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Keywords: engine
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Proceedings Papers
Proc. ASME. GT2024, Volume 11: Supercritical CO2, V011T28A049, June 24–28, 2024
Publisher: American Society of Mechanical Engineers
Paper No: GT2024-129421
... Abstract In the context of advancing aviation technology towards greater efficiency and reduced environmental impact, the design of a Microtube Precooler Heat Exchanger integrated with a Waste Heat Recovery System (WHRS) for a Jet Engine fuel system has emerged. The primary objective...
Proceedings Papers
Proc. ASME. GT2023, Volume 1: Aircraft Engine, V001T01A028, June 26–30, 2023
Publisher: American Society of Mechanical Engineers
Paper No: GT2023-103166
...Proceedings of ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition GT2023 June 26-30, 2023, Boston, Massachusetts, USA GT2023-103166 IMPACT OF SCO2 WASTE HEAT RECOVERY SYSTEM AIR COOLER INTEGRATION ON AIRCRAFT ENGINE THRUST PERFORMANCE Claire-Phonie Bury University of Central...
Proceedings Papers
Proc. ASME. GT2023, Volume 1: Aircraft Engine, V001T01A021, June 26–30, 2023
Publisher: American Society of Mechanical Engineers
Paper No: GT2023-102238
...Proceedings of ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition GT2023 June 26-30, 2023, Boston, Massachusetts, USA GT2023-102238 THRUST REBALANCE TO EXTEND ENGINE TIME ON-WING WITH CONSIDERATION OF ENGINE DEGRADATION AND CREEP LIFE CONSUMPTION Rafael Chiavegatto Yi-Guang Li...
Proceedings Papers
Proc. ASME. GT2023, Volume 8: Industrial and Cogeneration; Manufacturing Materials and Metallurgy, V008T17A019, June 26–30, 2023
Publisher: American Society of Mechanical Engineers
Paper No: GT2023-103706
...Proceedings of ASME Turbo Expo 2023 Turbomachinery Technical Conference and Exposition GT2023 June 26-30, 2023, Boston, Massachusetts, USA GT2023-103706 METHODICAL EVALUATION OF PROCESS CHAINS FOR THE MANUFACTURING OF ROTATING ENGINE COMPONENTS BLISK | IBR Martin Seimann Fraunhofer Institute...
Proceedings Papers
Proc. ASME. GT2020, Volume 1: Aircraft Engine; Fans and Blowers, V001T01A033, September 21–25, 2020
Publisher: American Society of Mechanical Engineers
Paper No: GT2020-16003
... Abstract In the development of an aero-engine combustor, the definition of a preliminary design is a practice in which know-how, product experience and design rules are focal in deriving a configuration able to meet the functional requirements. Several configurations, and hence multiple...
Proceedings Papers
Proc. ASME. GT2010, Volume 5: Industrial and Cogeneration; Microturbines and Small Turbomachinery; Oil and Gas Applications; Wind Turbine Technology, 495-506, June 14–18, 2010
Publisher: American Society of Mechanical Engineers
Paper No: GT2010-23149
... the compressor is usually treated as adiabatic. This is not the case since the heat fluxes from both the turbine and the engine must be taken into account in the compression process. Tests at Imperial College enabled the heat fluxes on a turbocharger installed on a 2.0 litre diesel engine to be quantified...
Proceedings Papers
Proc. ASME. GT2009, Volume 5: Microturbines and Small Turbomachinery; Oil and Gas Applications, 163-174, June 8–12, 2009
Publisher: American Society of Mechanical Engineers
Paper No: GT2009-59618
... the understanding of the heat transfer process taking place in a turbocharger when installed on an internal combustion engine. In order to do this, beyond the standard set of measurements needed to define the turbo operating point, a large number of thermocouples were installed on the turbocharger. The tests...
Proceedings Papers
Proc. ASME. GT2008, Volume 2: Controls, Diagnostics and Instrumentation; Cycle Innovations; Electric Power, 431-440, June 9–13, 2008
Publisher: American Society of Mechanical Engineers
Paper No: GT2008-50175
... 04 08 2009 Accurate estimation of performance status of a gas turbine engine at certain ambient and operating condition based on measured gas path parameters is very important for both engine designers and users alike. It could be a very challenging task for engine performance...
Proceedings Papers
Proc. ASME. GT2005, Volume 5: Turbo Expo 2005, 95-105, June 6–9, 2005
Publisher: American Society of Mechanical Engineers
Paper No: GT2005-68140
... 03 11 2008 Accurate simulation and understanding of gas turbine performance is very useful for gas turbine users. Such a simulation and performance analysis must start from a design point. When some of the engine component parameters for an existing engine are not available, they must...
