TY - JOUR A1 - Güsewell, Manfred A1 - Brandt, U. A1 - Himmelberg, Axel A1 - Küstner, F. A1 - Roth, Norbert T1 - Gastemperaturen in einer Zweiphasenströmung Flüssigkeit/Gas Y1 - 2001 ER - TY - JOUR A1 - Güsewell, Manfred A1 - Himmelberg, Axel A1 - Roth, Norbert A1 - Siepmann, Stefan T1 - Untersuchungen zu Quenchprozessen Y1 - 2001 ER - TY - JOUR A1 - Himmelberg, Axel A1 - Güsewell, Manfred T1 - Simulation von Zweiphasenströmungen in Gasquenchern Y1 - 2001 ER - TY - JOUR A1 - Roth, Norbert A1 - Güsewell, Manfred A1 - Himmelberg, Axel T1 - Gestaltung und Betrieb einer Technikumsquenchanlage Y1 - 2001 ER - TY - JOUR A1 - Roth, Norbert A1 - Güsewell, Manfred A1 - Himmelberg, Axel T1 - Messung von Tropfenmerkmalen in einer Quenchapparatur Y1 - 2001 ER - TY - CHAP A1 - Berg, Heinz Peter A1 - Antoshkiv, Oleksiy A1 - Himmelberg, Axel A1 - Izweik, Husni Taher A1 - Poojitganont, Thanapol T1 - Brennverfahrensentwicklung für eine neuartige Kreiskolbenmotorenfamilie, Wankelmotorenentwicklung KW - Wankelmotor KW - Verbrennung KW - Brennverfahren KW - Gemischbildung KW - Einspritzung KW - Optimierung Y1 - 2008 ER - TY - CHAP A1 - Antoshkiv, Oleksiy A1 - Berg, Heinz Peter A1 - Himmelberg, Axel T1 - Optimierung der Zündkerzenposition in einem Wankelmotor, Motorische Verbrennung KW - Wankelmotor KW - Zündung KW - Optimierung Spray KW - Gemischbildung Y1 - 2007 ER - TY - CHAP A1 - Poojitganont, Thanapol A1 - Berg, Heinz Peter A1 - Izweik, Husni Taher A1 - Himmelberg, Axel T1 - Wankel Rotary Engine for Small Aircrafts and UAVs Applications: The Simulation for Chamber Design Development KW - Wankelmotor KW - Flugantribe KW - Simulation KW - Verbrennung Y1 - 2007 ER - TY - CHAP A1 - Berg, Peter A1 - Himmelberg, Axel A1 - Malenky, Uwe A1 - Meincke, Marie A1 - Soontornpasatch, Tosaporns T1 - Hybrides Turbo Compound Fan Triebwerk T2 - Deutscher Luft- und Raumfahrtkongress 2016, Braunschweig N2 - Der Weg zum elektrischen Fliegen ist abhängig von der Entwicklung hochleistungsfähiger, kompakter und vor allem leichter Energiespeicher. Als mittelfristige, umweltschonende Überganglösung bieten sich, insbesondere für Flugtriebwerke mittlerer Leistungsklassen, Hybridsysteme aus Turbo-Compound-Kreiskolbenmotoren und Elektromaschinen für die Start- und Steigphasen an. Vorgestellt werden auf dem HSD-Konzept (HSD=Hybrid Super-Drive, vgl. [1]) beruhende luftfahrtechnische Anwendungen für unterschiedliche parallelhybride Flugantriebe. Die Basistechnologie stützt sich auf eine in der Produktion befindliche, vielstofffähige Wankeltriebwerksfamilie. Das HSD-Konzept legt hierbei ein Kammervolumen von 650ccm zu Grunde. Der Leistungsbereich (0,8 bis 1,36MW) wird mit einem innovativen elektrischen parallel-hybriden Turbo-Compound-Konzept abgedeckt. Hierbei kommt zur Aufladung der Kreiskolben-Verbrennungsmaschine eine neuartige luftgelagerte Turbomaschine mit integrierter E-Maschine zum Einsatz. Als Vortriebstechnologie trägt das Counter-Rotating-Fan (CRF)-Konzept, welches am Beispiel eines Flugzeugtechnologieträgers (Light-Jet) dargestellt wird, zur weiteren Steigerung der Wirtschaftlichkeit des Gesamtsystems bei. Der vorliegende Artikel basiert auf den in [1] beschrieben Grundlagen und stellt eine weiterführende Diskussion im Rahmen des DLRK dar. KW - Hyrides Fliegen KW - Luftfahrtantriebe Y1 - 2016 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:101:1-201610075510 PB - Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V CY - Bonn ER - TY - GEN A1 - Berg, Heinz Peter A1 - Himmelberg, Axel A1 - Lehmann, Mario A1 - Dückershoff, Roland A1 - Neumann, Mathias T1 - The Turbo-Fuel-Cell 1.0 – family concept - Compact Micro Gas Turbine (MGT) – Solid Oxide Fuel Cell (SOFC) energy converters in the 100 - 500 kW electrical power range for the future T2 - IOP conference series : Materials Science and Engineering N2 - The “Turbo-Fuel-Cell-Technology” has been described as a MGT-SOFC hybrid system consisting of a recuperated micro gas turbine (MGT) process with an embedded solid oxide fuel cell (SOFC) subsystem. SOFC stacks are connected to “SOFC stack grapes” and are equipped with the so called HEXAR-Module. This module is composed of a high-temperature heat exchanger (HEX), an afterburner (A) and a steam reformer (R). The MGT-concept is based on a generator driven directly by the turbomachine and a recuperator, which returns the exhaust heat to the pressurized compressor outlet air. This provides the necessary base for a highly effective, pure MGT process and the “MGT-SOFC-high-efficiency process”. This paper describes the concept and the thermodynamic background of a highly effective and compact design of the “Turbo-Fuel-Cell 1.0-Family” in the electrical performance class from 100 to 500kW. The technological state of the system is shown and a rating of the system with comparative parameters is discussed. It becomes visible that all necessary basic technologies should be available and that the technology (for stationary applications) can have the “entry into services (E.I.S.)” in the next 10 years. The MGT-SOFC performance map under different operation conditions is discussed. This article also provides an overview of the research on MGT-SOFC-Systems and the scenario of an energy supply network and a mobile energy conversion of the future introduction. KW - MGT-SOFC KW - Brennstoffzellen KW - Mikrogasturbinen KW - Hybrid Y1 - 2018 UR - http://iopscience.iop.org/article/10.1088/1757-899X/297/1/012004 U6 - https://doi.org/doi:10.1088/1757-899X/297/1/012004 SN - 1757-899X VL - 297 ER - TY - GEN A1 - Berg, Heinz Peter A1 - Kleissl, Marko A1 - Himmelberg, Axel A1 - Lehmann, Mario A1 - Prechavut, Nontavut A1 - Vorpahl, Michael ED - Prukvilailert, Monchai T1 - Heat balancing of direct reforming fuel cells in MGT-SOFC hybrid systems T2 - 9th Thai Society of Mechanical Engineers, International Conference on Mechanical Engineering (TSME-ICoME 2018) 11–14 December 2018, Phuket, Thailand N2 - Solid oxide fuel cells convert chemical energy in electrical energy and are highly suitable for the conversion of hydrocarbon based fuels and products from PowerToGas conversions. Embedded in a micro gas turbine-cycle instead of the combustion chamber the heat energy of the injected fuel, released in the SOFC-Stack, can additionally converted into work and by a turbine-generator into electricity. In a compact system, SOFC stacks are designed to realize a direct steam-reforming process inside. In such direct-reforming fuel cell systems the SOFC operating temperature due to the heat demand for reforming, can be reduced to a value in the range of the outlet temperature of the downstream flow (650°C). If the cycle uses a recuperating system, the operating conditions of the SOFC can be realized without additional high-temperature heat exchanger systems. The system with an uncooled turbine, described in [1], just can reach the operating temperature with an additional high-temperature heat exchange. The system described in this publication does not require an additional high-temperature heat exchanger, because the X-value, as the ratio between the exchanged heat quantity and the required amount of heat to complete the MGT-cycle [2] due to the referring process, is nearly zero and can be realized via the inner container wall (of the MLC). The cycle is completed (between the SOFC and the turbine entry) by the heat input of an afterburner. Here the unreacted fuel of the SOFC fuel-stream is used to provide the necessary heat energy for the downstream turbo-generator-system. KW - MGT-SOFC KW - Heat balancing KW - simulation KW - thermodynamic cycle KW - effectivity Y1 - 2018 UR - https://iopscience.iop.org/article/10.1088/1757-899X/501/1/012007/meta U6 - https://doi.org/10.1088/1757-899X/501/1/012007 SN - 1757-899X SP - 50 EP - 60 PB - IOP Publishing/IOP Science CY - Bristol ET - 1. Auflage ER - TY - GEN A1 - Berg, Heinz Peter A1 - Himmelberg, Axel A1 - Poojitganont, Thanapol T1 - Hybrid Turbo Compound Fan Engine an Eco-Efficient Propulsion System for Aviation T2 - Materials Science and Engineering : Thai Society of Mechanical Engineering, the 10th International