Refine
Year of publication
- 2019 (194) (remove)
Institute
- Fachbereich Medizintechnik und Technomathematik (63)
- IfB - Institut für Bioengineering (40)
- Fachbereich Luft- und Raumfahrttechnik (38)
- Fachbereich Elektrotechnik und Informationstechnik (30)
- Fachbereich Energietechnik (19)
- INB - Institut für Nano- und Biotechnologien (19)
- Fachbereich Maschinenbau und Mechatronik (16)
- Fachbereich Chemie und Biotechnologie (11)
- Fachbereich Bauingenieurwesen (8)
- MASKOR Institut für Mobile Autonome Systeme und Kognitive Robotik (8)
Has Fulltext
- no (194) (remove)
Language
- English (194) (remove)
Document Type
- Article (94)
- Conference Proceeding (75)
- Part of a Book (15)
- Book (4)
- Doctoral Thesis (3)
- Conference: Meeting Abstract (2)
- Talk (1)
Keywords
- Enterprise Architecture (2)
- Seismic design (2)
- Achilles tendon (1)
- Advanced driver assistance systems (ADAS/AD) (1)
- Aircraft design (1)
- Analytics (1)
- Architectural gear ratio (1)
- Assistive technology (1)
- Automatic control (1)
- BEV (1)
In this paper, an approach to propulsion system modelling for hybrid-electric general aviation aircraft is presented. Because the focus is on general aviation aircraft, only combinations of electric motors and reciprocating combustion engines are explored. Gas turbine hybrids will not be considered. The level of the component's models is appropriate for the conceptual design stage. They are simple and adaptable, so that a wide range of designs with morphologically different propulsive system architectures can be quickly compared. Modelling strategies for both mass and efficiency of each part of the propulsion system (engine, motor, battery and propeller) will be presented.
Flexible Fuel Operation of a Dry-Low-Nox Micromix Combustor with Variable Hydrogen Methane Mixtures
(2019)
Application of Low NOx Micro-mix Hydrogen Combustion to 2MW Class Industrial Gas Turbine Combustor
(2019)