Browse Topic: Air supply

Items (266)
Analysis of cabin depressurization is key to ensuring civil aircraft airworthiness safety. In this study, we use a comprehensive approach to analyze depressurization scenes under regulations such as CCAR 25.841. For cases with and without cabin altitude warnings, we calculated critical leakage areas using an orifice flow model and iterative numerical methods. This combines inputs like emergency descent envelopes, air supply rates, and cabin parameters. In our analysis, we evaluate system failure impact and structural breaches on cabin pressure dynamics. For cases where the critical leakage area failed to meet the limits, we use an equivalent safety analysis based on the Depressurization Exposure Index (DEI). This combines pressure and exposure duration to measure physiological risks. We validated this approach through Simulink simulations and case studies, and found that it supports airworthiness verification, emergency descent optimization, and structural design improvements. This method provides a robust framework for enhancing civil aircraft depressurization safety.
Zheng, Bian
The Stellantis North America Aero-Acoustic Wind Tunnel (AAWT) has been upgraded with a cutting-edge 5-belt Moving Ground Plane (MGP) system, featuring an 8.5-meter center belt and four Wheel Spinning Unit (WSU) belts with advanced coatings for durability and visibility. The expanded 9.4-meter turntable enables ±90° yaw and supports vehicles with wheelbases from 1800 mm to 4500 mm and weights up to 5000 kg, accommodating the full Stellantis North America product range. The original 2-stage boundary layer control system was retained, with new tertiary slots added for improved flow quality. A high-stiffness, six-component Horiba balance with integrated calibration weights and tractive force measurement ensures accurate and precise measurements. Facility enhancements include a 550 m2 building addition for equipment and vehicle prep, a dedicated compressor container for clean air supply, and a vehicle underbody wash booth for efficient cleaning. Commissioning confirmed that flow quality, axial static pressure distribution, and acoustic background noise meet or exceed system specifications. Operational since October 2024, the upgraded AAWT now delivers world-class aerodynamic and acoustic testing capabilities, with enhanced automation, safety, and efficiency.
Lounsberry, ToddLadouceur, BrentFadler, Gregory
Torque transients are challenging for turbocharged diesel engines. Engine torque response is limited by the lag in air flow, restricting the rate at which fuel can be delivered to avoid high engine-out soot emissions. Electrified forced induction systems (EFIS) offer a solution to address this challenge. In this study, an electrified supercharger (e-supercharger) is utilized in addition to the stock turbocharger on a 4.5-L 4-cylinder diesel engine to create a two-stage boosting system. Two control strategies were studied for e-supercharger control during engine transients, a model-based single-input single-output (SISO) controller and a model-based robust multiple-input multiple-output (MIMO) controller. Constant speed load acceptance (CSLA) experiments and emulated drive-cycles were performed to evaluate the performance of each control method. In-cylinder pressure measurements were acquired and apparent heat release calculations were performed and analyzed to better understand the transient engine response. The e-supercharged two-stage boosted engine demonstrated significant improvements over the baseline engine when using both control approaches. The rate of transient power generation was improved by as much as 59.4% resulting in reduced engine speed droop and decreased engine speed recovery time. Transient engine-out soot emissions were also reduced. Although both control approaches improved transient response relative to the baseline engine, the MIMO controller showed the greatest potential for future improvements.
Vang, NicholasRothamer, DavidGhandhi, JaalAshta, ShubhamQiu, WeijinRayasam, Sree HarshaShaver, GregFrushour, BryanDou, Danan
Fuel cell hybrid electric vehicles (FCHEVs) are a promising solution for decarbonizing heavy-duty transport by combining hydrogen fuel cells with battery storage to deliver long range, fast refuelling, and high payload capacity. However, many existing simulation models rely on outdated fuel cell parameters, limiting their ability to reflect recent technological improvements and accurately predict system-level performance. This study addresses this gap by integrating a state-of-the-art, physics-based model of a polymer electrolyte membrane fuel cell (PEMFC) into an open-source heavy-duty vehicle simulation framework. The updated model incorporates recent advancements in catalyst design and membrane conductivity, enabling improved representation of electrochemical behavior and real-time compressor control. Model performance was evaluated over a realistic 120 km long-haul drive cycle. Compared to the traditional fuel cell model, the updated system demonstrated up to 20% lower hydrogen consumption, significantly reduced compressor power demand, and improved cooling performance due to higher stack efficiency. Peak fuel cell efficiency approached 59%. The findings highlight the critical importance of using up-to-date fuel cell models in FCHEV simulations to enable accurate energy predictions and optimal system design. This work supports more effective deployment of zero-emission heavy-duty vehicles through improved model fidelity and control strategy development.
Dursun, BeyzaJohansson, MaxTunestal, Peraronsson, UlfEriksson, LarsAndersson, Oivind
To curb global warming and meet stricter greenhouse gas emission standards all over the globe, it is essential to minimize the carbon footprint of applications in the mobility and transport segment. The demands on mobility, transportation and services are constantly increasing in line with worldwide population growth and the corresponding need for economic prosperity. This ongoing trend will lead to a significant increase in energy requirements for mobility-related applications in the upcoming time, despite all efficiency improvements. The timely introduction and accelerated spread of low-carbon/carbon-neutral energy sources is therefore of crucial importance. In addition to the switch to electric propulsion systems, particularly in the light-duty vehicle sector, the use of advanced and optimized hydrogen (H2)-powered internal combustion engines (ICE) represents a parallel, compatible technical option, as these applications will also meet the most stringent requirements in terms of pollutant and greenhouse gas emissions. In fact, these converted H2 engines produce almost no CO2 emissions at the tailpipe and offer the benefits of known, mature technologies as well as existing production lines and supply chains. Nevertheless, hydrogen as a fuel has specific chemical properties and different combustion behavior that require appropriate development and optimization to meet current and future market requirements. All along with the engine development, the engineering objectives were set to develop the right technological combination which offer power, torque, and transient response comparable to current diesel engines. The upfront simulation work determined the new layout of the combustion system which meets the requirements for optimal in-cylinder charge motion with maximum degree of communality with the Diesel base engine and its original flat cylinder head design. Improvements on the thermodynamic side were achieved with the help of a refined and intensified air supply and an optimized bowl geometry with an adjusted compression ratio. The results shown demonstrate the great potential of hydrogen engine technology. The engine KPI corresponds to those of the base diesel engine and, thanks to the tuning of the engine control and the aftertreatment system calibration, offer almost emission-free driving behavior. The paper closes with a compiling overview and explicit examples of realized achievements to describe the main trends in the upcoming future.
Koerfer, ThomasZimmer, PascalLi, ZhenglingPischinger, StefanLückerath, Moritz
A tested method of data presentation and use is described herein. The method shown is a useful guide, to be used with care and to be improved with use.