Conference on Mechanical Engineering (TSME-ICOME2019) 10-13 December 2019, Pattaya, Thailand N2 - The path to electric propulsion systems depends on the development of powerful, compact and very light energy storage system with a high storage density. In order to create an environment-friendly intermediate solution in the medium term, especially for aircraft engines of medium power classes, it makes sense to use an innovative, electrically parallel hybrid unit based on rotary engines and electric boosters for start and climb phases as a propulsion system. An aero-engine application, based on the HSD concept (HSD = hybrid super-drive – hybrid Wankel rotary engine) for different hybrid-parallel propulsion systems is presented. In this article, the introduced technology is based on a currently produced family of multi-component Wankel rotary engines. The proposed HSD concept uses a chamber volume of 650ccm per rotor. The projected power range (0.8 to 1.36 MW) is covered by an innovative hybrid electric parallel turbo compound concept together with 2x4 rotary engine units. A novel, airbearing turbo engine with integrated electric drive is used as a turbocharger for charging the rotary engine. For the aero-engine technology, the counter-rotating fan (CRF) concept shown as an example for an aircraft technolo¬gy carrier (light jet) leads to a further increase in the efficiency of a complete system. KW - rotary engine, hybrid combustion engine, aero-engine, air bearing, counter rotating fan, electric flight Y1 - 2020 UR - https://iopscience.iop.org/article/10.1088/1757-899X/886/1/012010 U6 - https://doi.org/10.1088/1757-899X/886/1/012010 SN - 1757-899X VL - 2020 PB - IOP Science CY - Bristol ET - 1. Auflage ER - TY - GEN A1 - Dückershoff, Roland A1 - Berg, Heinz Peter A1 - Himmelberg, Axel A1 - Lehmann, Mario A1 - Kleissl, Marko ED - Ashton, Anete T1 - Influence on the Electrical Efficiency of a Hybrid MGT-SOFC-System by μ-fogging in a-Two-Staged Compressor System T2 - IOP Conference Series: Materials Science and Engineering N2 - Hybrid combinations of solid oxide fuel cell and recuperated micro gas turbines can convert the chemical energy of hydrocarbon-based fuels in electrical energy with high electrical efficiency. With an integrated and improved cycle management, more than 70% of the energy content of the fuel could be converted. Therefore, the systems are highly suitable for the Power-To-Gas conversion. In particular, a pressure charging of the SOFC fuel cell leads to an increase in stack performance. By a downstream turbo set, after residual fuels are intentionally oxidized with an afterburner, additional electrical energy can be gained from the expansion of the hot exhaust gas stream and the overall efficiency can be increased. In order to increase the electrical efficiency of the system, it is proposed, to ensure the required compression of the process air in particular by a-two-staged turbo compressor with an intermediate cooling system. By thus achievable reduction of the dissipation of the compressor and by targeted condensation of finest drops in front of the second compressor stage affected by intermediate cooling, an increase in efficiency of the system is possible. This is achieved by targeted cooling of the process air behind a low pressure compression, so that it is saturated over 100% relative air humidity. As a result, a slightly supersaturated airflow is available for the second compressor stage, which enters the compressor after heat removal via an intermediate cooling having a small number of microdroplets. Therefore, the condensed water evaporates again by the heat of compression in the second stage and the compressed flow ultimately enters the recuperation at a lower temperature than during normal compression. Thus, more heat can be recovered within the recuperation system. Therefore, the electrical energy of the system can be produced having higher efficiency, because the heat dissipation of the overall system decreases. In this article it is presented, how such a process