Browse Topic: Air supply

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This slash document collects general reference material related to gaseous oxygen system flow requirements and sizing calculations. This document will assist oxygen system equipment designers and operators to establish systems and equipment requirements. The document consists of charts, tables, system schematics, system requirements, and sample calculations for system sizing.
A-10 Aircraft Oxygen Equipment 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
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
Analysis of Defogging Pattern on Windshield and Ventilation Load Reduction based on Humidity Distribution Control2016-01-02564/5/2016
In the winter, windshield glass fogging must be prevented through the intake of outdoor air into a vehicle. However, the corresponding energy loss via the ventilation system cannot be ignored. In the present study, the defogging pattern on the windshield is evaluated and the water vapor transportation in the flow field in the vehicle is analyzed in order to investigate the ventilation load by means of a numerical simulation. Some examined cases involve new outlet positions. Additionally, a new, energy-saving air supply method for defogging, with so-called “double-layer ventilator”, is proposed. In this method, one air jet layer is obtained via a conventional defogging opening in the vicinity of the windshield, supplying an outdoor air intake. The other jet consists of recirculated air that covers the outdoor air, preventing it from mixing with the surrounding air. The calculation results indicate that the exhaust opening location, from which the internal vehicle air is obtained for recirculation, affects the cabin flow field, the windshield fogging pattern and the ventilation load. The water vapor generated from human occupants did not spread well and that is why there was the humidity gradient in the vehicle. This means that the flow field must be considered in order to achieve efficient defogging, that is done by emitting the water vapor immediately. The double-layer method exhibits the same level of defogging performance as single-layer techniques, even with half the airflow velocity. The energy load can be reduced by approximately 5 % using the appropriate conditions.
Nagano, HideakiTomita, KenjiTanoue, YasuhiroKobayashi, YujiKohri, ItsuheiKato, Shinsuke
Design and Optimisation of the Propulsion Control Strategy for a Pneumatic Hybrid City Bus2016-01-11754/5/2016
A control strategy has been designed for a city bus equipped with a pneumatic hybrid propulsion system. The control system design is based on the precise management of energy flows during both energy storage and regeneration. Energy recovered from the braking process is stored in the form of compressed air that is redeployed for engine start and to supplement the engine air supply during vehicle acceleration. Operation modes are changed dynamically and the energy distribution is controlled to realize three principal functions: Stop-Start, Boost and Regenerative Braking. A forward facing simulation model facilitates an analysis of the vehicle dynamic performance, engine transient response, fuel economy and energy usage. To identify respectively (1) the maximum overall fuel economy, (2) the maximum amount of air and energy recovered during the braking and (3) the minimum loss of available energy during acceleration, a number of variables in the control strategy are selected in an optimisation process. Three optimisation algorithms are compared in different aspects of the control strategy: (1) using the Pattern Search to optimise the initial air tank pressure for every stop-start event in order to maximize the pressure increment in the air tanks; (2) conducting the Genetic Algorithm optimisation to find out the best gear change strategy during braking in order to maximize the energy recovery to the air tanks; and (3) implementing the multiobjective optimisation to simultaneously minimize the fuel consumption and the loss of available energy in the air flow during acceleration. The rationale for the choice of optimisation methods is explained and recommendations made for the development of energy management strategies in which a variety of different vehicle functions contribute to an overall fuel economy benefit.
Bao, RanStobart, Richard
The Station Spacewalk game enables players to virtually conduct NASA repair work on the International Space Station, including jobs critical to help power up the space station so it can continue to operate. Players are provided with a limited quantity of oxygen during which they must complete extravehicular activities (EVAs) and return to the airlock before the air supply runs out.