S-12 Powered Lift Propulsion Committee
This Aerospace Information Report (AIR) outlines the design considerations and criteria for the control of water carryover from the environmental control system (ECS) with respect to causes and indicated corrective or preventative action. In addition, condensation on structure will be reviewed with possible preventative action described.
AC-9 Aircraft Environmental Systems Committee
This SAE Aerospace Recommended Practice (ARP) contains guidelines and recommendations for subsonic airplane air conditioning systems and components, including requirements, design philosophy, testing, and ambient conditions. The airplane air conditioning system comprises that arrangement of equipment, controls, and indicators that supply and distribute air to the occupied compartments for ventilation, pressurization, and temperature and moisture control. The principal features of the system are: a A supply of outside air with independent control valve(s). b A means for heating. c A means for cooling (air or vapor cycle units and heat exchangers). d A means for removing excess moisture from the air supply. e A ventilation subsystem. f A temperature control subsystem. g A pressure control subsystem. Other system components for treating cabin air, such as filtration and humidification, are included, as are the ancillary functions of equipment cooling and cargo compartment conditioning. The interface with the major associated system, the pneumatic system (Chapter 36 of ATA 100) is at the inlet of the air conditioning shutoff valves. This boundary definition aligns with that in the ATA 100 Specification.
AC-9 Aircraft Environmental Systems Committee
The air supply system in a Fuel Cell Electric Vehicle (FCEV) provides the oxygen needed for the fuel cell to react with hydrogen. The air compressor, being the main component of the air supply subsystem, has the highest power consumption among all auxiliary loads in an FCEV. Therefore, efficient control of the air supply system is critical for improving fuel cell performance. The air supply system has a slow response to dynamic load changes. Due to its weak transient response, an overshoot in airflow can lead to an increase in auxiliary power loss, while an undershoot can cause a delay in meeting power requirements. Thus, reducing transients is a crucial factor in improving the overall system efficiency. In conventional control, the battery supplies additional power needed during dynamic load changes. During high dynamic load changes, there is frequent switching between the battery and the fuel cell. This frequent charging and discharging of the battery can impact its longevity. Currently, the control of the air compressor in the fuel cell is reactive. The proposed solution aims to reduce the losses in the air compressor by predictively tuning the gain parameters of the controller and optimizing the power split between the fuel cell stack and the battery using the predicted vehicle load. Predictive tuning helps in reducing transients in fuel cell air compressor control, ensuring smooth power transfer and minimal losses due to the air system. The proposed method uses the topography ahead information and other vehicle parameters to estimate the load. The air compressor model, coupled with predictive and adaptive tuning, suggests the controller parameters that minimize the air system losses. The switching strategy between the fuel cell stack power and battery power takes the dynamics in predicted load changes into consideration.
Choubey, AyushPonangi, Babu RaoShah, SaurabhMunirajappa, Chandrashekara
Legislative challenges, changing customer needs and the opportunities opened-up by electrification are the major driving forces in today’s automotive industry. Fuel cell vehicles offer the potential for CO2 emission free mobility, especially attractive for heavy duty long-haul range application. The development of key components of fuel cell powered vehicles, namely the fuel cell stack itself as well as the related hydrogen/air supply and thermal management sub-systems, goes hand in hand with various challenges regarding performance, lifetime and safety. The proper layout and sizing of the stack and the related fuel and air supply system components, as well as the suitable dimensioning of the cooling system, are decisive for the overall system efficiency and achievable lifetime. Finally, the different components and sub-systems need to be integrated into the overall powertrain and vehicle configuration together with the related control functions to ensure proper operation under all driving scenarios and ambient conditions. In the above context, system simulation enables to support the development teams in the different phases of the development process, from concept layout, to detailed component and sub-system development to virtual integration and calibration. The current work presents such a versatile multi-physics simulation methodology and provides insights into the modelling fundamentals regarding the various components and subsystems adopted. To confirm the validity of the underlying modelling, comparisons of simulation results with corresponding experimental data are presented for selected fuel cell system components and operating conditions. The applicability of the overall simulation framework to support the development and optimization of fuel cell systems is demonstrated for selected use-cases.
Tatschl, ReinhardPoetsch, ChristophReiter, AntonRitzberger, Daniel
The dynamic response of proton exchange membrane (PEM) fuel cells’ anode pressure and the pressure difference between the cathode and anode significantly influence the performance and durability of fuel cells. To address the slow dynamic response of the anode pressure during rapid load drops, this study proposes a split range control strategy by introducing the hydrogen purge valve into the anode pressure control. By rational planning the split range block, the hydrogen purge valve is opened at appropriate times during load drops. To validate the effectiveness of the split range control, simulations are conducted under load drop conditions using an 80 kW fuel cell hydrogen and air supply subsystem model. The simulation results demonstrate that the split range control reduces the setting time of the anode pressure during load drops by half, with the most significant improvement observed at 67% load to idle condition, where the setting time is reduced from 2.6 s to 1.1 s. Furthermore, the pressure difference between the cathode and anode decreases from 67 kPa to 44 kPa. The impact of hydrogen purge valve frequency is investigated by comparing simulations using a 1 Hz low-speed hydrogen purge valve and a 100 Hz high-speed hydrogen purge valve. The results show that both valves effectively improve the dynamic response of the anode pressure during load drops, with identical maximum pressure differences between the cathode and anode. The findings indicate that the combination of a 1 Hz low-speed hydrogen purge valve and split range control can improve the dynamic response of the anode pressure during load drops.
Zhang, JunyuChen, FengxiangPei, FenglaiLi, TaoXu, Shuo
The multi-stack fuel cell system (MFCS) has the advantages of higher efficiency, stronger robustness and longer life, and could be widely used in high-power application scenarios such as automobiles, airplanes, trains, and ships. The appropriate air mass flow and air pressure have a crucial impact on the output power performance indicators of the MFCS. Considering that the designed integrated air supply system for the MFCS has significant gas supply hysteresis and strong coupling between the inlet air mass flow and air pressure of each stack, this paper identifies multiple steady-state operating points of the fuel cell system to obtain corresponding linear predictive models and establishes corresponding predictive control algorithms. The Model Predictive Control (MPC) algorithms are switched in real-time based on the current load throughout the entire C-WTVC (China World Transient Vehicle Cycle) working condition. The simulation results show that the designed MPC algorithm can control all inlet air flow and air pressure of the MFCS (20kW/70kW/120kW) within the error range of ± 2% of the expected target values, which is significantly better than the PID control algorithm.
Xie, ZhengchunGao, JianhuaZhou, Su
The intention of this standard is to establish a framework to measure the efficiency of PWM HVAC Blower Controllers and Brushless DC Motor Controllers and define a usage based overall efficiency. This result can then be used by vehicle OEMs to demonstrate compliance towards requirements or benchmarks established by regulatory agencies.