is thermodynamically modelled and how a technical realization can be built after optimization by simulations. Finally, in this study, the process-influencing factors are analyzed to show the highest possible electrical yield of such a system. KW - Micro Gasturbine, Hybrid, SOFC Fuel Cell, Fogging, Efficiency Y1 - 2020 UR - https://iopscience.iop.org/article/10.1088/1757-899X/886/1/012041 U6 - https://doi.org/10.1088/1757-899X/886/1/012041 SN - 1757-899X SP - 1 EP - 8 PB - IOP Science CY - Bristol ET - 1. Auflage ER - TY - GEN A1 - Berg, Heinz Peter A1 - Dückershoff, Roland A1 - Hertrampf, Stefan A1 - Kloshek, Alexander A1 - Himmelberg, Axel T1 - Development of an injector spark plug for the injection and ignition of gaseous fuels in internal combustion engines for use in conventional systems T2 - AIP Conference Proceedings N2 - An injection-ignition-system from an additive manufacturing process is presented with which gaseous fuels can be injected into the combustion chamber of an internal combustion engine under pressures of up to 80 bar and ignited. With the presented system, an improvement of the thermal efficiency can be achieved by a late fuel injection in the compression phase and with post-injection. With such a system, the engine becomes purely air-intake and a better filling level is achieved. Injection and ignition can take place simultaneously with this application. The system is designed with a high pressure stability for all components (200 bar) and can therefore also be used with higher compressions and combustion pressures. The spatial distribution of the fuel in the combustion chamber is achieved by angled fluid ports and also allows additional injections and ignitions in the power stroke and in the relief phase. This can improve thermal efficiency. A built-in annular channel also enables two different fuels to be injected as a mixing chamber. Finally, initial measurement results are shown for the use of hydrogen fuel in a single-cylinder engine. Indexing data and performance data of the engine indicate that the system can represent a significant increase in the efficiency of combustion engines with hydrogen fuel. Furthermore, the system can be used in conventional vehicle systems, whereby only fuel conditioning and control systems need to be adapted. KW - Combustion engine KW - Injection KW - Ilnition KW - Hydrogen Y1 - 2024 U6 - https://doi.org/10.1063/5.0238165 VL - 3626 (2024) SP - 1 EP - 8 PB - AIP Publishing CY - Chiang Mai ER - TY - GEN A1 - Dückershoff, Roland A1 - Berg, Peter A1 - Kleissl, Marko A1 - Himmelberg, Axel T1 - TURBO fuel cell as a bridging technology for decentralised power generation using hythane T2 - AIP Conference Proceedings N2 - The TURBO fuel cell is a hybrid combination of a micro-gas turbine (MGT) and solid oxide fuel cells (SOFC). With its high electrical efficiency and low line losses, it will contribute to an environmentally friendly, reliable and affordable energy supply in residential areas. Thanks to its high efficiency, it enables greater independence from fossil fuels. Furthermore, by choosing a fuel cell type that is embedded in a turbomachinery process, hybrid technology maximises fuel flexibility and ultimately enables the transition from the existing fossil natural gas economy to a hydrogen economy. Power-to-X" products from renewable energies can be converted into electrical energy with maximum efficiency. In this way, it contributes to stopping CO2 emissions by 2050. The turbo fuel cell supplies energy in a decentralised manner and therefore exactly where it is needed. The waste heat generated by the principle can be used for building air conditioning (heating or cooling). Thanks to the condensing technology, an overall efficiency of over 96% can be demonstrated. It also contributes to grid stability thanks to its high flexibility and cluster capability. When natural gas or green methane is used as a fuel gas in a TURBO fuel cell, a synthesis gas is produced from a CH4 partial flow via an integrated pre-reformer according to the