Browse Topic: Cooling

Items (49)
This SAE Information Report has been prepared at the request of the SAE Road Vehicle Aerodynamics Forum Committee (RVAC), incorporating material from earlier revisions of the document first prepared by the Standards Committee on Cooling Flow Measurement (CFM).Although a great deal is already known about engine cooling, recent concern with fuel conservation has resulted in generally smaller air intakes whose shape and location are dictated primarily by low vehicle drag/high forward speed requirements. The new vehicle intake configurations make it more difficult to achieve adequate cooling under all conditions. They cause cooling flow velocity profiles to become distorted and underhood temperatures to be excessively high. Such problems make it necessary to achieve much better accuracy in measuring cooling flows.As the following descriptions show, each company or institution concerned with this problem has invested a lot of time and as a result gained considerable experience in developing measuring techniques that appear to achieve reliable results. There is, however, little uniformity at the present time among the methods used by different companies and no indication at this time of a trend towards a simple and universally acceptable measuring technique.
Road Vehicle Aerodynamics Forum Committee
Quenching is a heat treatment process for the rapid cooling of a metallic workpiece in water, oil, or air to obtain certain desired material properties. It is the most critical step in the sequence of heat-treating operations to preserve the solid solution formed at the solution heat-treating temperature by rapidly cooling to near room temperature. Because of the complex interaction between temperature, phase-transformation, and stress/strain relation that depends on the temperature distribution and the microstructure of the workpiece, there is no performance-informed quenching process that can be applied reliably to reduce the high scrap rate of airframe aluminum forging parts with a significant amount of residual stress and distortion. Since large aluminum forging parts are increasingly used in aerospace structures to enable structural unitization, it is important to construct a digital twin modeling approach to mirror the physical quenching process for minimizing scrap rate, increasing production efficiency, and engineers and machine operators' handling of variances in forging operations. A high-fidelity modeling of the coupling of thermal, metallurgical, and mechanical interactions is a key component to creating a digital twin of the physical quenching process. A high-fidelity thermal multi-phase computational fluid dynamics (CFD) model is applied to simulate fluid dynamics and temperature fields in the quenchant tank. The developed immersogeometric modeling approach is used next for an efficient model generation of a 3D workpiece with various dipping orientations. Given the temperature and pressure profiles predicted from the CFD-based heat transfer module, residual stress and distortion prediction modules are developed by including temperature and pressure fields mapping and temperature and strain rate dependent property evolution via Abaqus' user-defined subroutines. Verification and demonstration studies are performed using aluminum coupons dipped into a quenching tank with different orientations. Time histories of the temperature and residual stress fields were predicted to explore the relationship between the process and performance.
Lua, JimPhan, NamPiccoli, JoshuaYan, JinhuiKaruppiah, AnandShrestha, Kalyan
In today’s automotive industry, the A/C (Air-conditioning) system is emerging into a high level of technological growth to provide quick cooling, warm up and maintaining the air quality of the cabin during all-weather conditions. In HVAC system, TXV plays vital role by separating high side to low side of vapor compression refrigeration system. It also regulates the amount of refrigerant flow to the evaporator based on A/C system load. The HVAC system bench laboratory conducts the test at different system load conditions to evaluate the outputs from tests during initial development stage to select the right TXV in terms of capacity and Superheat set point for a given system. This process is critical in HVAC developmental activity, since mule cars will be equipped with selected TXV for initial assessment of the system performance. The TXV tuning is conducted in system bench lab using defined test load cases which is developed using combination of given input boundary conditions and tests were conducted based on that. In this paper, major focus is laid on understanding potential importance of each system parameter, identify bench test boundary conditions that are critical for TXV set point decision making and understand internal stakeholder’s requirement. The whole process started with conducting personal interviews with internal stakeholders and suppliers to collect raw voices of customers. The DFSS tools were used to capture internal customer voices and translate into technical measures to provide insight of the data required for TXV selection. Tools used such as voice affinity, HOQ, Pugh Matrix, and Function tree diagram etc. The raw voices from interviews are translated into most important voice and mapped with current process using HOQ approach. The main purpose of house of quality is to derive the measurable targets to meet customer requirement. This study helps us to reduce the number of physical testing by approx. 35% without affecting TXV selection process and use objective approach to study system parameters.