ICTMS Supplier Committee
Air Supply Unit (ASU) serves as the pneumatic source for the air suspension system in the passenger car segment. The ASU is an electrically driven oil-free compressor with integrated air dryer to deliver dry air to the suspension system. Solenoid valve, Height Sensor and ECU adjusts the pressure in bellow based on the vehicle load condition. During the lab test, pressure was not building up in the compressor due to delivery valve failure. The type of valve in asu is reed valve type, it is mostly used in the micro compressors due to its low cost, simple structure and light weight configuration. The reed movement is based on the pressure difference between the inlet and the compression chamber. Failure analysis is carried out based on the finite element analysis to identify the root cause, the root cause identified is optimized to prevent the failure. An accelerated test condition is arrived based on the FEA and a tailored series of accelerated tests are carried out to reproduce the failure. The correlation between the test results and the FEA was found satisfactory. The significant factors that are responsible for the failure are identified with their respective control measures. This paper describes the reed valve failure simulation using finite element method and accelerated testing.
Subramanian, VivekT, Dr. SukumarGovindarasu, Anbarasu
Aircraft cabin temperature is controlled by regulating the cabin supply air temperature. This supply air temperature is a critical parameter which varies with respect to aircraft altitude and to be maintained properly to the required value corresponding to that altitude to have a good comfortable condition inside the cockpit. It is affected by many internal factors like engine bleed air flow rate, pressure, and temperature and also with external factors like ambient temperature, pressure, and attitude. Due to huge variations in these parameters especially in a fighter aircraft, the cabin temperature control system of this aircraft is often experience limit cycle oscillations and subsequent cabin temperature fluctuations. To minimize the cabin temperature fluctuations, suitable control logic needs to be considered at the design stage itself to avoid future tuning of such control system which makes additional flight-tests and generates large expenses. This paper focuses in developing the control strategies for a fighter aircraft cabin temperature control system using simulation model of ECS system presented in the previous work. The electronic controller of the system, using its control strategies, drives the actuator or Temperature Control Valve (TCV) to maintain the required temperature. The control architecture in the model has been modified to analyze different control strategies. Most of the conventional control0 methods or schemes do not take account the effect of variation in the input parameters on system performance in their control logic. This paper compares three different control strategies viz. PID, Time-delay control and a novel Variable Time-delay control along with control input normalization. The control strategies along with system architecture are modeled in LMS AMESim and transient responses of temperature control system have been studied for different control strategies. Finally, the novel control strategy using variable time-delay control with Control Input Normalization (CIN) is proposed, which minimizes the actuator movement, reduces temperature fluctuations and improves the system performance.
A, SathiyaseelanSelvan, V. Arul Mozhi
Proton exchange membrane fuel cells (PEMFC) are considered an environment-friendly alternative vehicle power in the future owing to their high power density and zero-carbon emission. To research the performance of the air supplied by the PEMFC air system, the PEMFC air system bench composed of an air compressor, cooler, emulated stack, back-pressure valve, and sensors was built. Then, a PEMFC system test bench composed of a hydrogen supply subsystem, stack, air supply subsystem, electronic control subsystem, and cooling subsystem was established. The fuel cell system control parameters and control method are complex due to the coupling and nonlinearity of the air supply system. The strategy composed of a feedforward table and piecewise proportional integral (PI) feedback control strategy was employed to regulate the pressure and flow rate of the air supply system. The air compressor map and the mapping relationship among the air compressor speed, opening of the back-pressure valve, and stack current were obtained by carrying out experiments on the PEMFC air system bench. The results show that the air pressure and flow rate follow the reference value, and the flow error and pressure error are 1.5 g/s and 0.25 kPa, respectively. The proposed strategy can coordinately control the air flow rate and pressure, and it can provide qualified pressure and flow rate for the PEMFC stack.
Zhang, BaitaoGong, DapengLiu, ZeXu, Sichuan
This SAE Recommended Practice provides instructions and test procedures for air braked vehicles including but not limited to trucks, truck-tractors, trailers, dollies, and buses used on highways but does not include off-highway vehicles.
Truck and Bus Brake Supply and Control Components Committee
This SAE Aerospace Recommended Practice (ARP) applies to blankets used for passenger comfort within transport category aircraft cabins. When the term “blanket” is used in this document it refers to all blankets that are provided by the aircraft operator for passenger warmth.
S-9A Safety Equipment and Survival Systems Committee
The existing compressor plants at railroad marshalling yards (MYs) are equipped with automatic compressed air supply control systems. However, this is implemented using outdated and ineffective methods. Taking into account the current trends in the field of three-phase motor control, as well as the requirements for energy saving, the most effective is the frequency regulation of performance. The work provides a justification for the need to use a variable frequency drive of a compressor unit (CU). A mathematical model has been developed for controlling an asynchronous motor (AM), taking into account the setting coefficient of performance. As a result, a computer simulation model for controlling the drive motor of a reciprocating compressor at an MY has been proposed and tested. The diagrams and values obtained made it possible to study in detail the automatic control system of the drive and select the optimal control laws for the frequency-controlled unit. An analysis of the results of simulation modelling showed that at the moments of starting and stopping the machine, transient surges of currents, voltages, and mechanical shocks are eliminated, which will significantly extend the service life of electrical and mechanical components. And the control characteristic will reduce energy consumption due to the optimal control of the motor speed and, as a consequence, the unit performance. Thus this model and principle can be applied in real installations. As a result of this approach, an economic effect is expected due to optimal performance management and savings on maintenance and replacement of compressor station power units.
Satsiuk, AleksandrVolodarets, MykytaGritsuk, IgorLitikova, HalynaPodnebenna, SvitlanaBelousov, EvgenVolkov, VladimirAhieiev, MaksymPohorletskyi, DmytroZinchenko, SerhiiKhudiakov, Igor
Vehicle aerodynamics has been the subject of extensive research, with a heavy emphasis on the vehicle. Heavy vehicles, such as trucks and buses, have undergone aerodynamic studies in recent years to reduce drag and improve fuel economy [1]. In this study, the distribution of air conditioning in the cabin of a passenger bus was investigated by discussing the factors that influence in attaining the desired thermal comfort values such as temperature distribution, relative humidity ratios, and air velocities inside the bus. The research was conducted on three different cases. In this study, different types of air-conditioning (AC) outlets—linear grills, slots diffusers, and gaspers—were used, and the effect of each outlet on temperature distribution, air velocities, and relative humidity ratios within the bus was investigated. In all three cases, the inlet air velocity was set to 0.8 m/s, and the return air was combined in the middle of the bus. Finally, comparisons were made between the cases to determine the best case for achieving the thermal comfort rates inside the bus. The results demonstrated that the slots diffuser could not be used in the bus air conditioning because of the presence of turbulences and swirl motions which impeded the flow of cold air. The gasper is the best flow outlet in the air distribution inside the cabin that achieves the required thermal comfort for the passengers because the flow is laminar and there is no turbulence, resulting in a good mixing between the conditioned air and the air inside the bus cabin and a good distribution of temperature inside the bus.
