Browse Topic: Soils

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This SAE Standard establishes terminology and the content of commercial literature specifications for self-propelled crawler and wheeled material handlers, pedestal mounted material handlers and their equipment as defined in 3.1. Illustrations used here are not intended to include all existing commercial machines or to be exactly descriptive of any particular machine. They have been provided to describe the principles to be used in applying this document. (Material handlers share many design characteristics with hydraulic excavators and log loaders; primarily 360 degree continuous rotation of the upperstructure relative to the undercarriage or mounting. They differ in their operating application. Material handlers are used for the handling of scrap material and normally utilize grapples or magnets. Hydraulic excavators are used for the excavation of earth, gravel and other loose material utilizing a bucket. Log loaders are used for the handling of logs and trees and normally utilize grapples.)
MTC1, Earthmoving Machinery
Experimental Investigation of the Droplet Field of a Rotating Vehicle Tyre2019-01-50686/18/2019
The consideration of vehicle soiling in the development process becomes ever more important because of the increasing customer demands on current vehicles and the increased use of camera and sensor systems due to autonomous driving. In the process of self-soiling, a soil-water mixture is whirled up by the rotation of the car’s own wheels and deposits on the vehicle surface. The validation of the soiling characteristics in vehicle development usually takes place in an experimental manner, but is increasingly supported by numerical simulations. The droplet field at the tyre has been investigated several times in the past. However, there are no published information regarding the physical background of the droplet formation process and the absolute droplet sizes considering the position at the tyre and the behaviour at different velocities. In the numerical self-soiling simulations, this droplet whirl up process is modelled by a non-rotating wheel, where equally sized droplets are injected tangentially from homogenous emitter lines on the tyre surface into the airfield. The impact of the simplifications of this approach on the final result of a self-soiling simulation has not yet been investigated. To achieve a more realistic droplet field, a new approach for the direct simulation of the droplet whirl up process is proposed by the authors in a previous publication. In order to have a validation basis for the new simulation method and to get a deeper understanding of the droplet formation process, experiments with a detailed analysis of the droplet field have been performed. This study presents the results of experimental investigations of the resulting droplet field for a single rotating tyre in a wind tunnel. The droplet field is exposed by a laser plane and is evaluated with respect to the droplet size and droplet velocity for two different tread designs and tyre speeds.
Strohbücker, VeithNiesner, ReinholdSchramm, DomenikKuthada, TimoJoos, Franz
Simulation Optimization of the NASA Mars Fuel In-Situ Resource Utilization and Its Infrastructure2018-01-196310/30/2018
The National Aeronautics and Space Administration’s (NASA) current objectives include expanding space exploration and planning a manned expedition to Mars. In order to meet the latter objective, it is imperative that humans generate their own products by harnessing space resources, a process referred to as In-Situ Resource Utilization (ISRU). ISRU will enable NASA to reduce both payload mass and mission cost by reducing the number of consumables required to be launched from Earth. The discrete-event simulation discussed focuses primarily on one ISRU system, the production of fuel for a return trip to Earth by utilizing Mar’s atmosphere and regolith. This ISRU system primarily uses autonomous rovers for exploration, excavation, processing of Mar’s regolith to produce fuel, and disposal of the processed regolith. This study explores individual rover and component requirements including rover speeds, travel distances, functional periods, charging, and maintenance times. The interactions of these individual components are highly interdependent and was evaluated to determine how they affect the overall ISRU system behavior, other components, and system requirements. By creating a simulation, the requirements and viability of the fuel ISRU system is now able to be evaluated and analyzed as a basis for planning and designing strategies. This study then aims to optimize uptime and number of different rovers required to reduce mission cost while still meeting fuel requirements. In addition, special efforts were given to improve visuals and animations to represent the process and to better communicate the Mars fuel ISRU requirements to a variety of audiences.
Vezina, AshleyCoutts, LindseyCohen, EmilyBurns, David
A Discrete-Event Simulation of the NASA Fuel Production Plant on Mars2017-01-20179/19/2017
The National Aeronautics and Space Administration (NASA) is preparing for a manned mission to Mars to test the sustainment of civilization on the planet Mars. This research explores the requirements and feasibility of autonomously producing fuel on Mars for a return trip back to Earth. As a part of NASA’s initiative for a manned trip to Mars, our team’s work creates and analyzes the allocation of resources necessary in deploying a fuel station on this foreign soil. Previous research has addressed concerns with a number individual components of this mission such as power required for fuel station and tools; however, the interactions between these components and the effects they would have on the overall requirements for the fuel station are still unknown to NASA. By creating a baseline discrete-event simulation model in a simulation software environment, the research team has been able to simulate the fuel production process on Mars. This research will mainly utilize the fuel component processing times, travel requirements, and In Situation Resource Utilization concepts to reach the end goal of producing enough fuel to safely get the astronauts home. This simulation displays the inner-working of each subcomponent and the effects that they have on the behavior of the overall system. The validation and verification of the fuel station simulation model includes reviewing historic models, NASA subject matter fuel experts, and a concurrent model. The results, which have been sought out for decades but technology and knowledge were limiting, will provide representative metrics and analysis of environmental effects and interaction of resources to create and maintain fuel on the red planet. This simulation model is the just the starting point of the planning and design strategies.
