Auswahl der wissenschaftlichen Literatur zum Thema „Hybrid Propulsion System“

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Zeitschriftenartikel zum Thema "Hybrid Propulsion System"

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Muhammad, Andi Haris, Baharuddin, and Hasnawiya Hasan. "DESAIN KONFIGURASI SISTEM PROPULSI HYBRID TERHADAP PENGURANGAN KONSUMSI BBM KAPAL PENANGKAP IKAN 30 GT (Configuration Design of a Hybrid Propulsion System to Reduce Fuel Oil Consumption of a 30 GT Fishing Vessel)." Marine Fisheries : Journal of Marine Fisheries Technology and Management 10, no. 1 (2019): 1–9. http://dx.doi.org/10.29244/jmf.10.1.1-9.

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This study aims to reduce fuel oil consumption of a 30 GT fishing vessel through configuration design of diesel and electric motor hybrids propulsion system. The configuration design of hybrids propulsion system systematically include; i) loading assumption; ii) prediction of speed-thrust; iii) prediction of fuel oil consumption. Design of hybrids propulsion system was analyzed by using the concept of time domain simulation of vessel movement. The result indicated that the hybrids propulsion system implemented to fishing vessel was very effective to reduce fuel consumption compared with conven
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ISVORANU, Dragoș Daniel, Petrișor-Valentin PÂRVU, and Octavian GRIGORE. "A HYBRID PROPULSION SYSTEM FOR UAS." SCIENTIFIC RESEARCH AND EDUCATION IN THE AIR FORCE 21, no. 1 (2019): 135–50. http://dx.doi.org/10.19062/2247-3173.2019.21.19.

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ORKISZ, Marek, Piotr WYGONIK, Michał KUŹNIAR, and Maciej KALWARA. "Comparative analysis of combustion engine and hybrid propulsion unit in aviation application in terms of emission of harmful compounds in the exhausts emitted to the atmosphere." Combustion Engines 178, no. 3 (2019): 213–17. http://dx.doi.org/10.19206/ce-2019-337.

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Comparative analysis of combustion and hybrid propulsion unit in aviation application in terms of emission of harmful compounds in the exhausts emitted to the atmosphere. For the propulsion of the AOS 71 motor glider, two types of propulsion were planned as de-velopment versions. The first analysed propulsion is based on a combustion engine, but of the Wankel type (LCR 814 engine with the power of 55 kW). The second designed propulsion is an hybrid based on a LCR 407 combustion engine with a power of 28 kW, which is connected in series with an electric generator propelling the engine (Emrax 22
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Leśniewski, Wojciech, Daniel Piątek, Konrad Marszałkowski, and Wojciech Litwin. "Small Vessel with Inboard Engine Retrofitting Concepts; Real Boat Tests, Laboratory Hybrid Drive Tests and Theoretical Studies." Energies 13, no. 10 (2020): 2586. http://dx.doi.org/10.3390/en13102586.

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The development of modern technologies and their increasing availability, as well as the falling costs of highly efficient propulsion systems and power sources, have resulted in electric or hybrid propulsions systems’ growing popularity for use on watercraft. Presented in the paper are design and lab tests of a prototype parallel hybrid propulsion system. It describes a concept of retrofitting a conventionally powered nine meter-long vessel with the system, and includes results of power and efficiency measurements, as well as calculations of the vessel’s operating range under the propulsion of
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Lents, Charles E. "Hybrid Electric Propulsion." Mechanical Engineering 142, no. 06 (2020): 54–55. http://dx.doi.org/10.1115/1.2020-jun5.

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Abstract Electrified propulsion holds the promise of reducing aviation’s CO2 emissions footprint through three means: access to green grid electric energy, improvements in aircraft performance through new airframe and propulsion system architectures and enabling further optimization of the gas turbine cycle. Charging an aircraft battery pack with green electric energy and using this energy to drive electric propulsors results in a zero emissions vehicle. This is practical for light aircraft and short missions. Boosting a Jet-A burning gas turbine with green electric energy (again stored in a g
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Ibrahim, K., S. Sampath, and D. Nalianda. "Voltage synchronisation for hybrid-electric aircraft propulsion systems." Aeronautical Journal 125, no. 1291 (2021): 1611–30. http://dx.doi.org/10.1017/aer.2021.56.