Hassan, Mahmoud Issa
This document deals with ground and flight test of airplane installed Environmental Control Systems (ECS), Figure 1. The ECS provide an environment, controlled within specified operational limits of comfort and safety, for humans, animals, and equipment. These limits include the following: pressure, temperature, humidity, ventilation air velocity, ventilation rate, wall temperature, audible noise, vibration, and environment composition (ozone, contaminants, etc.). The ECS are composed of equipment, controls, and indicators that supply, distribute, recycle and exhaust air to maintain the desired environment.
AC-9 Aircraft Environmental Systems Committee
An airplane fuel tank inerting system provides an inert atmosphere in a fuel tank to minimize explosive ignition of fuel vapor. This SAE Aerospace Information Report (AIR) deals with the three methods of fuel tank inerting systems currently used in operational aircraft: (1) on-board inert gas generation systems (OBIGGS), (2) liquid/gaseous nitrogen systems, and (3) halon systems. The OBIGGS and nitrogen systems generally are designed to provide full-time fuel tank fire protection; the halon systems generally are designed to provide only on-demand or combat-specific protection. This document also addresses other design considerations that affect fuel tank flammability such as fuel tank pressure and other methods for reducing fuel tank flammability. This AIR does not treat the subject of explosion suppression foam (ESF) that has been used for fuel tank explosion protection on some military aircraft. ESF is also available for retrofit for commercial airplanes. The primary disadvantages of foam are weight, reduction of usable fuel, and the added maintenance complexity when the foam must be removed for tank maintenance or inspection. AIR4170 is an excellent reference for the use of ESF for fuel tank explosion protection. Note that across the military and commercial aviation industry, different terminology has been used regarding fuel tank inerting. In military applications, the system is referred to as on-board inert gas generation system (OBIGGS). Regulatory agencies use the term flammability reduction means (FRM). OEMs in commercial applications use several terms: fuel tank inerting system (FTIS), flammability reduction system (FRS), inert gas system (IGS) and nitrogen generation system (NGS).
AE-5D Fuel Tank Flammability Reduction Systems Committee
Developing a NEXT-GEN VGT21TOFHP10_0310/1/2021
Engineers from Mitsubishi Heavy Industries refine the design of a variable geometry turbocharger for commercial vehicles. Variable geometry turbochargers (VGT) have been applied to commercial engines for a long time, owing to their operability at wide operation range. One of the major advantages of using a VGT is its ability to provide high boost pressure at low engine speeds, which ensures optimum supply of air for proper combustion, leading to a significant reduction in emissions. Recent emission standards by U.S. EPA and in Europe (Euro VI) demand a higher efficiency from the turbine at all operating points, which motivated engineers from Mitsubishi Heavy Industries to do an in-depth loss analysis of each component and carry out design modifications to achieve these demands. The multi-vane VGT, which has been found to be the most effective among all the configurations, consists of a plurality of nozzle vanes distributed circumferentially upstream of the radial turbine rotor. These vanes are controlled by an electric actuator working in coherence with the engine control unit (ECU) to control the mass flow rate entering the rotor. There are many different types of link mechanisms to transfer the actuation force to the vanes; the authors selected a mechanism consisting of a plurality of lever arms connected to each vane, driven by a drive ring moved circumferentially using a crank arm connected to the actuator.
The article proves the necessity for heating the air in the pneumatic engine of a hybrid power unit designed for moving a compact wheeled vehicle. The aim is to improve the pneumatic engine operation indicators by heating the compressed air before it is supplied to the cylinder using the obtained theoretical and experimental studies. For the easy-to-use of assessing the effectiveness of heating the air supplied to a pneumatic engine, the experiments were carried out by two pressure ps = 0.7 MPa and ps = 0.9 MPa, according to them the testing of a pneumatic unit was conducted without heating the compressed air at the temperature equal to the ambient temperature Ts = 293 K. Also, during the experiments a pneumatic engine was tested at other temperatures while supplying the compressed air at the inlet to the engine cylinder. So, at an inlet pressure ps = 0.7 MPa, the compressed air was heated up to the temperature Ts = 383 K, and at a pressure ps = 0.9 MPa it was heated up to the temperature Ts = 388 K. The conclusions reached regarding the efficiency of heating the air at the inlet to the pneumatic power unit cylinders were drawn for the case when the pneumatic engine is used as part of a vehicle hybrid power unit and the air is heated by using the heat of exhaust gases from an internal combustion engine operating simultaneously or a heat accumulator. The studies carried out in this article make it possible to determine the feasibility of the joint use of a pneumatic power unit and an internal combustion engine, not only in severe operating conditions with heavy traffic on busy road sections of large cities and megalopolises, but also during the independent operation of a pneumatic engine in traffic jams..
Leontiev PhD, DmitryVoronkov, OleksandrNikitchenko, IgorKorohodskyi, VolodymyrRyzhykh, LeonidRudenko, NataliiaMakarova, Tamara
Cabin Thermal Management Analysis for SuperTruck II Next-Generation Hybrid Electric Truck Design02-14-03-00229/9/2021
This article presents a multistage, coupled thermal management simulation approach, informed by physical testing where available, to aid design decisions for PACCAR’s SuperTruck II hybrid truck cabin concept. Focus areas include cabin insulation, battery sizing, and sleeper curtain position, as well as heating, ventilating, and air-conditioning (HVAC) component and accessory configurations, to maintain or improve thermal comfort while saving energy. The authors analyzed weather data and determined the national vehicle miles traveled weighted temperature and solar conditions for long-haul trucks. Example weather day profiles were selected to approximate the 5th and 95th percentile weighted conditions. A daylong drive cycle was developed to impose appropriate external wind conditions during rest and driving periods. Using the National Renewable Energy Laboratory’s vehicle HVAC modeling and simulation tool VTCab, HVAC load design trade-off studies for the new truck geometry concept were completed. Parameters analyzed included effects of paint color, insulation, glass transmissivity, and curtain location. Simulation results helped with early design material selections for efficient cabin climate control. A detailed three-dimensional computer-aided engineering (CAE), computational fluid dynamics (CFD), radiation, and human physiology co-simulation, referred to in this article as CAE Thermal-CFD, was used to evaluate thermal comfort and energy impacts of diffuser configurations and air supply settings in driving and hoteling modes. Analysis revealed that it is more difficult to heat the cabin in hoteling mode during the winter than to cool the space in the summer. This seasonal load profile drives the requirement of additional energy storage for heating comfort. To determine the battery capacity requirement, multiday HVAC operation drive cycle simulations were then completed, showing that a 15-kWh battery would be required for HVAC operation during hoteling. Results helped reduce cabin thermal loads, determine component sizing requirements, and improve occupant comfort to save fuel and contribute to the economic viability of the hybrid system.