Ninah, CatherineStrevens, BrianBarcia, ColeLabbe, IsabelleFrenna, MichaelFaulconer, AustinHabbaba, KeonLoundy, KatherineSchaefer, LouisFrost, AlexaForan, AndrewBrown, RobertRabelo, Luis
Sand Dune Impact Simulation2017-01-13183/28/2017
Robustness to sand dune impact is one of the key requirements for Jaguar Land Rover products. Historically off road vehicles were built on a ladder sub frame; and the steel cross beam at the front provided robust protection for the cooling pack. With the move to monocoque construction, the cooling pack became vulnerable to low speed grounding damage. Unfortunately this vulnerability is not confirmed until later in the program when fully representative vehicles are available, which results in late engineering changes that are expensive, time consuming and stressful. Like all late changes it is rarely optimised for cost and weight. With no historic literature or procedure available, the challenge was to model the physics of sand media and also solve the complex multi-physics problem of impact of the whole vehicle with the sand dune. This paper discusses various challenges faced while developing a state-of-the-art modelling method for sand media and a full vehicle impact with the sand dune. Our first challenge in modelling sand was to get accurate material properties for which rigorous testing was done in the lab. We also benchmarked various methods in structural dynamics CAE tool LS-Dyna including Arbitrary Lagrangian Eulerian (ALE), Discrete Element Solid (DES), Solid Finite Element Method (Solid FEM), and Smoothed Particle Hydrodynamics (SPH). This paper further discusses the merits of these methods and the best method to solve the complex multi-physics problem of a full vehicle impact with the sand dune.
Khapane, PrashantBhosale, Suresh
Development of Aluminium Hollow Subframe Using High-Pressure Die Casting2016-01-04064/5/2016
High-tensile steel plates and lightweight aluminum are being employed as materials in order to achieve weight savings in automotive subframe. Closed-section structures are also in general use today in order to efficiently increase parts stiffness in comparison to open sections. Aluminum hollow-cast subframe have also been brought into practical use. Hollow-cast subframe are manufactured using sand cores in gravity die casting (GDC) or low-pressure die casting (LPDC) processes. Using these manufacturing methods, it is difficult to reduce product thickness, and the limitations of the methods therefore make the achievement of weight reductions a challenge. The research discussed in this paper developed a lightweight, hollow subframe technology employing high-pressure die casting (HPDC), a method well-suited to reducing wall thickness, as the manufacturing method. Hollow-casting using HPDC was developed as a method of forming water jackets for water-cooled automotive engines. Because the volume of the sand cores used in the method is low despite the complexity of their shape, the hollow-casting of large parts such as subframe necessitated the molding of larger sand cores than are conventionally employed. In addition, it was necessary to develop a sand core baking technology that produced a good strength balance, making it possible for the cores to resist casting pressures but collapse easily in the sand removal process following casting. A sand core technology balancing pressure resistance with collapsibility, which had previously represented an issue, was developed in order to make it possible to hollow-cast large parts, and a non-heat-treated Al-Mg-Si alloy was employed in order to reduce costs. The developed hollow aluminum subframe is approximately 40% lighter than a conventional subframe manufactured from welded steel plates (Fig. 1).
Asami, AkihikoImanishi, TomoyukiOkazaki, YukioOno, TomohiroTetsuka, Kenichi
Planetary regolith (dust) is an aggregation of various minerals and different particle sizes. Collection, storage, processing, and disposal of this material are very challenging in the harsh planetary environment. Extraterrestrial operations involving In-Situ Resource Utilization (ISRU) require conveying of regolith. The regolith needs to be transported from the planetary surface to chemical/thermal reaction vessels, and spent (processed) regolith needs to be conveyed to a disposal area.
Influence of the Automotive Brake Wear Debris on the Environment - A Review of Recent Research2015-01-26639/27/2015
Automotive brake linings are complex composite materials. Some raw materials used by manufacturers or the compounds created during the friction process might be potentially hazardous and may cause various adverse effects. Different fractions of the brake wear debris can be released during braking: i) the airborne and ii) the nonairborne. Due to the small size and minimum gravitational action, the airborne particles could be spread for long distances from a source and typically remain suspended in the air for long periods of time. Our previous research demonstrated that the airborne fraction contains considerable amounts of different nanoparticulates. On the other hand, the emitted nonairborne fraction typically settles on vehicle/brake hardware surfaces and in the vicinity of roads. The nonairborne particles are considered to be relatively large, but it was shown that nano-sized particles readily attach to them and can be released later. This study is focused on the recent research in the field of brake wear debris detection in the environment (road dust, soil and sediments, water runoffs, air pollution) as well as on the possible impact on plants, animals and human health. The review of recently published papers allowed for the summary of the spectrum of relevant experimental techniques used currently for identification and analysis of brake wear debris, and for the most recent opinions on their impact on the environment and health. It is suggested that consideration of the environmental aspects becomes the necessary aspect of brake/friction materials design.
