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Multi-point design ...
Multi-point design of parallel hybrid aero engines
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- Sielemann, M. (författare)
- Modelon, Munich, Germany
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- Coïc, C. (författare)
- Modelon, Munich, Germany
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- Zhao, Xin, 1986 (författare)
- Chalmers University of Technology , Göteborg, Sweden,Chalmers tekniska högskola,Chalmers University of Technology
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- Diamantidou, Eirini (författare)
- Mälardalens högskola,Framtidens energi
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- Kyprianidis, Konstantinos (författare)
- Mälardalens högskola,Framtidens energi
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(creator_code:org_t)
- 2020-08-17
- 2020
- Engelska.
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Ingår i: AIAA Propulsion and Energy 2020 Forum. - Västerås : Institute of Electrical and Electronics Engineers Inc.. - 9781624106026 ; , s. 1-18
- Relaterad länk:
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https://urn.kb.se/re...
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https://doi.org/10.2...
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https://research.cha...
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https://research.cha...
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https://research.cha...
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Abstract
Ämnesord
Stäng
- A parallel hybrid configuration is a feasible means to reduce fuel consumption of gas turbines propelling aircraft. It introduces an electric drive on one of the spools of the gas turbine, typically the low pressure spool. The electric drive is supplied by a battery, which can also be charged when excess power is available (for instance during conditions requiring handling bleed in conventional designs). It also requires a thermal management system to dissipate heat away from electric components. While the scientific literature describes parallel hybrid studies and anticipated benefits assuming various future entry into service dates, there is limited information on the design of the gas turbine component of such a system. For conventional gas turbines, multi-point design schemes are used. This paper describes, in a consistent fashion and based on a formalized notation, how such multi-point design schemes are applied to parallel hybrid aero engines. It interprets published approaches, fills gaps in methodology descriptions with meaningful assumptions and summarizes design intent. It also discusses cycle designs generated by different methodologies based on the same cycle model. Results show that closure equations prescribing boost power can be preferable over closure equations prescribing temperature ratios for uniqueness and engineering intuitiveness while the latter can be beneficial in a second step for design space exploration.
Ämnesord
- TEKNIK OCH TEKNOLOGIER -- Annan teknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Other Engineering and Technologies (hsv//eng)
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering (hsv//eng)
- HUMANIORA -- Konst -- Design (hsv//swe)
- HUMANITIES -- Arts -- Design (hsv//eng)
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik -- Energiteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering -- Energy Engineering (hsv//eng)
Nyckelord
- Aircraft engines
- Combustion
- Gas turbines
- Petroleum prospecting
- Propulsion
- Closure equations
- Conventional design
- Design space exploration
- Electric components
- Limited information
- Scientific literature
- Temperature ratio
- Thermal management systems
- Electric drives
Publikations- och innehållstyp
- ref (ämneskategori)
- kon (ämneskategori)
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