principle of vapour reforming. This synthesis gas is fed to the high-temperature fuel cell for conversion into electricity. If a high proportion of hydrogen is added to this fuel gas, it is referred to as hythane. It is shown that when hythane is used in the turbo fuel cell up to a hydrogen content of 50 %, the very high efficiency of electricity generation by the TURBO fuel cell is maintained. The introduction of this technology can drive forward the decarbonisation of the energy industry. This demonstrates how important this technology is for the introduction of a hydrogen economy utilising existing infrastructures. Y1 - 2024 U6 - https://doi.org/10.1063/5.0237467 SN - 1551-7616 SN - 0094-243X VL - 3236 (2024) IS - 1 SP - 080009-1 EP - 080009-8 PB - AIP Publishing ET - 1 ER - TY - GEN A1 - Dückershoff, Roland A1 - Berg, Heinz Peter A1 - Kleissl, Marko A1 - Walther, Aniko A1 - Himmelberg, Axel T1 - Flexibilization of an MGT-SOFC hybrid system for electricity and hydrogen production for the realization of a sustainable hydrogen economy T2 - AIP Conference Proceedings N2 - The turbo fuel cell is a hybrid combination of a micro-gas turbine (MGT) and solid oxide fuel cells (SOFC). It will contribute to an environmentally friendly, reliable and affordable energy supply due to its high electrical efficiency and low line losses in close proximity to residential districts. The turbo fuel cell (MGT-SOFC hybrid system) makes it possible to increase independence from fossil fuels by choosing a fuel cell type with maximum fuel flexibility embedded in a turbo machine process. This hybrid technology makes it possible to transform the existing fossil gas economy into a hydrogen economy. This technology converts products from "power-to-X-gas" conversions from renewable energies into electrical energy with the highest conversion efficiency and thus contributes to the goal of stopping CO2 emissions by 2050. The turbo fuel cell supplies energy exactly where it is needed. The principle-related waste heat can be used for building air conditioning (heating or cooling) systems. Thanks to the condensing technology, an overall efficiency of over 96% can thus be demonstrated. Additionally, it contributes to grid stability through high flexibility and cluster capability. For methane to be converted into electricity in a turbo fuel cell, a synthesis gas is generated from a CH4 partial flow via an integrated pre-reformer according to the principle of steam reforming. Through high-temperature separation after the pre- reformer, hydrogen can be extracted from the synthesis gas and discharged for use in other applications (e.g., hydrogen mobility). Hydrogen extraction does not lead to a deterioration of electrical efficiency, which is about 70% in the system under consideration. In the living spaces of tomorrow, hydrogen and electrical energy for mobility can thus be provided even before the realisation of a supra-regional hydrogen supply economy. Decarbonisation of the energy economy can be advanced through the introduction of this technology. In this publication, it is shown how important this technology is for the introduction of a hydrogen economy with the inclusion of existing infrastructure. Y1 - 2024 U6 - https://doi.org/10.1063/5.0205000 VL - 3086 (2024) IS - 1 ER - TY - GEN A1 - Berg, Heinz Peter A1 - Himmelberg, Axel A1 - Dückershoff, Roland A1 - Kleissl, Marko A1 - Ring, Uwe T1 - Simulations using dimensionless key figures for the design and optimization of compact, hybrid MGT-SOFC systems of the “Turbo Fuel Cell” type for high efficiency T2 - 14th European Conference on Turbomachinery Fluid dynamics & Thermodynamics : ECT14, April 12-16 2021; Gdansk, Poland N2 - The "Turbo Fuel Cell" represents a highly integrated and highly compact technology system of a micro gas turbine fuel cell cycle (MGT-SOFC). It provides the solution for a highly efficient reverse electricity generation with an electrical efficiency of at least 68% (status 2020-21) to approx. 