Browse Topic: External combustion engines

Items (193)
Measuring the dynamic parameters of liquid fragments generated in the near-field of atomizing sprays poses a significant challenge due to the random nature of the fragments, the instability of the spray, and the limitations of current measuring technology. Precise determination of these parameters can aid in improving the control of the atomization process, which is necessary for providing suitable spray structures with appropriate flow rates and droplet size distributions for various applications such as those used in heat engines. In piston and gas turbine engines, controlling spray characteristics such as penetration, cone angle, particle size, and droplet size distribution is crucial to improve combustion efficiency and decrease exhaust emissions. This can be accomplished by adjusting the structural and/or operating parameters of the fuel supply system. This article aims to measure the breakup length, spray cone angle, axial velocity, breakup time, and liquid sheet film thickness for a swirl air-blast atomizer used in a gas-steam engine. The measurement was conducted using a shadowgraph imaging system developed specifically for this study, consisting of a high-speed camera, a lens, and a light source. While lasers are commonly used as light sources in the literature, this study utilized a special LED high-speed pulse light generator, which is cheaper, easier to handle, and provides a more uniform background. Images were processed using a MATLAB code developed for this study. Although the breakup zone is naturally random and the breakup location significantly varies with time, the novel method developed in this study helps quantify critical parameters under different operating conditions.
Phung, Duoc V.Pham, Thin V.X. Pham, Phuong
Thermoacoustic heat engines (TAHEs) are external combustion engines primarily designed to convert thermal power into acoustic power and, eventually, into mechanical, electric or other forms of high grade power. TAHEs rely on the presence of a porous core, often referred to as “stack”. A temperature gradient is established along the porous core and quasi-adiabatic heat exchanges occur between the solid walls of the pores and the surrounding gaseous medium undergoing pressure fluctuations. The internal geometry of the stack has tremendous impact on the efficiency of thermal-to-acoustic power conversion. In this study, the selective laser melting (SLM) has been used to produce stacks. The SLM is an additive manufacturing (AM) technique designed for 3D metal printing. It is based on high power- density laser which melts and fuses metallic powders together. Three sets of stacks, provided with different hydraulic radii and internal geometries, have been produced. Each set is constituted by two stacks with similar hydraulic radii, one with internal parallel plates and one with internal oblique pin array. The SLM provides precise control of the features of the printed object, allowing to explore geometries which are difficult to manufacture with conventional technologies but, possibly, more effective in the heat exchange process. This is the case of pin (and oblique pin) array geometries, which provide a reduced amount of viscous losses when the working fluid has Prandtl number Pr < 1, e.g. air. The printed stacks have been tested in a small scale standing-wave TAHE set up in Tallinn University of Technology (TalTech). Temperatures are monitored in proximity of the hot and cold heat exchangers, as well as the sound pressure within the engine resonator. The measured quantities are shown in time and frequency domain to analyze the onset and the stability of the thermoacoustic phenomenon.
Auriemma, FabioHolovenko, Yaroslav
Quantification of Windage and Vibrational Losses in Flexure Springs of a One kW Two-Stroke Free Piston Linear Engine Alternator2019-01-08164/2/2019
Methods to quantify the energy losses within linear motion devices that included flexural springs as the main suspension component were investigated. The methods were applied to a two-stroke free-piston linear engine alternator (LEA) as a case study that incorporated flexure springs to add stiffness to the mass-spring system. Use of flexure springs is an enabling mechanism for improving the efficiency and lifespan in linear applications e.g. linear engines and generators, cryocoolers, and linear Stirling engines. The energy loss due to vibrations and windage effects of flexure springs in a free piston LEA was investigated to quantify possible energy losses. A transient finite element solver was used to determine the effects of higher modes of vibration frequencies of the flexure arms at an operational frequency of 65 Hz. Also, a computational fluid dynamics (CFD) solver was used to determine the effects of drag force on the moving surfaces of flexures at high frequencies. A parametric study was performed to understand the effects of geometrical and operational parameters including the diameter of flexures, gap width between flexure arms, stroke length, and frequency of oscillation on the drag force coefficient on the flexure surfaces. The numerical results were compared to experimental results obtained from damping tests and steady-state tests in a vacuum chamber. Modeled results were in good agreement with experiments and showed between 30 to 40 Watts of mechanical energy loss at 65 Hz in the 1 kW LEA design including windage and vibrational losses. It was also found that windage losses contributed to between 10-15% of the total mechanical losses. Also, damping tests in a vacuum chamber showed that in the absence of windage and acoustic losses between 30-35% of total input energy was lost due to structural and frictional damping. Measuring the amplitude of damped vibrations the damping ratio was calculated to be ζ=0.003.