Development and Evaluation of a Multi-Functional Steering Wheel Switch2005-01-04244/11/2005
In this paper we propose a new multi-functional steering wheel switch for HVAC and audio systems. This new switch has five buttons on the front side of the spoke area and one button with vibration on the backside of it. Drivers can operate either HVAC or audio functions with the front switches, and HVAC or audio mode can be alternatively selected by pressing the back switch. Since different vibration modes are assigned for the HVAC and audio mode, drivers can also easily recognize which function can be operated. By changing the assignment of the mode in this way, the switch can operate more than 10 functions with 6 buttons allocated on the spoke area. Several kinds of evaluations were performed in order to develop this multi-functional switch. At first, to optimize the positions of the buttons, the behaviors of thumbs and fingers were measured. Also the physical workload of the thumb motion and middle fingers' postures was evaluated when subjects operated the switches. Secondly, tactile sensibility of humans was investigated, and sensory evaluations concerned with vibration sensitivity were performed to decide the specification of the vibration. Thirdly, functions for operating the HVAC and audio systems with this switch were selected by considering driving situations. Finally, the switch that was developed based on the results of these evaluations was re-evaluated by using a driving simulator to verify the operability of the switch. As a result of this evaluation, it was shown that the new switch with the functions for both the HVAC and audio systems performs well compared to the conventional switches.
Kamiya, NaokiTakeuchi, ShuichiShinzato, TakashiSuzuki, Takashi
Method for Analyzing Lubricating Oil Contamination of Aircraft Systems2002-01-294211/5/2002
Cabin air quality is of continuing importance [1]. Contamination of air with particulates or vapors has the potential of affecting the health of passengers and flight crew. Therefore, measures are required to maintain acceptable levels of cabin air quality. One potential source of cabin air contamination is lubricating oils used in the engines. Type II oils are required for the main engines, but Type I or Type II oils can be used for the APU, with Type I recommended by some engine manufacturers for its cold-start properties. Southwest Research Institutes (SwRI®) Department of Emissions Research used an internally developed analytical method called Direct Filter Injection/Gas Chromatograph (DFI/GC™) to analyze for volatile fractions of lubricating oil contaminants on Environmental Control System (ECS) components. Samples of two standard Type II aviation turbine lubricating oils were analyzed with the DFI/GC™ method and their spectra examined. Sufficient differences were observed to clearly identify the oils. A sample of accumulated contaminant taken from a part of a failed ECS pack was analyzed and clearly identified as one of the two lubricating oils. An aircraft was set up with one oil in the main jet engines and the other oil in the Auxiliary Power Unit. When a problem occurred with the ECS pack, samples of deposits were analyzed from ECS pack components, and the lubricating oil contaminant source was clearly identified. Therefore, the DFI/GC method was shown to be very useful in identifying the source of oil contamination on ECS pack components. It is believed that the technique has similar usefulness in investigating oil contamination of a variety of aircraft components.
Bartley, Gordon J. J.Anderson, Andy M.Jones, Kenneth B.
AE-1 Engine Accessory Installations Committee
An Automotive Hybrid Heating System for Parallel Hybrid Passenger Cars2000-01-12763/6/2000
The advancements in hybrid and electric vehicles require an optimal utilization of the on-board energy sources to increase vehicle fuel economy, provide a safe and comfortable driving environment, and extend heating and cooling capacity range. Recently, the application of parallel propulsion technology to design and build hybrid vehicles has caused new concerns on climate control engineering. This study is the first to address the challenges on developing an innovative heating system for parallel hybrid vehicle applications. This paper presents a hybrid heating system for a parallel hybrid passenger car, in which a conventional coolant heater core loop and a heat pump loop are installed to meet the needs of cabin heating. Thermodynamic characteristics of various subsystems are discussed with respect to the variations of ambient temperature through the experimental and analytical comparisons. Furthermore, thermodynamic analysis is applied to evaluate the design and operating effectiveness of the hybrid heating system. To synthesize the operation of the heating system, a hybrid heating concept is proposed and applied to direct the optimal integration and identify the dynamic operating modes through a hypothetical drive simulation. The work reported in this paper is aimed at laying a theoretical and applied foundation to the development of automotive hybrid heating systems.
Zeng, X.Major, G. A.Hirao, T.Imaiida, T.