Sambandan, SaravananValencia, ManuelKhawaja, AamirS, Sathish Kumar
Optimization of the Engine Intake Air Temperature through the Air Conditioning Unit2018-01-09734/3/2018
In modern turbocharged internal combustion engines the cooling of the air after the compression stage is the standard technique to reduce temperature of the engine intake air aimed at improving cylinder filling (volumetric efficiency) and, therefore, overall global efficiency. At present, standard values for the intake air temperature are in the range 30-70°C, dependently on engine load, external air conditions and vehicle speed and the adoption of a dedicated cooling fluid operating at low temperatures (-10-0°C) is addressed as the most viable option to achieve an effective temperature reduction. This paper investigates a pilot engine set-up, featuring an evaporator on the intake line of a turbocharged diesel engine, tested on a high speed dynamometer bench: the evaporator was a part of an air refrigeration unit – the same used for cabin cooling - composed also by a compressor, a condenser and a thermostatic expansion valve. The effects of the undercooling of the charge air have been experimentally assessed in terms of fuel consumption and regulated emission reduction, evaluated on the most common engine operating points. Mechanical power needed by the compressor was obviously taken into account in order to assess the overall benefits. A fuel consumption reduction has been demonstrated in the order of 2.5% when the intake air subcooling is turned on. A benefit on the regulated emissions has been observed (NOx, PM). HC and CO behavior, on the contrary, deserves some more attention and involves engine control parameters (for instance, EGR rate) and combustion performances.
Di Battista, DavideVittorini, DiegoDi Bartolomeo, MarcoCipollone, Roberto
Improved Modeling of Near-Wall Heat Transport for Cooling of Electric and Hybrid Powertrain Components by High Prandtl Number Flow2017-01-06213/28/2017
Reynolds-averaged Navier-Stokes (RANS) computations of heat transfer involving wall bounded flows at elevated Prandtl numbers typically suffer from a lack of accuracy and/or increased mesh dependency. This can be often attributed to an improper near-wall turbulence modeling and the deficiency of the wall heat transfer models (based on the so called P-functions) that do not properly account for the variation of the turbulent Prandtl number in the wall proximity (y+< 5). As the conductive sub-layer gets significantly thinner than the viscous velocity sub-layer (for Pr >1), treatment of the thermal buffer layer gains importance as well. Various hybrid strategies utilize blending functions dependent on the molecular Prandtl number, which do not necessarily provide a smooth transition from the viscous/conductive sub-layer to the logarithmic region. This work relies on the k-ζ-f turbulence model and the underlying hybrid wall treatment, which is capable of predicting the near-wall momentum and heat transfer with more fidelity, compared to the standard or low-Re variants of the k-z-ε turbulence model. Based on a new DNS database for turbulent flow and heat transfer in a heated pipe (Reτ=360, Pr=1, 10, and 20), a two-layer wall heat transfer model has been formulated. A priori analysis and RANS predictions of the reference heated pipe flow are encouraging, showing improvements of the near-wall heat transfer predictions with respect to accuracy and mesh independence. The potential of the proposed model in real engineering applications is demonstrated in the cooling of electric/hybrid powertrain components, by simulating heat and fluid flow in the e-motor water jacket model.
Saric, SanjinEnnemoser, AndreasBasara, BranislavPetutschnig, HeinzIrrenfried, ChristophSteiner, HelfriedBrenn, Günter
Thermal Management of Power Batteries for Electric Vehicles Using Phase Change Materials: A Review2016-01-12044/5/2016
As one of the most crucial components in electric vehicles, power batteries generate abundant heat during charging and discharging processes. Thermal management system (TMS), which is designed to keep the battery cells within an optimum temperature range and to maintain an even temperature distribution from cell to cell, is vital for the high efficiency, long calendar life and reliable safety of these power batteries. With the desirable features of low system complexity, light weight, high energy efficiency and good battery thermal uniformity, thermal management using composite phase change materials (PCMs) has drawn great attention in the past fifteen years. In the hope of supplying helpful guidelines for the design of the PCM-based TMSs, this work begins with the summarization of the most commonly applied heat transfer enhancement methods (i.e., the use of thermally conductive particles, metal fin, expanded graphite matrix and metal foam) for PCMs by different researchers. Newly developed TMS configurations such as the multi-layer PCMs and sandwiched ones are also discussed in detail. In addition, the hybrid TMS combining PCM cooling with air or liquid cooling, and battery heating by these PCM-based TMSs under cold environment are also summarized. Based on the analysis of previous studies, several possible research topics on PCM cooling are finally proposed in the conclusion/summary part.