Okaeme, CharlesLustbader, JasonSigler, CoryJorgensen, InerGrover, BenKiesser, JordanMoniot, Matthew
This document considers the cooling of equipment installed in equipment centers, which usually consist of rack-mounted equipment and panel mounted equipment in the flight deck. Instances where these two locations result in different requirements are identified. This document generally refers to the cooled equipment as E/E equipment, denoting that both electrical and electronic equipment is considered, or as an E/E equipment line-replaceable-unit (LRU). The majority of cooled equipment takes the form of LRUs. The primary focus of this document is E/E equipment which uses forced air cooling to keep the equipment within acceptable environmental limits. These limits ensure the equipment operates reliably and within acceptable tolerances. Cooling may be supplied internally or externally to the E/E equipment case. Some E/E equipment is cooled solely by natural convection, conduction, and radiation to the surrounding environment. This document discusses specification requirements, system design considerations, component design, and system testing. It also discusses the analysis and test considerations for the thermal design of the avionic equipment. The discussion of supplementary cooling systems includes consideration of a refrigeration system. This document just covers air cooling of equipment. AIR1811 should be consulted for information on liquid cooling of equipment. Although this document is targeted at transport category airplanes, most of the material applies to other classes of aircraft with possible adaptions.
AC-9 Aircraft Environmental Systems Committee
This SAE Aerospace Information Report (AIR) provides information on aircraft cabin air quality, including: Origins of chemical airborne contaminants during routine operating and failure conditions. Exposure control measures, including design, maintenance, and worker training/education. This AIR does not deal with airflow requirements.
AC-9 Aircraft Environmental Systems Committee
The centrifugal compressor is one of the most commonly used air compressors for fuel cell air supply systems, and it has the small volume, high pressure ratio and low noise. However, surge in a centrifugal compressor severely limits its stable flow range. In this paper, a mathematical model of the compressor aerodynamic performance based on the energy transfer method was established, some parameters of model were identified by experimental data, and the model was validated through experiments. Then the dynamic model of the compression system was derived based on the compressor model and the Moore-Greitzer model. The stability analysis of the compression system was conducted, and it was strictly proved that when the compression system is unstable, there is the limit cycle in this nonlinear system, namely the surge cycle. Furthermore, the simulation of the compression system was conducted and the instability condition of the compression system was presented. The results show that at almost all constant speeds, the compression system instability occurs as the opening of the throttle valve decrease to a specific value, and at some opening of the throttle valve, the compression system instability occurs as speed decrease to a specific value. At last, the effects of structural parameters of the compression system on surge characteristics were analyzed. This research can guide the operating condition match of compressors and the active surge control design of the compression system for fuel cell vehicles.
Chen, SiyueZuo, ShuguangWu, Zhipeng
In Toyota’s 2nd generation FCV, an electric turbo-type air compressor has been adopted for downsizing and cost reduction. Automotive Fuel Cell applications present several challenges for implementing a turbo-type air compressor. When operating a fuel cell in high-temperature or high-altitude locations, the FC stack must be pressurized to prevent dry-up. The flow rate vs pressure conditions that the FC must pass through or in some cases operate at are typically within the surge region of a turbo-type air compressor. Additionally, Toyota requires quick air transient response (< 1 sec) for power generation, energy management, and FC dry-up prevention. If the turbo-type air compressor is not precisely controlled during quick transients, it can easily enter the surge region. To solve the above issues, we developed a new air supply controller which can avoid compressor surge by controlling 3 variables, ‘FC stack air flowrate’, ‘FC stack air pressure’, and ‘FC stack air Bypass’ independently with high accuracy. The controller was designed using a model-based development approach. At first, the physical characteristics of the air systems compressor, valves, pipes, and FC stack were modeled and integrated into a system level simulation that can run real-time on-board the vehicle Engine Control Unit (ECU). Next, the feedforward and feedback (PI) control were developed by implementing inverse models of the air system component equations. We confirmed that this control development approach could achieve Toyota’s air supply control performance requirements and prevent turbo-type air compressor surge.
Tomi, NaokiHasegawa, ShigekiFarnsworth, JaredImanishi, HiroyukiIkogi, YoshihiroSato, Kenichiro
Control Strategies for Prevention of PEMFC Oxygen Starvation: A Review2021-01-07434/6/2021
Proton Exchange Membrane Fuel Cell (PEMFC) which has advantages of starting fast, high energy density, high efficiency, lower operating temperature and little pollution is widely regarded as one of the most promising energy sources. The PEMFC system includes several subsystems such as air supply subsystem, hydrogen supply subsystem, thermal management subsystem, water management subsystem, energy management subsystem and so on. The Air supply subsystem has great influence on the performance and life of PEMFC stack. Whether oxygen supply in air supply subsystem is sufficient or not will affects reaction rate of fuel, the operating temperature and degradation of PEMFC stack and so on. To solve the issue of oxygen starvation in PEMFC stack, the control strategies for improving dynamic response and preventing air shortage of the PEMFC air supply subsystem are reviewed. In this paper, the traditional proportional integral differential control, model predictive control, self-adaptive control, sliding mode control, robust control, intelligent control consists of fuzzy logic control, neural network control and composite control are analyzed. In addition, the control oriented model used to calculate the output power is essential in control system, so this part is also studied. In each section, different control methods and models are classified and various investigation techniques for evaluating efficiency of air supply subsystem are discussed, by comparing and summarizing the various control strategies, the prospect of solving the problem of oxygen starvation is put forward. At the end, on the strength of the current status of the research studies, topics, activities that require further research on preventing PEMFC oxygen starvation are discussed.
Gong, DapengXu, SichuanZhang, Baitao
This SAE Aerospace Information Report (AIR) covers the design parameters for various methods of humidification applicable to aircraft, the physiological aspects of low humidities, the possible benefits of controlling cabin humidity, the penalties associated with humidification, and the problems which must be solved for practical aircraft humidification systems. The design information is applicable to commercial and military aircraft. The physiological aspects cover all aircraft environmental control applications.
AC-9 Aircraft Environmental Systems Committee
This SAE recommended practice provides procedures and methods for testing service, spring applied parking and combination brake actuators for air disc brake applications. Methods and recommended samples for testing durability, function and environmental performance are listed in 1.1 and 1.2.
