIONS; HISTORIES; CONTROL THEORY; TURBOFAN ENGINES; AIRCRAFT MODELS; SENSORS; FAULT DETECTION; ENGINE FAILURE

Advanced Aero-engine Concepts and Controls

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Author :
Publisher :
ISBN 13 :
Total Pages : 432 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Advanced Aero-engine Concepts and Controls by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Symposium

Download or read book Advanced Aero-engine Concepts and Controls written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Symposium and published by . This book was released on 1996 with total page 432 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aircraft Engine Design

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Publisher : AIAA
ISBN 13 : 9781600860164
Total Pages : 732 pages
Book Rating : 4.8/5 (61 download)

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Book Synopsis Aircraft Engine Design by : Jack D. Mattingly

Download or read book Aircraft Engine Design written by Jack D. Mattingly and published by AIAA. This book was released on 2002 with total page 732 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation A design textbook attempting to bridge the gap between traditional academic textbooks, which emphasize individual concepts and principles; and design handbooks, which provide collections of known solutions. The airbreathing gas turbine engine is the example used to teach principles and methods. The first edition appeared in 1987. The disk contains supplemental material. Annotation c. Book News, Inc., Portland, OR (booknews.com).

Development and Validation of a Civil Aircraft Engine Simulation Model for Advanced Controller Design

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Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (757 download)

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Book Synopsis Development and Validation of a Civil Aircraft Engine Simulation Model for Advanced Controller Design by : Sonny Martin

Download or read book Development and Validation of a Civil Aircraft Engine Simulation Model for Advanced Controller Design written by Sonny Martin and published by . This book was released on 2010 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: This thesis is concerned with the results of a joint academic and industrial study on the development of a detailed nonlinear dynamic model of a turbofan jet engine to be used for research into advanced control strategies for civil turbofan aircraft engines. The model is representative of a dual shaft engine with variable bleed, variable stator vanes, turbine cooling, heat transfer, and a duct and exhaust nozzle. A switched, gain-scheduled, feedback control system incorporating bumpless transfer and antiwindup functionality has been designed and implemented according to current industrial practice. This baseline implementation permits realistic transient operation of the simulation and may act as a reference design for further control work. The simulation computes a non-iterative solution, by progressing calculations in the direction of the gas stream flow. Where possible the underlying physics are used and empirical approximations are avoided so that the model requires minimum data. This approach also makes a future inclusion of component failure easier to implement. The simulation is modular in nature so that engine or control modules can be easily replaced or modified if an improved design becomes available. The Simulink implementation of the control architecture has been redesigned to permit the addition or removal of control loops, also during the simulation?s operation, to allow testing of advanced control strategies. The entire controller can also be easily replaced. A detailed description of the modeling process, the various simulation issues that arise with a model of this complexity, and the results of the overall aero-engine system are presented. The design of the switched, gain-scheduled aero-engine controller with bumpless transfer and antiwindup which achieves dynamic performance that closely matches that of a real aero-engine is also discussed.

Digital Implementation of the TF30-P-3 Turbofan Engine Control

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Author :
Publisher :
ISBN 13 :
Total Pages : 68 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Digital Implementation of the TF30-P-3 Turbofan Engine Control by : David S. Cwynar

Download or read book Digital Implementation of the TF30-P-3 Turbofan Engine Control written by David S. Cwynar and published by . This book was released on 1975 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Active Control of Inlet Noise on the Jt15d Turbofan Engine

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781720369615
Total Pages : 58 pages
Book Rating : 4.3/5 (696 download)

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Book Synopsis Active Control of Inlet Noise on the Jt15d Turbofan Engine by : National Aeronautics and Space Administration (NASA)