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AbstractIncreasing demand for commercial air travel is projected to have additional environmental impact through increased emissions from fuel burn. This has necessitated the improvement of aircraft propulsion technologies and proposal of new concepts to mitigate this impact. The hybrid-electric aircraft propulsion system has been identified as a potential method to achieve this improvement. However, there are many challenges to overcome. One such challenges is the combination of electrical power sources and the best strategy to manage the power available in the propulsion system. Earlier meth
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Xiao, Nengqi, Ruiping Zhou, and Xiang Xu. "Vibration of diesel-electric hybrid propulsion system with nonlinear component." Journal of Vibration and Control 24, no. 22 (2018): 5353–65. http://dx.doi.org/10.1177/1077546317753010.

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The lumped parameter method is used to model the components of a marine diesel-electric hybrid propulsion system. Modular modeling and five basic models of torsional vibration are used to establish the torsion of the diesel-electric hybrid propulsion system with a nonlinear components vibration mathematical model. In order to include the nonlinear parts of the marine diesel-hybrid propulsion shafting torsional vibration system characteristics, by combining the perturbation method with the advantages and disadvantages of the harmonic method, a perturbation-harmonic method is presented to solve
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Wieczorek, Bartosz, Łukasz Warguła, and Dominik Rybarczyk. "Impact of a Hybrid Assisted Wheelchair Propulsion System on Motion Kinematics during Climbing up a Slope." Applied Sciences 10, no. 3 (2020): 1025. http://dx.doi.org/10.3390/app10031025.

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Overcoming terrain obstacles presents a major problem for people with disabilities or with limited mobility who are dependent on wheelchairs. An engineering solution designed to facilitate the use of wheelchairs are assisted-propulsion systems. The objective of the research described in this article is to analyze the impact of the hybrid manual–electric wheelchair propulsion system on the kinematics of the anthropotechnical system when climbing hills. The tests were carried out on a wheelchair ramp with an incline of 4°, using a prototype wheelchair with a hybrid manual–electric propulsion sys
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Rizzo, Gianfranco, Shayesteh Naghinajad, Francesco Tiano, and Matteo Marino. "A Survey on Through-the-Road Hybrid Electric Vehicles." Electronics 9, no. 5 (2020): 879. http://dx.doi.org/10.3390/electronics9050879.

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Hybrid Electric Vehicles (HEVs) can be divided into three categories according to how the two propulsion systems (the thermal and the electric ones) supply the driving torque to the vehicle. When the torque is supplied only by an electric propulsion system, while the heat engine takes care of generating the electricity needed to operate the system, it is called a hybrid-series. Conversely, when both propulsion systems provide torque, the vehicle is identified with parallel hybrid wording. Among the parallel hybrids there is a particular configuration called Through-the-Road (TTR). In this conf
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Ghaderi, Ahmad, Amir A. F. Nassiraei, and Kazuo ISHII. "2P1-C18 A Novel Hybrid Propulsion System For Mobile Robots." Proceedings of JSME annual Conference on Robotics and Mechatronics (Robomec) 2008 (2008): _2P1—C18_1—_2P1—C18_3. http://dx.doi.org/10.1299/jsmermd.2008._2p1-c18_1.

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Dissertationen zum Thema "Hybrid Propulsion System"

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Ahmed, Ozomata D. "Hybrid propulsion system for CubeSat applications." Thesis, University of Surrey, 2016. http://epubs.surrey.ac.uk/812899/.

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The CubeSats platform has become a common basis for the development and flight of very small, low cost spacecraft-particularly amongst University groups. The smallest CubeSats are just 1 litre in volume-comprising a 10.
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Green, Michael W. "HAPSS, Hybrid Aircraft Propulsion System Synthesis." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/817.