Truck and Bus Brake Actuator Committee
Hybrid powertrains utilize an engine to benefit from the power density of the liquid fuel to extend the range of the vehicle. On the other hand, the electric machine is used for; transient operation, for very low loads and where legislation prohibits any gaseous and particulate emissions. Consequently, the operating points of an engine nowadays shifted from its conventional, broad range of speed and load to a narrower operating range of high thermal efficiency. This requires a departure from conventional engine architecture, meaning that analytical models used to predict the behavior of the engines early in the design cycle are no longer always applicable. Friction models are an example of sub-models which struggle with previously unexplored engine architectures. The “pressurized motored” method has proven to be a simple experimental setup which allows a robust FMEP determination against which engine friction simulation can be fine-tuned. This is due to the elimination of the experimental variability introduced by combustion, whilst retaining the fired-like load on the cranktrain, as reported in SAE 2018-01-0121. It employs a “shunt pipe” recirculating air from the exhaust back into the intake, therefore requiring very little air supply demands. The temperature of the bulk gas was also maintained similar to that of a fired engine with the use of Argon as the working gas, reported in SAE 2019-01-0930. Mixtures of Argon-to-air were also used to investigate the effect of temperature on FMEP, published in SAE 2019-24-0141 and SAE 2020-01-1063. This leaves one pending criticism of the pressurized motoring method - that of having a relatively fixed location of peak pressure (≈1DegCA BTDC), when compared to a fired engine, which is around 10DegCA for CI and 20DegCA for SI. In this publication, a simulation investigation is performed to assess the viability and extent of an experimental modification to the pressurized motoring method, involving the use of small fuel injections to shift the location of peak pressure in the aim of replicating better the fired engine, whilst retaining the benefits of a motored setup.
Sammut, GilbertPipitone, EmilianoCaruana, CarlFarrugia, Mario
Mechanical friction and heat transfer in internal combustion engines are two highly researched topics, due to their importance on the mechanical and thermal efficiencies of the engine. Despite the research efforts that were done throughout the years on both these subjects, engine modeling is still somewhat limited by the use of sub-models which do not fully represent the phenomena happening in the engine. Developing new models require experimental data which is accurate, repeatable and which covers wide range of operation. In SAE 2018-01-0121, the conventional pressurized motored method was investigated and compared with other friction determination methods. The pressurized motored method proved to offer a good intermediate between the conventional motored tests, which offer good repeatability, and the fired tests which provide the real operating conditions, but lacks repeatability and accuracy. A ‘shunt pipe’ was utilized between the intake and exhaust manifolds which reduced significantly the air supply demand. In SAE 2019-01-0930, Argon was used in place of air in the experimental setup which resulted in bulk gas temperatures synonymous to the fired engine. In SAE 2019-24-0141 and SAE 2020-01-1063 mixtures between air and Argon were utilized to investigate the relationship of mechanical friction with a controlled gradual increase in the bulk in-cylinder temperature. In this publication, a one-dimensional engine model is developed to assess the capability of the 1D model to capture the effects on the motored engine imposed by changing the working gas. From the experimental studies on the pressurized motored engine, increasing the proportion of Argon to air showed an increase in the peak bulk gas temperature of around 600°C. This resulted in an increase in the heat losses, a decrease in the pumping losses and no measureable difference in the mechanical friction.
Sammut, GilbertPipitone, EmilianoCaruana, CarlFarrugia, Mario
This SAE Aerospace Information Report (AIR) includes a discussion of liquid and particulate contaminants which enter the aircraft through the environmental control system (ECS). Gaseous contaminants such as ozone, fuel vapors, sulphates, etc. are also covered in this AIR. This publication is concerned with contamination sources which interface with ECS and fuel tank inerting systems, and the effects of this contamination on equipment. Methods of control will be limited to the equipment and interfacing ducting which normally falls within the responsibility of the ECS designer.
AC-9 Aircraft Environmental Systems Committee
Fuel cell technology can play a major role in reducing transportation-related emissions, especially in heavy-duty, long-haul applications. Consequent transfer of technology from air supply systems for combustion engines to cathode air paths serves as an enabler for necessary system cost reduction. To achieve the required system lifetime, the supply of clean air is essential. Gases like NOx, SO2 and NH3 poison the catalyst, leading to increased stack degradation rates. Effective removal with functionalized activated carbons enhances the catalyst´s lifetime. Research on real-life concentrations of these contaminants under different driving patterns and road profiles enables knowledge-based design of cathode air filter elements. To prevent flooding of components like air filter, humidifier, or stack, water separators are integrated at different position inside the system. Plastic air ducts with integrated sensors and flaps required to manage the air flow connect the different functional components. Broadband silencers are applied to reduce noises inside the system, e.g. generated by the compressor. Essential components like humidifier and air-cooler can easily be incorporated into the system. In the cathode air exhaust path, an additional water separator is applied to protect turbine blades and to prevent emission of splash water from the tailpipe. The consistent transfer of technology from air supply systems for combustion engines to cathode air paths enables cost-, noise and packaging-optimized, plausible system concepts with enhanced energy efficiency.
Harenbrock, MichaelKorn, AlexanderWeber, AndreasHallbauer, Eva
Continuous efforts to improve thermal efficiency and reduce exhaust emissions of internal combustion engines have resulted in development of various solutions towards improved lean burn ignition systems in spark ignition engines. The Dual Mode, Turbulent Jet Ignition (DM-TJI) system is one of the leading technologies in that regard which offers higher thermal efficiency and reduced NOx emissions due to its ability to operate with very lean or highly dilute mixtures. Compared to other pre-chamber ignition technologies, the DM-TJI system has the distinct capability to work with a very high level of EGR dilution (up to ~40%). Thus, this system enables the use of a three-way catalyst (TWC). Auxiliary air supply for pre-chamber purge allows this system to work with such high EGR dilution rate. This work presents the results of experimental investigation carried out with a Dual Mode, Turbulent Jet Ignition (DM-TJI) optical engine equipped with a cooled EGR system. The results show that the DM-TJI engine could maintain stable operation (COVIMEP<2%) with 40% external EGR at stoichiometric (λ ~ 1) operating conditions. The relative timing between the auxiliary air and fuel inside the pre-chamber was found to be critical to maintaining successful operation at 40% EGR diluted condition. Ultra-lean (up to λ ~ 2) operation was also demonstrated at two different compression ratios with good combustion stability. A range of pre-chamber nozzle orifice diameters were tested with both lean and EGR diluted conditions. In general, smaller orifice diameters resulted in shorter overall burn duration due to more favorable distribution in ignition sites.
Atis, CyrusChowdhury, Sadiyah SabahAyele, YidnekachewStuecken, ThomasSchock, HaroldVoice, Alexander K.