Pan, DongchangXu, SichuanLin, ChunjingChang, Guofeng
An Investigation of Deformation Effects on Phase Transformation in Hot Stamping Processes2016-01-03614/5/2016
To reduce the fuel consumption as well as to improve the crash safety of vehicles, the usage of hot stamping parts is increasing dramatically in recent years. Aisin Takaoka has produced hot stamping parts since 2001 and has developed various technologies related to Hot Stamping. In an actual hot stamping process, parts with insufficient strength could be produced sometimes at a prototyping phase, even under the proper forming conditions. In order to understand these phenomena, in this paper, phase transformation in a boron steel 22MnB5 under various cooling rates were investigated and the effects of pre-strain conditions on the phase transformations were characterised. Uniaxial tensile specimens were stretched under isothermal conditions to different strain levels of 0-0.3, at strain rates of 0.1-5.0/s and deformation temperatures of 650-800°C. A dilatometer was used to measure the dimensional changes of the specimen to rationalize the phase transformation of the boron steel during rapid cooling after deformation. The results showed that the deformation at austenite phase causes the reduction in martensitic phase transformation. For a certain strain level, deformation applied at a lower temperature and a higher strain rate would result in less amount of martensitic phase transformation. In addition, the relations between hot stamping conditions and Vickers hardness, which are normally used as a daily quality check in the industry, are also presented in the paper.
Matsumoto, TakekiLi, NanShi, XinLin, Jianguo
While precise and fast, the down side to cutting with microsecond (ms) fiber lasers has been that the parts require a number of post-processing operations after they are cut, which add significantly to part cost, and can also damage mechanically delicate parts.
The Thermal and Aerodynamic Development of a Cooling and Heat Resistance Package for a New Hybrid Sports Car2015-01-15264/14/2015
A sports car exhibits many challenges from an aerodynamic point of view: drag that limits top speed, lift - or down force - and balance that affects handling, brake cooling and insuring that the heat exchangers have enough air flowing through them under several vehicle speeds and ambient conditions. All of which must be balanced with a sports car styling and esthetic. Since this sports car applies two electric motors to drive front axle and a high-rev V6 turbo charged engine in series with a 9-speed double-clutch transmission and one electric motor to drive rear axle, additional cooling was required, yielding a total of ten air cooled-heat exchangers. It is also a challenge to introduce cooling air into the rear engine room to protect the car under severe thermal conditions. This paper focuses on the cooling and heat resistance concept. The experimental and computational developments of ten air cooled-heat exchangers are described with the tradeoffs that were required during the development process. Since the cooling and heat resistance package was being developed as the vehicle concept and styling were coming together, CFD played a large role in the heat exchanger size, location, heat resistance package and performance. Specific correlation tests were conducted to gain a greater understanding of the performance of some of the heat exchangers. Ultimately, the flow through all of the heat exchangers was confirmed as meeting all the targets at the first wind tunnel test and also heat resistance package was fixed with significant CFD support.
Onishi, YasuyukiRamsay, ThomasJuan, TimothyMcKillen, James
Numerical Analysis of Cooling Effects of a Cylinders in Aircraft SI Engine2014-01-288310/13/2014
This paper focuses on the issues concerning gyroplane powertrain cooling. The Rotax 912S engine was selected as a propulsion system following a detailed analysis. A one-dimensional model, simulated with the AVL Boost software, was applied to determine the heat balance of the engine and the heat flux penetrating through each of engine's surfaces. The geometrical quantities defined in the model were obtained by measuring a three-dimensional geometry provided by an authorized Rotax engine supplier company. Calculation results were then verified by comparing the obtained values with data available from the Rotax 912S engine and with the values of individual parameters given in the literature. The CFD simulation studies, performed with Ansys Fluent, enabled to determine the required airflow capable of absorbing up to 6 kW of heat, the properties for sufficient cooling of the cylinders in the gyroplane powertrain system and the manner of directing the air flow in order to achieve the smallest possible temperature gradient. The modelling tasks were to develop four different design solutions of the cylinder cooling system. As specified in the in-built instruction, the inlet channel was mounted with a constant cross-section of not less than 0.01 m2. The air flow velocity prevented from exceeding the cylinder maximum temperature which should not excess 200°C, as specified by the manufacturer. The proposed solution meets the requirements of the engine installation instructions. The results contain meeting the maximum cylinder temperature requirements with a margin of 18°C and the correct temperature gradients.