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Hybrid Aircraft Propulsion System Synthesis (HAPSS) is a computer program that sizes and analyzes pure-series hybrid electric propulsion systems for aircraft. The development of this program began during a NASA SBIR contract, in conjunction with Empirical Systems Aerospace (ESAero), with the creation of a propulsion fan design tool. Since the completion of this contract in July 2010, the HAPSS program has been expanded to combine the many aspects of a hybrid propulsion system such as the propulsive fans, electric motors, generators, and controllers, and the internal combustion engines. This th
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Åkesson, Elsa, Maximilian Kempe, Oskar Nordlander, and Rosa Sandén. "Unmanned Aerial Vehicle Powered by Hybrid Propulsion System." Thesis, KTH, Skolan för kemi, bioteknologi och hälsa (CBH), 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-277115.

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I samband med den globala uppvärmningen ökar efterfrågan för rena och förnybara bränslen alltmer i dagens samhälle. Eftersom flygindustrin idag är ansvarig för samma mängd växthusgaser som all motortrafik i Sverige, skulle ett byte till en avgasfri energikälla för flygfarkoster vara ett stort framsteg. Därför har projektet genom modellering framtagit ett hybridsystem av ett batteri och en bränslecell och undersökt hur kombinationen av olika storlekar på dem presterar i en driftcykel. Då batterier har hög specifik effekt men är tunga, kompletteras de med fördel av bränsleceller, som är lättvikt
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Ren, Zhongling. "Optimization Methods for Hybrid Electric Vehicle Propulsion System." Thesis, KTH, Energiteknik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-235932.

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Design of hybrid vehicles is a hot topic because of the strict restriction on the emissions of the vehicle. The optimal design of hybrid vehicles becomes necessary to reduce the cost or emissions of the vehicle. The propulsion system of a hybrid electric vehicle is inherently more complex than that of a conventional vehicle as an electric power supply branch is added. The design involves topology design, component design and control design, where all phases are interrelated. The idea to handle all the three design phases together is called system level design. Due to its complexity, it is not
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Lundin, Johan. "Flywheel in an all-electric propulsion system." Licentiate thesis, Uppsala universitet, Elektricitetslära, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-222030.

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Energy storage is a crucial condition for both transportation purposes and for the use of electricity. Flywheels can be used as actual energy storage but also as power handling device. Their high power capacity compared to other means of storing electric energy makes them very convenient for smoothing power transients. These occur frequently in vehicles but also in the electric grid. In both these areas there is a lot to gain by reducing the power transients and irregularities. The research conducted at Uppsala university and described in this thesis is focused on an all-electric propulsion sy
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Chaudhari, Anita. "Thermodynamic analysis, modelling and control of a novel hybrid propulsion system." Thesis, Loughborough University, 2011. https://dspace.lboro.ac.uk/2134/9878.

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Stringent emission regulations imposed by governments and depleting fossil fuel reserves have promoted the development of the automotive industry towards novel technologies. Various types of hybrid power plants for transport and stationary applications have emerged. The methodology of design and development of such power plants varies according to power producing components used in the systems. The practical feasibility of such power plants is a pre-requisite to any further development. This work presents thermodynamic analysis and modelling of such a novel power plant, assesses its feasibilit
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Kumar, Sandeep. "Non-AXisymmetric Aerodynamic Design-Optimization System with Application for Distortion Tolerant Hybrid Propulsion." University of Cincinnati / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1613749886763596.

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Lin, Qing. "Small-Signal Modeling and Stability Specification of a Hybrid Propulsion System for Aircrafts." Thesis, Virginia Tech, 2021. http://hdl.handle.net/10919/103515.

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This work utilizes the small-signal impedance-based stability analysis method to develop stability assessment criteria for a single-aisle turboelectric aircraft with aft boundary-layer propulsion (STARC-ABL) system. The impedance-based stability analysis method outperforms other stability analysis methods because it does not require detailed information of individual components for system integration, therefore, a system integrator can just require the vendors to make the individual components meet the impedance specifications to ensure whole system stability. This thesis presents models of a
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Nakka, Sai Krishna Sumanth. "Co-design of Hybrid-Electric Propulsion System for Aircraft using Simultaneous Multidisciplinary Dynamic System Design Optimization." University of Cincinnati / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1602153187738909.

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Sellers, Jerry Jon. "Investigation into hybrid rockets and other cost-effective propulsion system options for small satellites." Thesis, University of Surrey, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309201.

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Bücher zum Thema "Hybrid Propulsion System"

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Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Physics & Process Modeling (PPM) and Other Propulsion R&T: Proceedings of the PPM and Other Propulsion R&T Conference held at the Cleveland Airport Marriott ... Cleveland, Ohio, May 1, 1997. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Physics & Process Modeling (PPM) and Other Propulsion R&T: Proceedings of the PPM and Other Propulsion R&T Conference held at the Cleveland Airport Marriott ... Cleveland, Ohio, May 1, 1997. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Physics & Process Modeling (PPM) and Other Propulsion R&T: Proceedings of the PPM and Other Propulsion R&T Conference held at the Cleveland Airport Marriott ... Cleveland, Ohio, May 1, 1997. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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PPM and Other Propulsion R & T Conference (1997 Cleveland, Ohio). Physics & Process Modeling (PPM) and Other Propulsion R&T: Proceedings of the PPM and Other Propulsion R&T Conference held at the Cleveland Airport Marriott ... Cleveland, Ohio, May 1, 1997. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Physics & Process Modeling (PPM) and Other Propulsion R&T: Proceedings of the PPM and Other Propulsion R&T Conference held at the Cleveland Airport Marriott ... Cleveland, Ohio, May 1, 1997. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5.

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Bose, Bimal K. Advanced propulsion power distribution system for next generation electric/hybrid vehicle: Phase I, preliminary system studies : final report. National Aeronautics and Space Administration, Lewis Research Center, 1995.

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Min-Huei, Kim, and Lewis Research Center, eds. Advanced propulsion power distribution system for next generation electric/hybrid vehicle: Phase I, preliminary system studies : final report. National Aeronautics and Space Administration, Lewis Research Center, 1995.

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Simpson, Andrew. Energy storage system considerations for grid-charged hybrid electric vehicles. U.S. Dept. of Energy, National Renewable Energy Laboratory, Office of Energy Efficiency & Renewable Energy, 2005.

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United States. National Aeronautics and Space Administration., ed. Hybrid motion planning with multiple destinations: Annual technical report : reporting period 06/10/97 through 06/10/98. National Aeronautics and Space Administration, 1998.

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Buchteile zum Thema "Hybrid Propulsion System"

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Macutkevičius, Andrius, and Raimundas Junevičius. "Parameter Analysis of the Series Hybrid Vehicle Propulsion System." In TRANSBALTICA XIV: Transportation Science and Technology. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-52652-7_13.

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Nazemian, Amin, Evangelos Boulougouris, and Myo Zin Aung. "Simulation of Hybrid Fuel Cell-Battery Propulsion System Scrutinizing Multi-scheme Energy Management for a CTV Boat." In Lecture Notes in Mobility. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-89444-2_62.

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Abstract This paper proposes a model of a hybrid fuel cell-battery propulsion system for a Crew Transfer Vessel (CTV). A multi-scheme energy management strategy is also applied to the EMS block to optimize energy flow. A fuel cell-battery hybrid system was developed by integrating PEM fuel cells with Li-ion batteries to provide electricity to the propeller propulsion system, and hotel load. Accordingly, a hybrid battery/fuel cell propulsion system with the capability of both charging the battery at both stations and bunkering the fuel tanks will be proposed. During cruising, docking, stopping,
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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. "Optimal Control and System Optimization of Ground Vehicle Hybrid Drive System." In Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5_5.

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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. "Architecture of the Ground Vehicle Hybrid Drive System." In Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5_2.

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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. "Modeling and Simulation Technology for Ground Vehicle Hybrid Propulsion System." In Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5_3.

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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. "The Nonlinear Programming Optimal Control of a Hybrid Drive System." In Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5_6.

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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. "The Modeling and Identification of Lithium-Ion Battery System." In Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5_4.

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Akgul, Burak, and Ismail Ata. "Conceptual Application of Hybrid-Electric Propulsion System Configurations on Cessna 172S." In Advances in Electric Aviation. Springer International Publishing, 2023. http://dx.doi.org/10.1007/978-3-031-32639-4_29.

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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. "Application of Hybrid Drive System Modeling and Control for Wheeled Vehicles." In Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5_7.

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Zou, Yuan, Junqiu Li, Xiaosong Hu, and Yann Chamaillard. "Application of Hybrid Drive System Modeling and Control for Tracked Vehicles." In Modeling and Control of Hybrid Propulsion System for Ground Vehicles. Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-53673-5_8.

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Konferenzberichte zum Thema "Hybrid Propulsion System"

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Kurniawan, Edi, Eddy Setyo Koenhardono, Adi Kurniawan, and Indra Ranu Kusuma. "Literature Review of Hybrid Propulsion System on Ship." In 2024 IEEE 2nd International Conference on Electrical Engineering, Computer and Information Technology (ICEECIT). IEEE, 2024. https://doi.org/10.1109/iceecit63698.2024.10859836.

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DeSmidt, Hans, and Zhisheng Ai. "Dynamics of a Variable Speed Hybrid-Electric Helicopter Propulsion System." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1252.

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In this paper, a comprehensive dynamic simulation of a parallel hybrid gas-electric single main rotor helicopter involving a motor/generator (MG) pair and a differential planetary gear transmission (PGT) arrangement forming an electronic continuously variable transmission (E-CVT) was performed. This notional hybrid electric helicopter was sized based on a retrofit of a dual engine, 10000 lb, 2500 Hp class helicopter. The total weight added by the electric components was 182 lbs which increased the propulsion system weight from 1184 to 1366 lbs. The simulation results found that at 110 kts crui
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Sawata, Tadashi, and Stephen Minshull. "Development of 1 MW Hybrid Electric Propulsion Drive System." In 2024 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC). IEEE, 2024. https://doi.org/10.1109/esars-itec60450.2024.10819918.

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Mercier, Christian, Marc Gazzino, and Marc Mugnier. "State of the Art of Helicopter Hybrid Propulsion." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11519.

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State of the art of Helicopter hybrid Propulsion perspectives is presented. As done in the car industry, it can be envisaged replacing thermal energy necessary for helicopter propulsion and sustentation by electrical energy. Improvements on electrical technologies allow proposing electrical systems with attractive power to mass ratio to complement the thermal engine providing the mechanical power necessary for the helicopter propulsion. The differences between automotive functions devoted to hybridization and these possible in the case of a helicopter are explained. The different architectures
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Sollazzo, Loredana, Sergio Pica, Gerardo Spera, Silvia Occhigrossi, Shila Shojaee, and Anna Notarantonio. "Hybrid Propulsion System for Satellite." In 31st AIAA International Communications Satellite Systems Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-5629.

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Chandler, Ashley, Brian Cantwell, and G. Hubbard. "Hybrid Propulsion for Solar System Exploration." In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6103.

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Landolfi, Olga, and Leone Martellucci. "New Propulsion System for Hybrid Vehicles." In International Pacific Conference On Automotive Engineering. SAE International, 1993. http://dx.doi.org/10.4271/931882.

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Sun, C., Y. Wang, and Z. Li. "Research on Hydrodynamic Performance of Hybrid Propulsion System." In Waterjet Propulsion 5. RINA, 2008. http://dx.doi.org/10.3940/rina.wp.2008.07.

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Volchenko, V. G., and A. N. Ser’yoznov. "Hybrid and electric propulsion system of aircrafts." In INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020). AIP Publishing, 2021. http://dx.doi.org/10.1063/5.0052622.

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Patil, Sunil, Mazen El Houte, Nils Heuermann, and Mike Slack. "Fail Safe Hybrid-Electric Propulsion System Design." In AIAA SCITECH 2023 Forum. American Institute of Aeronautics and Astronautics, 2023. http://dx.doi.org/10.2514/6.2023-1208.

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Berichte der Organisationen zum Thema "Hybrid Propulsion System"

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Richter, Tim, Lee Slezak, Chris Johnson, Henry Young, and Dan Funcannon. Advanced Hybrid Propulsion and Energy Management System for High Efficiency, Off Highway, 240 Ton Class, Diesel Electric Haul Trucks. Office of Scientific and Technical Information (OSTI), 2008. http://dx.doi.org/10.2172/1092149.

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Jiang, Yuxiang. Unsettled Technology Areas in Electric Propulsion Systems. SAE International, 2021. http://dx.doi.org/10.4271/epr2021012.

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Electric vehicle (EV) transmission technology—crucial for battery electric vehicles (BEVs) and hybrid electric vehicles (HEVs)—is developing quickly and customers want good performance at a low cost. Single-speed gearboxes are popular in electric drive systems due to their simple and cost-effective configuration. However, multispeed gearboxes are being taken to market due to their higher low-speed torque, dynamic performance, and energy efficiency. Unsettled Technology Areas in Electric Propulsion Systems reviews the economic drivers, existing techniques, and current challenges of EV transmiss
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Jivkov, Venelin, and Vatko Draganov. Controlled Friction Clutch for Hybrid Propulsion Mechanical Systems with Kinetic Energy Accumulator. "Prof. Marin Drinov" Publishing House of Bulgarian Academy of Sciences, 2020. http://dx.doi.org/10.7546/crabs.2020.07.13.

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Vargas, J. V. Modeling and Optimization of Renewable and Hybrid Fuel Cell Systems for Space Power and Propulsion. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada563592.

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Klett, James William, and Jim Conklin. Final Report: Use of Graphite Foam as a Thermal Performance Enhancement of Heavy Hybrid Propulsion Systems. Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1015677.

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6

Alwosheel, Abdulrahman, and Michael Samsu Koroma. Environmental Performance of Passenger Cars in the KSA: Comparison of Different Technologies via a Life Cycle Assessment Approach. King Abdullah Petroleum Studies and Research Center, 2024. https://doi.org/10.30573/ks--2024-dp69.

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Analyzing the environmental performance of alternative vehicle technologies in the current energy landscape of the Kingdom of Saudi Arabia (KSA) is very important given their expected role in future transportation systems. This study presents a comprehensive life cycle assessment (LCA) of sedans and sport utility vehicles (SUVs) powered by different propulsion systems to analyze their environmental performance in the KSA context. The LCA examines multiple impact categories, with a particular focus on global warming potential (GWP). The results reveal that hybrid electric vehicles (HEVs), fuel
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Heavy vehicle hybrid propulsion systems R and D program plan, FY 2000-2005. Office of Scientific and Technical Information (OSTI), 2000. http://dx.doi.org/10.2172/782848.

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Analysis of Recompression-Regeneration sCO 2 Combined Cycle Utilizing Marine Gas Turbine Exhaust Heat: Effect of Operating Parameters. SAE International, 2022. http://dx.doi.org/10.4271/2022-01-5059.

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Gas turbines are fast being explored to replace the existing steam or diesel-based power packs to propel marine transportation. Marine gas turbines have already come to power high-speed marine vessels transporting perishable goods as well as high-speed naval fleets. This article investigates the potential of gas turbine to be made hybrid with supercritical recompression-regeneration carbon dioxide (CO2) cycle drawing thermal energy from the exhaust of marine gas turbines. The recompression unit acts as the topping cycle and the regeneration unit acts as the bottoming cycle of the proposed comb
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