A Modular Internal Combustion Engine Blow Rig and Cold-Flow Analysis Concept for Industrial Particle Image Velocimetry Measurements under Steady, Near-Reality Charge Air Conditions03-13-03-00223/19/2020
A modular, stationary IC engine blow rig for differential and integral flow field measurements using particle image velocimetry (PIV) has been developed. Unlike conventional PIV blow rigs, the given design is capable of operating under near-reality charge air conditions, that is, highly pressurized, hot intake air supply at high flow rates. Its conceptual flexibility as well as peripheral infrastructure allow for comprehensive and wide-ranging flow field analysis. Because of a modular architecture, it is neither confined to a specific cylinder head design nor limited solely to the application of PIV for differential flow field analysis. It also already accounts for direct inlet flow determination through an additional PIV access point upstream of the cylinder head. The inlet and outlet ducts have been designed with regular shapes and smooth walls, such that a digital twin-type CFD model of the blow rig is conveniently feasible. A specifically developed pseudostereoscopic reconstruction method is applied to acquire fully 3D volumetric velocity fields from plain sequential 2D measurements using only a single PIV camera and laser sheet. The resulting volumetric flow field is used to, for instance, determine the locations of vortex cores, 3D streamlines as well as zonal swirl coefficients in the sense of a “virtual paddle wheel” measurement.
Lichtmes, MartinFreitag, MartinFrenzel, MathiasHarder, Peter
This SAE Recommended Practice provides instructions and test procedures for measuring air consumption of air braked vehicles equipped with Antilock Brake Systems (ABS) used on highways.
Truck and Bus Brake Systems Committee
The dynamic and efficiency of automotive fuel cell drives is significantly influenced by air supply system. Different air compression architectures use electric compressor (EC), electric turbocharger (ETC), or a serial booster (SB) consisting of turbocharger and electric compressor. These three variants of air compression systems were modeled using a map approach and added to a 0D fuel cell air supply model. The characteristic maps of the turbomachinery were measured on the test bench under fuel cell conditions. Subsequently, the calculated isentropic efficiencies were corrected with respect to heat transfer phenomena occurring during the measurement. Moreover, a scaling method for the maps of the turbomachinery is explained. The initial simulation of the air compression systems with equal diameters for the turbomachinery showed no difference in the mechanical power demand. Therefore, the particle swarm algorithm (PSA) was applied to optimize the turbomachinery maps of EC, ETC, and SB with the scaling method. The PSA reduces the mechanical power demand of EC by 17%, of ETC by 18%, and of SB by 27%. This leads to the lowest power consumption of SB followed by ETC and last EC. The best performance of SB is caused by the higher recuperated mechanical power of the turbine.
Uhrig, FlorianSchinnerl, MarioHaluska, PeterKurzweil, Petervon Unwerth, Thomas
Research on Control Algorithm of Air Supply System for High-Pressure PEMFC Engine2019-01-03794/2/2019
The Proton Exchange Membrane Fuel Cell (PEMFC) is the most widely used engine in fuel cell vehicles. For PEMFC, whether the supply of oxygen for cathode is adequate or not is a critical factor for its net output power and service life, and the proper control of air supply mass flow and pressure can effectively improve its system performance and efficiency. At present, fuel cells need to reduce the mass and volume and increase the power density. Therefore, it is necessary to increase the air supply pressure for PEMFC. But at the same time, many auxiliary devices are appended to the system to provide high-pressure air, such as air compressor, intercooler, and back pressure valve, which make the control of the entire air supply system very complicated. So an excellent control algorithm is needed. This paper mainly focuses on the air supply system of a 85kW high-pressure PEMFC stack, researches its control algorithms, and discusses and studies the control effects of the feedforward control and the feedback control. For the feedback control, the traditional PID method is firstly studies, and the relationship between the fuel cell stack’s pressure and mass flow under different working conditions is analyzed. After that, the decoupled PID control algorithm is used to eliminate the mutual coupling among different channels. Then, the paper researches the model predictive control (MPC) algorithm and compares its effects with those of the PID algorithm. Finally, the linear variable parameter (LPV) model is constructed as the predictive model of MPC. This paper also studies the control effects of adaptive MPC algorithm and single-point MPC algorithm, which shows that the former can gain control effects with higher precision of the stack’s pressure and mass flow in the whole working condition range.
Chen, FengxiangLin, ZhichengJiao, JieranHe, Jilong
Experimental PEM-Fuel Cell Range Extender System Operation and Parameter Influence Analysis2019-01-03784/2/2019
Fuel cells as alternative propulsion systems in vehicles can achieve higher driving ranges and shorter refueling times compared to pure battery-electric vehicles, while maintaining the local zero-emission status. However, to take advantage of pure battery electric driving, an externally rechargeable battery can be combined with a fuel cell range extender. As part of a research project, an efficient air supply system for a fuel cell range extender was developed. To this end, a 25 kW PEM fuel cell system test bench was set up. The different parameter influences of the test bench, in particular of the air supply system, were analyzed and evaluated in terms of stack/system efficiency and functionality. The control software of the test bench was specifically developed for the flexible operating parameter variation. All adjustable variables of the system (air ratio, stack temperature, pressure, etc.) were varied and evaluated at steady-state operating points. Likewise, the system was analyzed during dynamic operation and fault cases in adverse operating conditions (water condensation, oxygen deficiency) were identified. The system's warm-up process was also evaluated in regard to efficiency and functionality, since at lower temperatures, a larger air mass flow is needed to counteract water condensation inside the stack. Finally, the hydrogen purging losses were quantified at different operating pressures purging intervals. The experimental results show that, above all, the air supply has a significant influence on the efficiency of the system and is decisive for the proper operation and further improvement of the system. In summary, depending on the load point and operating conditions, a system efficiency between 42 % and 56 % was achieved.
Höflinger, JohannesHofmann, PeterGeringer, Bernhard
This SAE Recommended Practice provides procedures and methods for testing service, spring applied parking, and combination brake actuators with respect to durability, function, and environmental performance. A minimum of six test units designated A, B, C, D, E, and F are to be used to perform all tests per 1.1 and 1.2.
Truck and Bus Brake Actuator Committee
This document summarizes published measurement data and reference values for marker chemical compounds listed in ARP4418 (see 2.1.1) potentially found in aircraft engine bleed air.
E-31B Bleed Air Committee
This SAE Aerospace Recommended Practice (ARP) contains guidelines and recommendations for subsonic airplane air conditioning systems and components, including requirements, design philosophy, testing and ambient conditions. The airplane air conditioning system comprises that arrangement of equipment, controls and indicators that supply and distribute air to the occupied compartments for ventilation, pressurization, and temperature and moisture control. The principal features of the system are: a A supply of outside air with independent control valve(s). b A means for heating c A means for cooling (air or vapor cycle units and heat exchangers) d A means for removing excess moisture from the air supply e A ventilation subsystem f A temperature control subsystem g A pressure control subsystem Other system components for treating cabin air such as filtration and humidification are included, as are the ancillary functions of equipment cooling and cargo compartment conditioning. The interface with the major associated system, the pneumatic system (Chapter 36 of ATA 100) is at the inlet of the air conditioning shutoff valves. This boundary definition aligns with that in the ATA 100 Specification.
AC-9 Aircraft Environmental Systems Committee
Experimental Investigation of the Aerodynamic Benefits of Truck Platooning2018-01-07324/3/2018
Lawrence Livermore National Laboratory (LLNL) has conducted a series of scaled wind tunnel tests to investigate the aerodynamic benefits of heavy vehicle platooning and the availability of cooling air for trailing vehicles on two- and three-vehicle platoons. To measure the aerodynamic drag, scale models are mounted onto a LLNL designed splitter plate by means of a low-friction linear bearing and a load cell located within each model trailer. In addition to drag, pressure measurements are made with a pitot probe positioned at the center of each model radiator grill. Particle Image Velocimetry (PIV) and Infrared Thermography (IRT) measurements are used to map the three-dimensional velocity field and flow structures around the vehicles. Three different vehicle platoon configurations have been tested: two aligned vehicles with separation distances of 5′-320′ with and without trailer boattails; three aligned vehicles with 30′, 40′, and 50′ separation distances between first and second vehicles and 5′-220′ separation distances between the second and third vehicles without trailer boattails; two misaligned vehicles with separation distances of 30′, 50′, and 160′ with a misaligned percentage of 0-50% based on the trailer width with and without trailer boattails. Wind tunnel data is acquired for yaw angles ranging from −9° to 9° in 3° increments to account for crosswind effects. The cooling air supply to the trailing vehicle varies with vehicle spacing and becomes quite small and even negative for spacing less than 15′; however, at 120′ and larger separation distances it asymptotically approaches 70% of the lead vehicle air supply. For separation distances of 30′-50′, the aerodynamic benefit for the two-vehicle platoon ranges from 21% to 23% and 10% to 13% for vehicles with and without trailer boattails, respectively. Increasing the number of vehicles in the platoon increases the overall aerodynamic benefit and an additional benefit is achieved by adding boattails to the platoon vehicles.
Salari, KambizOrtega, Jason
High pressure fuel cell engine, namely high pressure fuel cell system for automobiles, is the core power plant of fuel cell vehicle. Among many categories of fuel cells, proton exchange membrane fuel cell (PEMFC) is the most widely used one for automotive applications, with the characteristic of high power density, fast response and moderate working conditions. The cathode oxygen supply in PEMFC is one of the most important factors which affects its output power and operational lifespan. Reasonable regulation of air supply process flow and pressure can effectively improve system’s performance and efficiency. In this paper, a mathematical model of the air supply system and a model of altitude and environmental pressure are established in MATLAB \ Simulink by mechanism modeling method. Then the modules of the air supply system are integrated to supply air to the 85 KW PEMFC stack model. According to the nonlinear optimal theory, the optimal steady-state condition of the system under different net power is found. Simulate the air supply system under different altitude from 0 m to 4000 m. With analyzing the simulation results, it can be concluded that high-voltage fuel cell engine maximum output net power will be reduced by about 6% with each 1000 meters rise of altitude in the condition of the altitude below 3000 meters. From 3000 to 4000 meters, it will be reduced by 11%. At the same time for high-pressure fuel cell engine in high altitude environment, to ensure that it has the same net output power and the best efficiency as low altitude areas, the speed, the opening of back pressure valve and current must be increased as appropriate.
Chen, FengxiangChen, XiaoyuChen, Xing
Several methods are nowadays used by OEM’s in order to determine engine friction through experiments to help them develop friction correlations to be used in 1D simulation models. Some of the friction measurement methods used are; Willans Line, Morse test, Teardown test and Indicated Method. Each of these methods have their own disadvantages, with some reliant on heavy assumptions. In this paper a friction measurement method is discussed which requires a conventional motoring dynamometer cell by which the engine can be motored at different speeds. The exhaust manifold of the motored 2 litre, 4 cylinder diesel engine was shorted to the intake manifold with an unrestrictive ‘shunt’ pipe which reroutes the exhausted air to the intake [1]. The shunt pipe was pressurized by an external source of compressed air to make up for blow-by losses. It is noted that the compressed air supply is thus a small fraction of what would be required if no recirculation is used. In fact a small compressor that supplied shop air to the laboratory was more than adequate. In this manner the engine could be loaded with peak in-cylinder pressures reaching those reached whilst firing, thus engine friction can be determined at any particular combination of engine speed and load. This method computes the rubbing friction mean effective pressure (RFMEP) from a subtraction of the brake mean effective pressure (BMEP) and indicated mean effective pressure (IMEP). Since in motoring both the IMEP and BMEP are comparable in magnitude to the FMEP, error propagation is kept to a minimum. Thermodynamic loss angle, cylinder to cylinder variability, cycle-to-cycle variability, setpoint stability and repeatability of measurements are presented for a 5 rpm by 4 MAP test matrix, 1100, 1400, 2000, 2500 and 3000 rpm and 1.0, 1.5, 2.0 and 2.5 bar MAP.
Caruana, CarlFarrugia, MarioSammut, Gilbert
Of late there has been a resurgence in studies investigating parameters that quantify combustion knock in both standardized platforms and modern spark-ignition engines. However, it is still unclear how metrics such as knock (octane) rating, knock onset, and knock intensity are related and how fuels behave according to these metrics across a range of conditions. As part of an ongoing study, the air supply system of a standard Cooperative Fuel Research (CFR) F1/F2 engine was modified to allow mild levels of intake air boosting while staying true to its intended purpose of being the standard device for American Society for Testing and Materials (ASTM)-specified knock rating or octane number tests. For instance, the carburation system and intake air heating manifold are not altered, but the engine was equipped with cylinder pressure transducers to enable both logging of the standard knockmeter readout and state-of-the-art indicated data. For this study, the engine was operated using primary reference fuel 90 (PRF90) at 600 rpm, first following the procedures of the ASTM D2699 research octane number test protocol in order to define the geometric compression ratio set point for standard knock number. Thereafter, compression ratio sweeps were conducted at intake temperatures ranging from 30 to 150°C and intake air boost extending from 0 to 0.3 bar above ambient. The resulting operating map provided a broad envelope of compressed in-cylinder conditions relevant to modern spark-ignition engines. Detailed analysis of the indicated data highlighted a poor correlation between established knock intensity metrics and the knockmeter reading, which is used to characterize a fuel’s octane number. It was further found that the auto-ignition characteristics of PRF90 could be perturbed by means of intake air boosting and heating without being captured by the knockmeter reading.
Rockstroh, TobyKolodziej, Christopher P.Jespersen, Mads C.Goldsborough, S. ScottWallner, Thomas
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