Grabowski, LukaszCzyz, ZbigniewKruszczynski, Krzysztof
A Heat Pipe Assisted Air-Cooled Rotary Wankel Engine for Improved Durability, Power and Efficiency2014-01-21609/16/2014
In this paper, we address the thermal management issues which limit the lifespan, specific power and overall efficiency of an air-cooled rotary Wankel engine used in Unmanned Air Vehicles (UAVs). Our goal is to eliminate the hot spots and reduce the temperature gradients in the engine housing and side plates by aggressive heat spreading using heat pipes. We demonstrate by simulation that, for a specific power requirement, with heat spreading and more effective heat dissipation, thermal stress and distortion can be significantly reduced, even with air cooling. The maximum temperature drop was substantial, from 231°C to 129°C. The temperature difference (measure of temperature uniformity) decreased by 8.8 times (from 159°C to 18°C) for a typical UAV engine. Our heat spreaders would not change the frontal area of the engine and should have a negligible impact on the installed weight of the propulsion assembly. We expect our approach could lead to a very significant reduction in thermal stress-induced warping which is primarily responsible for wear and high friction. With reduced friction and wear, the thermal efficiency of the rotary engine is increased, and the durability of the engine would be improved very significantly at the same time. Under proper thermal management, the Wankel engine could be run at a higher rpm to yield a higher specific power. Rotary engines represent a huge emerging market for aerospace as well as a myriad of commercial applications if key issues related to life, combustion efficiency, power density and specific fuel consumption can be improved.
Wu, WeiLin, Yeong-RenChow, Louis
Performances and Opportunities of an Engine Cooling System with a Double Circuit at Two Temperature Levels2012-01-06384/16/2012
In the last years, the design of internal combustion engines (ICE) has evolved significantly, mainly because of the changing demand of mobility, the need to limit the pollution produced by vehicles, and recently, the opportunity to reduce emissions of climate-altering gases. Among the more interesting technologies, those connected to a revision of the engine cooling, as well as, in general, of the thermal needs on board vehicle (oil cooling, intercooling of the turbocharging air, EGR cooling, cabin conditioning...) appear very promising, also because characterized by a lower cost increase per unit of CO₂ saved. In this paper, the Authors present a mathematical model of an internal combustion engine physically consistent that appraises the performances of conventional and unconventional engine cooling systems and the integration of vehicle thermal needs. In particular, the Authors studied a double cooling circuit, at two different temperature levels, that allows several improvements in terms of engine warm up, fuel saving and air boosting. The model has been applied to an existing engine whose experimental characterization was done concerning the heat rejection toward the cooling fluid. On this engine a double circuit at two temperature levels has been proposed, according to a layout which redistributes in an optimal way the engine and vehicle thermal requirements.
Cipollone, RobertoDi Battista, Davide
Study of Hybrid Diffusers for Use in Gas Turbine Combustors2011-01-249610/18/2011
Significant development in the gas turbine technology has brought about an increase in the performance requirements for modern engines. This has generated a significant interest in researching into implementation of novel technologies for various engine components, which will allow for the design of engines to match the new performance requirements. One such technology is the use of hybrid diffusers in gas turbine combustors against conventional combustors like dump diffusers. The hybrid diffuser concept has been around for a while and has the potential of giving a greater performance than conventional diffusers. However, due to limited information available in the public domain, not much has been fully understood about the mechanism of the hybrid diffuser concept. Much of the previous work done on hybrid diffusers are done on designs having a vortex chamber bleed, based on the belief that vortex chambers helps to stabilize the flow separation. However, this paper takes looks into the proposition that the primary mechanism of a hybrid diffuser is the air bleed rather than the vortex chamber itself. This paper looks at a comparative study between a hybrid diffuser with a vortex chamber and that of a new hybrid diffuser design where the vortex chamber is replaced with a duct bleed. The Diffuser Pressure Loss, Bleed Pressure Loss and Pressure Recovery Coefficients of each were analyzed at different bleed rates. The results yield that the duct bleed hybrid diffuser has a similar performance to that of a vortex chamber hybrid diffuser. However, it was observed that a duct bleed needed even less bleed air to achieve a good performance and thus suggesting Walker's proposition to be true that a vortex chamber is not a necessary configuration in hybrid diffuser. Also included is the analysis of performance characteristics of various configurations of duct bleed hybrid diffusers. These include changes in post-diffuser divergence angles, bleed angles and changes in the dump gap. Changes in Diffuser angles do give a better performance but at the expense of larger amount of air bleed from the mainstream. Reducing the bleed angle made no significant gain to the diffuser performance but improved the quality of bleed air which can be used for other purposed like turbine cooling. The paper also discusses as to why there hasn't been any real practical application of this novel technology until now and also suggests specific area where hybrid diffuser could provide immediate benefits.