Zamani Meymian, NimaClark, NigelSubramanian, JayaramHeiskell, GregoryJohnson, DerekMahmudzadeh, FereshtehDarzi, MahdiMusho, TerenceFamouri, Parviz
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
The approaching the ideal efficiency assumption is possible in Stirling engine. Regenerator is the main component in improving the efficiency of the engine. Besides the Geometry and materials of the regenerator, amount and quality of porosity have significant impacts on the regenerator performance which is focused on this research. The main idea of this study is to evaluate the effect of porosity, or unsymmetrical porosity gradient in pressure drop and the thermodynamic performance of regenerator, so three models of regenerator are developed and analyzed: First, a model in which the porosity is constant and do not change (Common mode). In the Second model, the length of regenerator porosity is changed from high to low and in the third model, the length of regenerator porosity is changed from low to high. All versions of models have the same global porosity. Each of these models is separately simulated in Ansys software and validated with experimental results from a laboratory sample. The results show that in the second model with a small increase in pressure drop during recovery, the amount of energy recovery increase dramatically compared to the conventional model.
Arab, MajidMajidi, Majid
Higher fuel economy of the vehicle is a critical concern in automobile industry. Traditional internal combustion (IC) engines waste a large portion of the available fuel energy as heat loss via exhaust gas. This proposal aims at recovering the available exhaust heat of the IC engines using stirling engine (SE) as an add-on device. SE is a type of cyclic heat engine which operates by compression and expansion of the working fluid, at different temperature levels resulting in a conversion of the heat energy into mechanical work. A thermodynamic analysis is performed on the chosen beta SE rhombic drive configuration with different combinations of design parameters like working fluid mass, total dead volume, thermal resistance, and hot side and cold side temperatures. A regenerator temperature model is developed to account for first law consistency in the regenerator section of SE, along with heat transfer in accordance with mass flow within the regenerator. In conclusion, the results indicate that a device based upon the typical tube fin type compact heat exchanger and Hydrogen as working fluid will have a working fluid volume of about 7.8 liters with 1016 W power at 12.65% thermal efficiency. For similar power output (1028 W), a smaller heat exchanger like the printed circuit heat exchanger (PCHE) requires 3.25 liters of working fluid volume at 10.85% thermal efficiency.
Saxena, ShubhamAhmed, Mudassir
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
The world today is majorly dependent upon fossil fuels for power generation, of which diesel forms an integral part. Diesel engines, having the highest thermal efficiency of any regular internal or external combustion engine, are widely used in almost all walks of life and cannot be dispensed with in the near future. However, the limited availability of diesel and the adverse effects of diesel engine emissions like nitrogen oxide (NOx) and soot particles raise serious concerns. Hence, their performance and emission improvement continues to be an avenue of great research activity. In this research work, the effects of blending Diethyl Ether with diesel in various proportions (5%, 10%, 15% and 20% by volume) were evaluated on engine performance and emissions of an industrial internal combustion engine. Several properties of DEE such as its low viscosity, high volatility, high cetane number, low auto ignition temperature and high solubility in diesel make it favorable for use in compression ignition engines. The data obtained from experimentation were carefully studied and a detailed theoretical analysis was carried out for each of the blends by comparing with baseline diesel performance data. The results were promising. The DEE blends showed a simultaneous decrease in carbon monoxide, unburned hydrocarbon, smoke emissions and brake thermal efficiency whereas the brake specific fuel consumption and the NOx emissions showed an increase. It was concluded that the 5% DEE-Diesel blend is the most effective combination from the performance and emission point of view.