This SAE Aerospace Information Report (AIR) presents safety criteria for pneumatic type engine starting system design and component hardware. Included are safety criteria in design of both starter control valves and starters as well as in design of airframe control systems. Safety topics concern starter valve operation and material application, airframe controls and instrumentation installations and starter rotor integrity and containment.
AE-6 Starting Systems and Auxiliary Power Committee
Thermal and Environmental Control of the Crew Transport Vehicle9723147/1/1997
Following the objectives of the European Space Agency, specific studies have been performed concerning a Crew Transport Vehicle (CTV) based on the Ariane 5 launcher. This vehicle is designed to transport a maximum crew of 4 members to/from the International Space Station, with a limited amount of payloads. It is mainly composed of: Crew Module (CM), capable of withstanding the severe environmental conditions of the atmospheric re-entry, offering an adequate habitable environment for the crew all mission time long. Resource Module (RM), where most of provisions and electrical equipment (e.g. batteries) supporting the vehicle orbital life is stored; the truncated cone shape external surface of RM is entirely exploited for mounting dedicated fluid radiators. Transfer Vehicle (TV), a propulsion module designed to supply means and resources for the vehicle orbital manoeuvres and attitude control from launcher separation up to de-orbitation, when the RM + TV composite is jettisoned. The thermal control of the CTV requires the adoption of technical solutions compatible with extremely different environmental conditions (ranging from the cold boundaries of orbital exposure to the high aerothermal fluxes during re-entry) and various operational modes (the vehicle is fully active in free-flying phases, but it is in dormant mode when ISSA docked, with most of equipment switched off). Temperature and humidity in the habitable compartment are controlled by a dedicated section of the Environmental Control and Life Support Subsystem. An air loop is designed to collect the cabin heat loads due to crew metabolism, external environment and part of the spacionics dissipation. These loads are then transferred via a Condensing Heat Exchanger to a couple of hot redundant water loops (Active Section of Thermal Control Subsystem) which also receive the thermal power released by the electronic equipment mounted on cold plates. The resulting global heat loads are transported to the available heat sinks, which may be different depending on the various mission phases. During ascent and re-entry, waste heat dissipated by means of evaporators and / or managed through the vehicle thermal capacitance. In orbital conditions a set of radiators, connected to a low freezing temperature coolant loop, provides the necessary rejection to space. Passive thermal control provisions are complementarily adopted, including Multilayer insulation, foam blankets and heaters. The major design features of the CTV Thermal Control are highlighted, taking into account the interface subsystems (e.g. Electrical Power Supply, DMS / GNC, Thermal Protection), the mission timeline, and the constraints related to the failure tolerance criteria adopted.
Bottacini, M.Fenoglio, F.Ferro, C.Loddoni, G.
A New Model for Fuel Supply Dynamics in an SI Engine9402083/1/1994
In this paper we introduce an improved model for the fuel supply dynamics in an SI engine. First, we briefly investigate all the thermodynamic phenomena which are assumed to have a significant impact on fuel flow into the cylinder (i.e., fuel atomization, droplet decay, wall-wetting, film evaporation, and mixture flow back). This theoretical analysis results in a basic set of dynamic equations. Unfortunately, these equations are not convenient to use for control purposes. Therefore, we proceed to a simplified formulation. Several unknown parameters remain, describing phenomena which are difficult to quantify, such as heat and material transfer characteristics. These parameters are subject to operating conditions and are not discussed further. In order to validate the model dynamics, we refer to frequency and step response measurements performed on a 4-cylinder, 1.8 liter BMW engine with sequential fuel injection. From the frequency response measurements we first extract the time constants of the oxygen sensor used throughout the experiments. Provided with these parameters we investigate the transient behavior of the model due to both steps in air and in fuel supply. In order to vary fuel supply we control injection time, whereas air supply variations are generated by controlling the throttle set point. For this purpose, the amount of air residing in the cylinder is calculated according to intake manifold pressure, thereby eliminating intake manifold dynamics. We verify that the model proposed is sufficient to describe most of the dynamic phenomena in fuel supply.
Turin, Raymond C.Casartelli, Ernesto G. B.Geering, Hans P.
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