Khandelwal, BhupendraBao, LiuKumar, Karamveer SinghSethi, VishalSingh, Riti
Self-Configuring Hybrid Duct System and Attachment Technologies for Environmental Control Systems2009-01-327711/10/2009
Environmental Control Systems (ECS) ducts on airplanes are primarily fabricated from aluminum or thermoset composites, depending on temperature and pressure requirements. It is imperative to fabricate lightweight, cost effective, durable, and repairable systems with minimal tooling. It is also important that the duct systems are easy to assemble even with alignment issues resulting from structural variations, tolerance accumulation, variation from thermal expansion of different materials, and inherent duct stiffness. These requirements create an opportunity and need for a technology that can address all of these issues, while increasing performance at the same time. This report provides a background on current ECS ducting systems. It also introduces a new, innovative duct system technology and self-torquing attachment system for use in high temperature and pressure systems with the following characteristics: less than half the weight of current systems it is replacing, cost effective, environmentally friendly, superior durability, self-compensating (i.e. flexibility to conform to specific assembly configurations and accommodates factors such as structural variability and expansion), and inherent vibration and noise dampening capabilities. This new technology meets the stringent FAA regulatory flammability and smoke density requirements, and can be used in over 700 aircraft system applications such as: Ram Air, Avionics Cooling, Trim Air, De-icing, Pressurization, Flight Deck Cooling, APU intake and exhaust, Cargo Heating, Passenger Service Unit, and Cabin Air Conditioning.
Patel, Jayant D.Amorim, Vitor M.
Soymilk And Tofu Processing On Mars: Can We Really Stow It?2004-01-25237/19/2004
The Soymilk, Tofu, Okara and Whey (STOW) Processor Prototype was designated for use in a habitat or extended base [Closed Environment Life Support System (CELSS)] where soybeans will be supplied in bulk or grown locally. Project objectives were to evaluate the STOW Processor’s ability to produce quality soymilk and tofu from the soybean cultivar Hoyt. Hoyt, a small standing, high protein cultivar was selected by the NASA Biomass Production System to be grown hydroponically in the Advanced Integration Matrix (AIM) facility for Mars missions. The quality and yield of the soymilk and tofu from Hoyt was compared to soymilk and tofu produced from three high protein cultivars [Vinton 81 (Gold Standard), C1994, and IA 2032LS]. Composition and characterization of each cultivar was determined using raw soybeans and finished products from small scale stove top systems, large scale steam kettle systems, and STOW simulations. The 2002 field grower Hoyt cultivar had less protein in the bean and resulting tofu than all of the other cultivars. Its tofu and okara were an unacceptable gray/black mottled color compared to the cream colored Vinton 81. IA 2032LS produced the mildest flavored tofu with better yields, texture, and color using less heat than the blanching process. STOW simulations demonstrated that turbulent flow was necessary to properly coagulate the tofu, an automated press was required, and properly coagulated tofu was hard to pump into the press basket. The current STOW needs a major redesign to meet sanitary guidelines, with better temperature and press controls to insure safe and efficient operation. Upon modification, optimization studies can be initiated to produce safe, quality tofu with a minimum of labor for the Advanced Food Technology (AFT) team. Clear hilum, high protein, low beany flavored food grade soybeans, such as Vinton 81 or IA 2032LS should be used to produce soyfoods with lower inputs (solid and liquids) and high quality outputs (yield, sensory properties, low waste).
Wilson, Lester A.Zehr, AndyFrench, Stephen J.Perchonok, Michele
Physical Metallurgy Applications and Enhanced Machinability of Microalloyed V-Ti-N Forging Steels9808842/23/1998
Medium-carbon, microalloyed forging steels represent a cost effective replacement of quenched and tempered grades. Their strength properties are derived from precipitation during cooling from the forging temperature. Because of the relatively high carbon content, vanadium is the most suitable addition to achieve precipitation strengthening. The effectiveness of vanadium is enhanced by the presence of nitrogen. For components subjected to impact loading, improvement in toughness is achieved by refining austenitic grains, pinning their boundaries by means of dispersed titanium nitrides. Precipitation strengthened ferrite-pearlite steels exhibit superior machinability compared to that of quenched and tempered alloy steels. As a result, the total machining costs are substantially reduced compared to the costs of machining heat-treated steels. The frequency of tool breakage and tool changes decrease dramatically, virtually eliminating line scrap and unnecessary downtime. Improved machinability features greatly increase the economic advantages of microalloyed steels. The incorporation of microalloyed forging steels into industrial production requires close cooperation between the steel mill, forge shop, machine shop and component designer. Experience gained in the past decades provides a solid foundation for the safe application of microalloyed forging steels in a variety of critical automotive components. The resulting cost reduction provides the driving force for a rapid adoption of this relatively new class of steels.
Banerji, S. K.Glodowski, R. J.Korchynsky, M.
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