75-80% (in the future). In the context of industrial research on such a hybrid process, adapted, dimensionless parameters should be used in the design and optimization of the overall system. As an example, simulations of thermally optimized solutions to improve the energy yield using various dimensionless key figures are presented. Above all, heat integration measures enable an increase in system efficiency and a reduction in primary energy input. On the basis of exergetic analyzes by use of a modified Heat Balance Factor Y, as presented at ETC12, and the consideration of the SOFC enthalpy spread j, as well as a highly integrative use of the High Temperature Heat Exchanger Function F, it is shown how the hybrid cycle process efficiency can be optimized through innovative coupling of the individual heat flows. Measures to change the hybrid process can be used to deliberately shift the useful energy from the predominant heat yield in order to optimize electrical efficiency. A developed system enables primary energy to be used with the highest possible efficiency. The primary fuel used here is gaseous primary energy in the form of methane (natural gas) and hydrogen from renewable sources. Treatment mechanisms, such as the reforming of the methane used, and the targeted use of modern heat insulation and recovery mechanisms also have been considered. For the optimized hybrid system, total electrical efficiencies of more than 68% could be demonstrated and additional thermal energy for heating purposes could be extracted. Ultimately, overall efficiencies for the utilization of the energy content of the primary energy of up to 97% can be achieved. Energy converters with a maximum system output of around 200-300kW were examined. In the near future, such plants can replace existing fossil power plants being part of decentralized network systems. By their flexibility, they can guarantee the necessary security of power supply. Y1 - 2021 U6 - https://doi.org/10.29008/ETC2021-644 ER - TY - GEN A1 - Berg, Heinz Peter A1 - Dückershoff, Roland A1 - Vorpahl, M. A1 - Himmelberg, Axel T1 - Results of the measurement of SOFC fuel cell stacks under pressure conditions T2 - IOP Conference Series: Materials Science and Engineering N2 - Results from the measurement of SOFC fuel cell stacks under pressure conditions are presented. As part of a measurement campaign, the operation of a stack system is investigated, particularly under the operating conditions of a recuperated micro gas turbine. Above all, the performance and effectiveness of selected stack types at various operating pressures and operating temperatures are measured. With the test facility set up for such investigations, cell systems could be examined under atmospheric conditions and with pressures of up to 5 bar. It is shown that in operating conditions under pressure, the output of the fuel cell systems are improving. From a gauge pressure of 4 bar, the performance curve is flattened and higher pressures only produced a marginal increase in performance. Furthermore, the cells tested at overpressure show a steady-state behavior more quickly under load change requirements than in atmospheric operation. This means that more flexible operating modes with faster response behavior can be realized. By choosing a suitable operating temperature, the efficiency of the system is further increasing. Care was taken to select the operating conditions of the cell systems so that coking can be prevented. Finally, a statement can be made about the pressure dependence of the fuel conversion rate. Parasitic reactions at the anode can be related to the power output. The tests carried out have shown that the high-temperature fuel cell is a promising service provider of the future. A combination of SOFC high-temperature fuel cells and micro gas turbines in one machine could, in addition to the internal provision of the required pressure, also lead to better dynamics of the entire system and increase the energy yield from the primary energy source. Y1 - 2021 U6 - https://doi.org/10.1088/1757-899X/1137/1/012009 VL - 1137 SP - 1 EP - 11 ER -