Multidisciplinary design optimization of aero engines: environmental performance-based methodology

• Autorzy: Celis C , Mohseni M , Kyprianidis K , Sethi V , Ogaji S , Haslam A , Pilidis P , Sethi Vi
• Konferencja: International Symposium SYMKOM Compressor & Turbine Flow Systems, Treory & Application Areas (15-17.09.2008; Łódź; Polska)
• Języki publikacji: EN

Abstrakty

EN

A methodology and tool that allows evaluating and quantifying aero engines design trade-offs originated as a consequence of addressing conflicting objectives such as low environmental impact and low operating costs is presented, and applied to a general case study to assess the feasibility of using new highly efficient engine configurations: intercooled-recuperated (ICR) engines. The case study results show that according to the ICR systems performance (heat exchangers effectiveness, pressure losses, and weight penalty) they could find usage in practical applications.

Słowa kluczowe

EN

aero-engines; aircraft environmental impact; MDO

PL

silnik pneumatyczny; ocena ilościowa; metodologia

• Wydawca: Wydawnictwo Politechniki Łódzkiej
• Czasopismo: Zeszyty Naukowe. Cieplne Maszyny Przepływowe - Turbomachinery / Politechnika Łódzka
• Rocznik: 2008
• Tom: nr 133
• Strony: 87--94
• Opis fizyczny: Bibliogr. 14 poz.

Twórcy

autor

Celis C

• Department of Power and Propulsion, School of Engineering, Cranfield University, Cranfield, Bedfordshire, MK43 0AL, United Kingdom

autor

Mohseni M

autor

Kyprianidis K

autor

Sethi V

autor

Ogaji S

autor

Haslam A

autor

Pilidis P

autor

Sethi Vi

Bibliografia

• [1] Boggia, S., and Rüd, K., 2005, Intercooled Recuperated Gas Turbine Engine Concept, AIAA 2005-4192, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson, Arizona, US.
• [2] Colmenares, F., Pascovici, D., Ogaji, S., and Pilidis, P., 2007, A Preliminary Parametric Study for Geared, Intercooled and/or Recuperated Turbofan for Short Range Civil Aircrafts, GT2007-27234, Proceedings of GT2007 ASME Turbo Expo, Montreal, Canada.
• [3] European Union, 2003, Europe at a Crossroads: The Need for Sustainable Transport, European Commission, Brussels, Belgium.
• [4] Fanourakis, E., 2006, Inter-cooled Recuperated Aero-Engine: Feasibility Investigation, M.Sc. Thesis, School of Engineering, Cranfield University, UK.
• [5] iSIGHT, Version 10.0, Engineous Software, Inc., < www.engineous.com>.
• [6] Javed, A., 2007, Silent Aircraft Initiative, Design of an Intercooled Recuperated Aero Engine - Study of the Effects on Noise Levels & Integration, M.Sc. Thesis, School of Engineering, Cranfield University, UK.
• [7] Kyprianidis, K., Colmenares, F., Pascovici, D., Ogaji, S., Pilidis, P., and Kalfas, A., 2008, EVA – A Tool for Environmental Assessment of Novel Propulsion Cycles, GT2007-50602, Proceedings of GT2008 ASME Turbo Expo, Berlin, Germany.
• [8] Laskaridis, P., Pilidis, P., and Kotsiopoulos, P., 2005, An Integrated Engine-Aircraft Performance Platform for Assessing New Technologies in Aeronautics, ISABE-2005-1165, Munich, Germany.
• [9] Le Dilosquer, M., 1998, Influence of subsonic aero engine design and flight routes on atmospheric pollution, Ph.D. Thesis, School of Mechanical Engineering, Cranfield University, UK.
• [10] Ogaji, S.O.T., Pilidis, P., and Hales, R., 2007, TERA - A Tool for Aero-engine Modelling and Management, Second World Congress on Engineering Asset Management and the Fourth International Conference on Condition Monitoring, Harrogate, UK, 2007.
• [11] Pascovici, D.S., Colmenares, F., Ogaji, S.O.T., and Pilidis, P., 2007, An Economic and Risk Analysis Model for Aircrafts and Engines, GT2007-27236, Proceedings of GT2007 ASME Turbo Expo, Montreal, Canada.
• [12] Riddlebaugh, and Stephen, M., (edit.), 2007, Research & Technology 2006, NASA/TM – 2007-214479, NASA Glenn Research Center, Ohio, US.
• [13] Svensson, F., 2004, Potential of Reducing the Environmental Impact of Civil Subsonic Aviation by Using Liquid Hydrogen, PhD Thesis, School of Engineering, Cranfield University, UK.
• [14] Whellens, M. W., 2003, Multidisciplinary optimisation of aero-engines using genetic algorithms and preliminary design tools, Ph.D. Thesis, School of Engineering, Cranfield University, UK.