Ahlawat, VaibhavGupta, MayankAnand, ShaswatBansal, VismitJain, VibhorKumar, Naveen
Gustave de Ponton d'Amécourt, Gaspard Félix Tounachon and Guillaume Joseph Gabriel de La Landelle, dubbed the "Triumvirat Hélicoptèroidal" by French physicist Jacques Babinet, played indirect and subtle roles in the early history of the development of rotary-wing flight in the latter 19th century in Paris. Tournachon, adopting the professional name of 'Nadar', innovated aerial photography (from a balloon), forever changing the way people viewed the earth and significantly contributing to an enthusiasm for aviation, a term thought to have been coined by fantasy artist Gabriel de la Landelle. Landelle's appealing representations of just-possible future helicopter-ships caught the public fancy, also contributing to an awareness of such potential flight. Vicomte Gustave de Ponton d'Amécourt had begun working on a steam-powered coaxial rotary-wing design in 1853 - in the process, coining the word 'helicopter', and by 1863 a steam powered aluminum model had been produced by mechanic L. Joseph of Arras. Although the model aircraft failed, it represented the first use of aluminum in engine construction and was a milestone attempt to solve the weight/power issues necessary for manned flight that had been set forth by Sir George Caley, the "father of aerodynamics", in his 1809-10 series of papers under the collective title "On Aerial Navigation." These three, under the direction and promotion of Nadar, formed the 'Société d'Autolocomotion Aérienne' in 1862, the name of which was changed two years later to Société d'Aviation – the first organization to employ this term. These efforts resulting in a greatly increased public enthusiasm and awareness among the common people and notables of the time, and came to involve and inspire Jules Verne, who became the organization's secretary and promoter. Verne, in 1886, wrote Robur-le-Conquérant (Robur the Conqueror), known in English as The Clipper of the Clouds, the first helicopter novel, which would be read a young Russian boy and, much later, cited as a seminal inspiration – his name was Igor Sikorsky
Charnov, Bruce
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
A unique engine, based on the regenerative principle, is being developed with the goal of achieving high brake efficiency over a wide power range. It can be characterized as an internal combustion Stirling engine (ICSE). The engine is a split-cycle configuration with a regenerator between the intake/compression cylinder and the power/exhaust cylinder. The regenerator acts as a counter-flow heat exchanger. During exhaust, the hot gases are cooled by the regenerator. The regenerator stores this heat. On the next cycle, compressed gases flow in the opposite direction and are heated by the regenerator. The gases coming from the regenerator into the power cylinder are very hot (~900°C), which provides the necessary gas temperature for auto-ignition of diesel and other fuels. A simplified Air Cycle analysis of the ICS engine is presented to validate the concept thermodynamics and to show the inherent difference between the ICS and conventional internal combustion engine (ICE) indicated efficiency. The ICE engine indicated efficiency increases with increasing compression ratio and is insensitive to peak temperatures, whereas in the ICS engine indicated efficiency increases with decreasing compression ratio and increasing peak temperature. This engine concept is a candidate for application of adiabatic engine technology which has been explored for many years. With materials that can withstand high temperatures, brake efficiencies of 60-70% are possible. Low heat transfer is important to the proper operation of the engine. A multi-step cycle computer indicated thermodynamic and fluid flow model of the ICS engine of increasing detail was used during the engine development. Finally, detailed perturbation studies were conducted to fully understand the ICS design sensitivities. An engine friction model was added to the computer model to be able to compare estimates of ICSE BSFC and BMEP with ICE engines. Important ICS engine innovations include elimination of throttling losses, low friction due to low compression ratio, and very high air cycle efficiencies (~80%) combined with low compression ratio. The engine is designed for the highest possible efficiencies. In addition to these advantages, the engine has nearly constant pressure combustion, which should help reduce NOx formation. The major findings were: the ICS engine is more efficient than either gasoline or diesel engines over the entire operating range especially at part power. At wide open throttle, an ICS engine is more efficient than either a gasoline or a diesel engine. This advantage increases at part power. On the negative side, the ICS engine has inherent low power density (volumetric efficiency) because of low compression ratio, late air intake and late combustion. A prototype engine and a modest engine test dynamometer and instrumentation are nearing completion to demonstrate the P&B Enterprises, Inc. (PBEI), ICSE concept. The prototype is a retrofitted two-cylinder diesel engine. The prototype uses the existing engine block, and the crankshaft and camshaft fit into existing spaces in the block. Anticipated problems to be addressed with the prototype engine are starting, combustion characteristics, regenerator temperature control and high turbocharging ratios to achieve reasonable power density.