Download or read book Active Control of Inlet Noise on the Jt15d Turbofan Engine written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-29 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the key results obtained by the Vibration and Acoustics Laboratories at Virginia Tech over the year from November 1997 to December 1998 on the Active Noise Control of Turbofan Engines research project funded by NASA Langley Research Center. The concept of implementing active noise control techniques with fuselage-mounted error sensors is investigated both analytically and experimentally. The analytical part of the project involves the continued development of an advanced modeling technique to provide prediction and design guidelines for application of active noise control techniques to large, realistic high bypass engines of the type on which active control methods are expected to be applied. Results from the advanced analytical model are presented that show the effectiveness of the control strategies, and the analytical results presented for fuselage error sensors show good agreement with the experimentally observed results and provide additional insight into the control phenomena. Additional analytical results are presented for active noise control used in conjunction with a wavenumber sensing technique. The experimental work is carried out on a running JT15D turbofan jet engine in a test stand at Virginia Tech. The control strategy used in these tests was the feedforward Filtered-X LMS algorithm. The control inputs were supplied by single and multiple circumferential arrays of acoustic sources equipped with neodymium iron cobalt magnets mounted upstream of the fan. The reference signal was obtained from an inlet mounted eddy current probe. The error signals were obtained from a number of pressure transducers flush-mounted in a simulated fuselage section mounted in the engine test cell. The active control methods are investigated when implemented with the control sources embedded within the acoustically absorptive material on a passively-lined inlet. The experimental results show that the combination of active control techniques with fuselage-

Control Mode Studies for Advanced Variable-Geometry Turbine Engines

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Publisher :
ISBN 13 :
Total Pages : 89 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Control Mode Studies for Advanced Variable-Geometry Turbine Engines by : Edward C. Beattie

Download or read book Control Mode Studies for Advanced Variable-Geometry Turbine Engines written by Edward C. Beattie and published by . This book was released on 1974 with total page 89 pages. Available in PDF, EPUB and Kindle. Book excerpt: This program addressed the definition and refinement of control modes for a variable cycle, non-mixed exhaust, turbofan engine incorporation fan and compressor vanes, variable high and low-pressure turbine nozzle areas, Under a previous Air Force contract, a control mode for a nonaugmented version of this engine was developed utilizing a dynamic computer simulation of the engine, and operation was demonstrated over a range of flight conditions. Under the program reported herein, this control mode was updated and refined to enable satisfactory transient response over a typical military flight envelope to meet MIL-E-5007C requirements. An implementable control scheduling approach was also developed to provide compliance with steady-state engine rating requirements.

Advanced Detection, Isolation, and Accommodation of Sensor Failures in Turbofan Engines

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Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722048945
Total Pages : 34 pages
Book Rating : 4.0/5 (489 download)

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Book Synopsis Advanced Detection, Isolation, and Accommodation of Sensor Failures in Turbofan Engines by : National Aeronautics and Space Administration (NASA)

Download or read book Advanced Detection, Isolation, and Accommodation of Sensor Failures in Turbofan Engines written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-06-30 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of the Advanced Detection, Isolation, and Accommodation Program is to improve the overall demonstrated reliability of digital electronic control systems for turbine engines. For this purpose, an algorithm was developed which detects, isolates, and accommodates sensor failures by using analytical redundancy. The performance of this algorithm was evaluated on a real time engine simulation and was demonstrated on a full scale F100 turbofan engine. The real time implementation of the algorithm is described. The implementation used state-of-the-art microprocessor hardware and software, including parallel processing and high order language programming. Delaat, John C. and Merrill, Walter C. Glenn Research Center RTOP 505-62-01...

Advanced Detection, Isolation, and Accommodation of Sensor Failures in Turbofan Engines

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Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Advanced Detection, Isolation, and Accommodation of Sensor Failures in Turbofan Engines by : John C. DeLaat

Download or read book Advanced Detection, Isolation, and Accommodation of Sensor Failures in Turbofan Engines written by John C. DeLaat and published by . This book was released on 1990 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Up Den Hansedach to Lueneborch 1889

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Publisher :
ISBN 13 :
Total Pages : 2 pages
Book Rating : 4.:/5 (249 download)

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Book Synopsis Up Den Hansedach to Lueneborch 1889 by :

Download or read book Up Den Hansedach to Lueneborch 1889 written by and published by . This book was released on 1889 with total page 2 pages. Available in PDF, EPUB and Kindle. Book excerpt: