Browse Topic: Stirling engines

Items (81)
Fuel Consumption Saving Potential of Stirling Machine on Series Parallel Hybrid Electric Vehicle: Case of the Toyota Prius2018-01-04214/3/2018
Investigations on alternative fuels and new hybrid powertrain architectures have recently undergone significant efforts in the automotive industry, in attempt to reduce carbon emissions from passenger cars. The use of these fuels presents a potential for re-emerging the deployment of external combustion non-conventional engines in automotive applications, such as the Stirling engines, especially under the current development context of powertrain electrification. This paper investigates the potential of fuel consumption savings of a series-parallel hybrid electric vehicle (SPHEV) using a Stirling machine as fuel converter. An exergo-technological explicit analysis is conducted to identify the Stirling system configuration presenting the best compromise between high efficiency and automotive implementation constraints. The Stirling engine with combustion chamber preheater is prioritized. A SPHEV model is developed based on the Prius power-split hybrid electric architecture. Energy consumption simulations are performed on the worldwide-harmonized light vehicles test cycle (WLTC) using dynamic programing as global optimal energy management strategy. Results show improved fuel consumption performance of the Stirling machine compared to the ICE. In addition, the Stirling offers other intrinsic advantages such as low noise and vibration operation and mainly multi-fuel use capability. Consequently, the studied Stirling presents a potential for implementation on SPHEVs.
Bou Nader, WissamMansour, CharbelNemer, MarounDumand, Clement
Numerical Computational Optimization Applied To The Dynamic Behavior of an Articulated Cursor, Connecting Rod and Crank Mechanism - Case Studies for Implementing a Beta Stirling Engine2014-36-02829/30/2014
The Stirling engine is a device that has great potential for being used in applications where energy (heat) is available in the system. As an example, a Stirling motor can use the energy available in the gases from the combustion process of an automotive engine by using exhaust manifold as hot source. The Stirling motor consists of a piston that can move along a cylinder that is fulfilled by a working fluid and a displacer installed between the hot and cold chambers. Due to the large temperature difference between the chambers, it becomes feasible to use the corresponding energy to drive the Stirling engine. For design purposes, a multi-objective problem is formulated so that the maximization of thermodynamic efficiency, the minimization of energetic loss associated with the movement of the displacer set, and the minimization of energetic loss related to the fluid displacement between the two chambers is obtained for the optimal configuration of the system. To solve this optimal design problem, the Non- dominated Sorting Genetic Algorithm is used. The preliminary results demonstrated that the methodology proposed represents a promising approach for the design of Stirling engines. The theoretical results were used to construct a prototype of a Stirling engine for evaluating the whole design process.
de Paula Brito, GelcinoBorges, José Antônio Ferreira
Temperature Controlled Exhaust Heat Thermoelectric Generation2012-01-12144/16/2012
The amount of energy wasted through the exhaust of an Internal Combustion Engine (ICE) vehicle is roughly the same as the mechanical power output of the engine. The high temperature of these gases (up to 1000°C) makes them intrinsically apt for energy recovery. The gains in efficiency for the vehicle could be relevant, even if a small percentage of this waste energy could be regenerated into electric power and used to charge the battery pack of a Hybrid or Extended Range Electric Vehicle, or prevent the actuation of a conventional vehicle's alternator. This may be achieved by the use of thermodynamic cycles, such as Stirling engines or Organic Rankine Cycles (ORC). However, these systems are difficult to downsize to the power levels typical of light-vehicle exhaust systems and are usually bulky. The direct conversion of thermal energy into electricity, using Thermoelectric Generators (TEG) is very attractive in terms of minimal complexity. However, current commercial thermoelectric modules based on Seebeck effect are temperature-limited, so they are unable to be in direct contact with the exhaust gases. A way to downgrade the temperature levels without significantly reducing the regeneration potential is to interpose Heat Pipes (HP) between the exhaust gas and the Seebeck modules in a controlled way. This control of maximum permissible temperature at the modules is achieved by regulating the pressure of phase change of the service fluid of the HP. In this way the system will be failsafe against overheating and will be able to operate efficiently under both low and high thermal loads. Such is the case of the range extender unit being developed by the team, which has a low (15 kW) and a high (40 kW) power mode of operation. Various designs concepts were evaluated by simulation, design and test. Although efficiencies were still moderate, it was possible to demonstrate the potential of this system for optimizing the output of commercially available temperature-limited TEGs.
P. Brito, FranciscoMartins, JorgeGoncalves, L.M.Sousa, Rui
Hydrogen Permeation Issue for Gas Fired AMTEC Systems1999-01-25578/2/1999
Diffusion of hydrogen in solids is an intriguing intellectual problem. Permeation of hydrogen generated in combustion into gas fired Alkali Metal Thermal to Electric Converter (AMTEC) systems can be detrimental to AMTEC performance for various reasons. Potential effects include depriming of the AMTEC cell arteries, blockage of the condenser and hydride formation. Numerous papers and reports have been published concerning hydrogen diffusion in solids (Birnbaum and Wert, 1972; Garber, 1975; Strehlow and Savage, 1974). Many of these papers concern the embrittling effects of hydrogen and many concern the diffusion process itself. Hydrogen permeation and permeation resisting strategies have been examined extensively in connection with other energy conversion technologies such as Stirling engines (Alger, 1988; Khalili etal., 1989) and high temperature heat pipes (Anderson et al., 1995; North and Anderson, 1997). Due to the different boundary conditions and materials involved, it was necessary to conduct experiments specifically designed for AMTEC to evaluate hydrogen permeation rates into AMTEC cells, to understand the effect of this permeation on AMTEC performance and finally, if hydrogen permeation turns out to be a cause for concern, to identify strategies to reduce permeation, and to design an AMTEC cell which will perform with adequate lifetime. This paper describes experiments and their results for AMTEC cells operated in a partial pressure of hydrogen. Experiments in which the hydrogen permeation rate across different thickness cell walls were measured with and without barrier coatings are also described. Due to greater sensitivity, the change in pressure on the vacuum side of the specimen was observed as hydrogen permeated the metal. Depending on the operating conditions and the operating life requirements of specific AMTEC systems, hydrogen permeation barriers may need to be included in the cell design. Some of the solution approaches that were implemented and their effectiveness in minimizing AMTEC degradation are also elucidated.
Mital, R.Butkiewicz, D. A.Childs, K. F.Hayes, D. D.Svedberg, R. C.Hunt, T. K.
Free-Piston Stirling Convertor Dynamic Gas Bearings9293848/3/1992
Using a dynamic gas journal bearing in a free-piston Stirling convertor requires an analysis of the bearing which takes into account the actual working conditions of the bearing with high surrounding pressure, different boundary pressures on the bearing edges and axial movement of the “shaft”. Such an analysis has been developed and provides the steady state and dynamic characteristics of the gas bearing. Based upon this analysis a FORTRAN code has been written which, in addition, may be used to determine the influence of thermal, mechanical and manufacturing distortion. A generic bearing typical of one used in a 25 kW Stirling convertor was analyzed. The reported steady-state performance includes the load capacity, the power lost in friction and the axial flow. The dynamic analysis establishes the stability criteria of the gas lubricant film. The bearing radial clearance has a strong influence on the load capacity and axial flow past of the bearing. This influence can be used to optimize the bearing clearance with respect to the bearing efficiency and manufacturing possibilities. The pressure difference at the bearing edges and the axial movement of the shaft have negligible influence on the bearing performance. A perfect cylindrical bearing runs with whirl motion but could be accept. Any distortion, in the bearing radial clearance, can improve the bearing performance. A waved bearing concept has been shown to improve both the steady-state and the dynamic performance.
Dimofte, FlorinLiebler, Kenneth A.
Energy Source Selection for Stirling Engine Driven AUV's9294048/3/1992
Many non-renewable land-based resources are becoming depleted and the search for alternative sources of raw materials is intensifying. This situation has lead to the involvement of a number of countries, especially those of the European Community, in heavily funded ‘Wealth from the Oceans’ projects. A significant element of the research being conducted under the auspices of these projects is concerned with the development of small unmanned and untethered autonomous underwater vehicles (AUVs). To carry out their intended autonomous missions these vehicles will need reliable power systems which have high energy densities. However, although research into navigation, control and command systems has progressed considerably under this development effort, only limited headway has been made in the development of power systems which could be readily integrated into these vessels. Electrochemical power systems have been used in underwater applications for a number of years but those presently available cannot meet the rigorous specifications demanded by AUV missions. Consequently high performance fuel cells and advanced battery systems are being developed which should be generally available within the next ten years. Until then, power systems based on the utilisation of the more mature heat engine technologies appear to offer the possibility of a quicker solution to the energy density problem. Of the heat engine types available the Stirling Engine, already proven in larger submarines, shows considerable promise. One of the main reasons for the selection of the Stirling engine is it's ability to utilise any heat source, such as radioisotopes, thermal energy storage and metallic fuels. In this paper a project is described in which the design requirements for a Stirling engine driven AUV have been examined together with the identification of the most suitable primary energy source for a specific mission. As part of this project a user-friendly PC-based computer program has been developed which allows rapid assessments of the use of different energy sources with a double-acting Stirling for user defined missions. The structure and use of this code is discussed.
Potter, I. J.Reader, G. T.Walker, G.
100-kWe Lunar/Mars Surface Power Utilizing the SP-100 Reactor with Dynamic Conversion9294468/3/1992
An integration study was performed coupling an SP-100 reactor with either a Brayton or Stirling power conversion subsystem. A power level of 100 kWe was selected for the study. The power system was to be compatible with both the lunar and Mars surface environment and require no site preparation. In addition, the reactor was to have integral shielding and be completely self-contained, including its own auxiliary power for start-up. Initial reliability studies were performed to determine power conversion redundancy and engine module size. Previous studies were used to select the power conversion optimum operating conditions (ratio of hot-side temperature to cold-side temperature). Results of the study indicated that either the Brayton or Stirling power conversion subsystems could be integrated with the SP-100 reactor for either a lunar or Mars surface power application. For the lunar environment, the reactor and primary coolant loop would be contained in a guard vessel to protect from a loss of primary loop containment. For the Mars environment, all refractory components including the reactor, primary coolant, and power conversion components would be contained in a vacuum vessel for protection against the CO2 environment. The vacuum would be maintained by an active ion pumping system. These active ion vacuum systems have no moving parts and have a long history of reliable operation.
Harty, Richard B.Mason, Lee S.
Visualization of Entry Flow Separation for Oscillating Flow in Tubes9294668/3/1992
Results of visualization experiments are presented for the entry flow to circular tubes under oscillatory flow conditions. Geometries and conditions have been chosen to simulate the flow in a Stirling engine with straight heat exchanger tubes. Since oscillating flow in Stirling engines is unavoidably strongly influenced by the entry conditions, such documentation is useful when engine designs are being considered and is needed when test results are being interpreted. Two entry geometries are explored, one with unrestricted entry to a squared-edged tube and another with entry from one side. The visualization technique is by illumination of neutrally-buoyant, helium-filled soap bubbles with laser light, capturing with still photography. Each picture is an ensemble of exposures from 150 cycles. Each entry to the ensemble is taken at the same range in crank position, typically five degrees. Thus, one picture may visualize the flow from 75 to 80 degrees of crank rotation, for instance. Such documentation is done for representive points throughout the cycle. The figures show that, upon entry, there is separation of streamlines from the wall with a separation bubble length of few diameters. During the acceleration phase of the cycle, this separation zone becomes larger with increasing velocity and Reynolds number. During the deceleration phase of the cycle, the scale of the separation region is roughly constant. It does not grow as might be expected. Circuitous bubble trajectories in photos taken during later portions of the deceleration phase hint that eddy circulation is intense. Such circulation may be curtailing the separation bubble growth. When the entry flow is restricted to one side, the recirculation zone on the side from which the flow enters becomes considerably larger than when the flow entry is unrestricted. In this case, the separation bubble does grow somewhat during the period of strong decelaration.
Qiu, SonggangSimon, Terrence W.
Stirling Bottoming Cycle for the Gas Turbine Exhaust Streams of Pipeline Compressor Stations9293938/3/1992
In pipeline compressor stations natural gas fuelled aircraft derivative gas turbines are frequently used in conjunction with a power turbine to drive the large centrifugal compressors for ‘boosting’ the pipeline pressure. Typically two thirds of the energy provided to drive the turbine is carried off as heat in the exhaust stream. These hot exhaust streams, typically at temperatures around 500 K contain very substantial energies, 50 MW being not uncommon. This paper summarises recent studies carried out to assess the feasibility and worth of applying Stirling power systems to generate electric power from these ‘waste’ streams. Both ‘bottoming’ and topping cycles are of interest and are briefly considered in this paper. An elementary, but realistic, performance analysis indicates the possibility of recovering as much as 9 MW power from the exhaust of a gas compressor equipped with a Rolls-Royce RB 211 aircraft derivative gas turbine. There are approximately 6000 gas turbine/compressor units in 2750 gas pipeline compressor stations distributed throughout North America. On this basis it appears feasible that as much as 54,000 MW electric power may be generated from the existing turbine exhaust. It is anticipated the cost of the Stirling engine system would be about half the cost of the alternative Rankine cycle system.
Walker, G.Kremer, J.Fauvel, R.Reader, G.Bingham, E. R.
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