Patton, RichardBennett, George
As the buzz about space grows, and with the potential for government resurrection of funding, materials for space travel-and materials creation in space-are taking on new life. New materials for space applications can be exceptionally expensive to develop, and expensive has not been a positive concept in the space community for many years. Never mind the technology spin-offs from space exploration; give no consideration to the advances in metals, composites, electronics, you name it-all of which have moved ahead since the 1950s thanks to rocket and space research. The national dismay and envy around Sputnik translated into government dollars. Not surprisingly, project numbers rose when funding was the most free and the romance of space travel caught the fancy of the public. Today, time has dimmed the romance, national pride has taken a back seat to international projects, and there have been high-profile reminders that life in space is precarious. The result: relatively low research funding.
Gayman, David
The device illustrated in Figure 1 is designed primarily for use as a regenerative heat exchanger in a miniature Stirling engine or Stirling-cycle heat pump. A regenerative heat exchanger (sometimes called, simply, a “regenerator” in the Stirling-engine art) is basically a thermal capacitor: Its role in the Stirling cycle is to alternately accept heat from, then deliver heat to, an oscillating flow of a working fluid between compression and expansion volumes, without introducing an excessive pressure drop. These volumes are at different temperatures, and conduction of heat between these volumes is undesirable because it reduces the energy-conversion efficiency of the Stirling cycle. Hence, among the desired characteristics of a regenerative heat exchanger are low pressure drop and low thermal conductivity along the flow axis.
The editors of Automotive Engineering International highlight some of the more innovative new products and technologies on display at the SAE 2006 World Congress, based on the latest information provided by exhibiting companies. The TurboDISI engine from FEV is a 1.8-L turbocharged gasoline direct-injection engine that offers impressive low-end torque and a fuel economy typically associated only with diesel engines. The engine, which can replace larger, heavier naturally aspirated engines, also promises reduced emissions compared to naturally aspirated and port-fuel-injected turbocharged engines. Compared to the larger 2.6-L naturally aspirated engine that it replaces, the TurboDISI engine produces the same peak torque and power, but reaches peak torque more quickly while offering better specific fuel consumption throughout the engine map. It minimizes the traditional turbo-lag drawback experienced by conventional turbocharged engines, which is characterized by a delay in the torque rise during acceleration, and applies technologies such as variable valve timing, an integrated charge air cooler in the intake manifold, and advanced charge air devices.
Caterpillar believes that a total revamp of its track-type tractors should trim operating costs by 30 to 70%. As Caterpillar's track-type tractors enter their second century, the OEM has dramatically revamped its undercarriage technology. The company claims its SystemOne upgrades extend operating life, reduce operating costs, and improve ride characteristics. A project team created in 1999 redesigned the undercarriage from the ground up, something that Cat hadn't done since the 1970s. That effort yielded more than two dozen patents.
Costlow, Terry
Ignition and Combustion Process of a Steam Injected Diesel Engine (STID) Studied in a Constant Volume Rig2003-01-324910/27/2003
A new engine concept using direct injection of super heated steam in diesel engines is studied in a Constant Volume Bomb (CVB). The basic idea behind the Steam Injected Diesel Engine (STID) is to reduce the emissions of both particulates and NOx in addition to increasing the efficiency. By using air cooling and exhaust heat to generate the steam, the STID engine is believed to achieve an increase in the shaft efficiency and a substantial reduction of NOx and particulates emissions. This paper presents results from studies of the influence of superheated steam injection on the ignition delay. The justification for the study is the large amount of steam injected necessary for the STID engine and the need for studying the effect of superheated steam on engine operation. The background for the study is the massive steam injection necessary for the STID engine, and a detailed study is required when it comes to its effect on engine operation. Different ratios of air-to-steam mass and steam-to-fuel are selected in the range present in the Wasa 32 engine used for STID experiment at the Wärtsila factory in Finland. The pressure development is measured in these test series. The definition for ignition delay employed is the time from the triggering of the diesel injector until the pressure gradient exceeds dp/dt ≥2. The results indicate a surprisingly moderate dependence of the ignition delay on variations on both air-to-steam ratio and steam-to-fuel ratio in the Constant Volume Bomb (CVB). A small increase is found in the ignition delay as a function of the A/S-ratio. The steam tested was superheated at approximately 500 °C. This high temperature of the steam may explain the minor influence on the ignition and combustion process. Increasing the pressure and temperature inside the Constant Volume Rig at the time of diesel injection from 50 bar to 60 bar reduces the average ignition delay with 23 %.
Bysveen, MarieAlmås, Terje
Performance of Stirling Engine Hybrid Electric Vehicles: A Simulation Approach2001-01-25138/20/2001
Hybrid Vehicles have gained momentum in the automotive industry. The joint action of power sources and energy storage systems for energizing the vehicle improves the vehicle's fuel economy while reducing its pollutant emissions and noise levels, challenging automotive designers to optimize vehicle's cost, weight and control. The marketing success of hybrid vehicles significantly depends on the selection, integration and cost of the energy systems. The internal combustion engine, dominant of the vehicle market, has been the “option of choice” for auxiliary power unit of the hybrid vehicle, although other power sources as fuel cells, Stirling engines and gas turbines have been employed as well [1]. This document is focused in the application of Stirling engines as the power source for automobile propulsion. In order to optimize this process, a simulation tool for Stirling vehicle was developed based in ADVISOR, a proven hybrid electric vehicle simulation software, and MARWEISS, a Stirling engine simulator. [2] The simulation tool allows the study of Stirling-powered vehicles in conventional or hybrid electric (series, parallel or split) configurations, determining parameters of the vehicle like fuel consumption, power output, emissions, energy flow and the engine's temperature profile. The analysis of the simulation results can be employed to identify the critical features of the Stirling-powered vehicle.
Figueroa, LuisFauvel, Owen R.Reader, Graham T.
Experiments have shown that an assembly of multiple free-piston Stirling engines can be designed and constructed in such a way as to both (1) make the vibrations of the engines balance each other to minimize the overall level of vibration, and (2) enable the engines to operate independently of each other, so that if one fails, the other(s) can continue to provide power. Prior to these experiments and to the research and development effort that preceded them, it was not possible to achieve both redundancy and suppression of vibrations: The only previously demonstrated method to balance out vibrations of multiple Stirling engines was by use of counter-oscillating pistons coupled to each other via a common thermodynamic hot space, with the engines driving linear alternators connected electrically in series. This older scheme precludes redundancy because the common thermodynamic interaction and the series electrical connection causes both engines to fail when one fails.
An important secondary topic addressed in the research and development effort described in the preceding article is the use of artificial neural networks to improve the monitoring and thus the control and safety of multiple free-piston Stirling engines. Information collected by monitoring subsystems constitutes essential feedback for use by control and safety subsystems. This information includes such externally measurable quantities as heater-head temperatures, motions of engine housings, and output currents and voltages.
Design and Analysis Code for Radiators of Stirling Power Systems With General Purpose (GPHS) Heat Sources1999-01-26748/2/1999
An efficient finite difference (FD) computational code has been developed for the analysis and design of circular sector radiators for linear alternator output “Free Piston Stirling Engine” space power systems utilizing a radioisotope Pu-238 General Purpose (GPHS) heat source. The code calls on a subroutine developed by the author to solve the second order, fourth degree, ordinary differential equation (ODE) of a fin (extended heat transfer surface) radiating to the space environment. Although the code was originally written for a rectangular coordinates system, it was transcribed into polar (cylindrical) coordinates for the present application. The circular sector radiator panel analyzed has an embedded heat pipe at an arbitrary radial location conducting cycle reject heat from the Stirling engine cold end to the radiator. For a required radiator heat load and a given set of geometrical and thermo-physical properties of the radiator sector, the code will compute the required radiator surface area and mass, surface temperature and heat flux profiles and also the optimum radial location for the heat pipe. A novel second subroutine is also used to determine equilibrium space sink temperatures anywhere within the Solar System. Since this non-zero sink temperature is included in the FD iterative solution of the non-linear ODE, the code has been useful in analyzing radiator temperatures of spacecraft with a perihelion well inside the orbit of Venus, as planned for some deep space missions.
Juhasz, Albert J.Thieme, Lanny G.
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.
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