Peikertova, PavlinaFilip, Peter
A method was developed for transfer of lunar soil into and out of process equipment. The Lunar Materials Handling System (LMHS) conveys solids to a process vessel, provides a gas-tight seal, prevents seal contamination, and minimizes wear from abrasive particles. The LMHS increases equipment life and minimizes process losses, thereby increasing overall in-situ resource utilization (ISRU) leverage. The LMHS is based on a seal arrangement by which lunar or Mars regolith can be repeatedly introduced into, and removed from, reaction chambers operating under a wide range of conditions. An integrated LMHS was demonstrated during operation in a one-cubic-meter vacuum chamber using hydrogen reduction as an ISRU process demonstration platform.
The interaction between the solar wind and the Earth’s magneto - sphere results in “space weather.” To determine the true nature of the solar wind-magnetosphere interaction, scientists require global measurements of processes occurring at the bow shock, in the magnetosheath, and at the magnetopause. Such observations can only be obtained from imaging this interaction globally. This will produce a paradigm shift similar to how satellite imaging revolutionized terrestrial weather forecasting.
This technology was developed for the Soil Moisture Active Passive (SMAP) mission and for the IRAD-FY13 Technology for Radiometer RFI Noise Detection & Mitigation Based on HHT2. Spacecraft beyond the present state-of-the-art passive radiometry will make use of natural thermal emissions to remotely sense Earth phenomena of interest to science (soil moisture, for example) in the technologically challenging microwave L-band. In this 1.4-GHz band (used by SMAP), a terrestrial source thermal signal emission to space suffers less attenuation by the intervening atmosphere. Unfortunately, the relative insensitivity of the L-band region to atmospheric effects also makes it an extremely attractive spectral range for wireless communications and radars that are causing radio frequency interference (RFI) with the spaceflight science radiometer instruments’ terrestrial phenomenon signal of interest, even as this band is protected by radio-communication regulations. Detection and excision or mitigation of the RFI-contaminated measurements is a challenge to the state of the art.
Manufacturing Technology for Hollow Structure Large Aluminum Parts Production by High Pressure Die Casting (HPDC)2015-01-13194/14/2015
When using aluminum for vehicle body parts to reduce weight, the high pressure die casting (HPDC) is widely applied due to its adaptability to thin-wall products, near-net-shape castability, and short casting cycle time. Since a hollow construction is advantageous to increase stiffness of body parts, there has been a need of development of techniques for casting of hollow parts by HPDC. So far, hollow casting by HPDC has been realized for small parts using sand cores. When applying that method to large parts, however, it is necessary to increase filling speed. When the filling speed is increased, the core tends to break. In this project, we have developed a method to estimate changes of pressure distribution when filling molten metal by the casting simulation in order to analyze damages to the core. Through the analysis, we discovered occurrence of impulsive pressure waves. Furthermore, the impulsive changes of molten metal pressure have been confirmed through the precise measurement of molten metal pressure. On the basis of the aforementioned findings, we have established a method to prevent core damage by controlling impulsive pressure waves by modifying the flow path. With the newly-developed method applied, the filling speed is increased by 1.5 times more than that of the conventional casting method for small parts, thus realizing casting of large hollow parts by HPDC.
Koya, EitaroFukuda, YukihideKitagawa, ShinyaMurakami, MitsunoriKawauchi, AtsushiFurue, Sadanori
The in situ production of vital gases and raw materials on the lunar surface is an integral part of NASA’s exploration vision. Development of processes for extraction of oxygen and metallics from the lunar regolith will be vital not only for life support on the lunar surface, but also for spacecraft propulsion to travel further beyond low Earth orbit. This will have a direct impact on cost reduction associated with minimizing the raw material mass from Earth. Aside from utilization of in situ resources, one of the significant limitations of current simulant is the lack of constituents, such as agglutinates. These agglutinates are typically mineral fragments of the lunar regolith that are held together by glass and, depending on location, may constitute 60% to 70% of the lunar regolith.
A fast Fourier transform (FFT) was developed as part of the Soil-Moisture Active/Passive (SMAP) project. The FFT was created on 16-bit data arriving at a rate of 48 MHz to run on a resource-constrained, space-grade field programmable gate array (FPGA).
There is a need to develop an efficient method for processing lunar regolith in support of future missions to colonize the Moon. A system for heating lunar regolith (“moon soil”) using microwaves for processing has been developed. It relies on an enhanced heating effect based on a large temperature gradient forming when a sample of lunar regolith under microwave radiation emits heat from its surface rapidly as the core is melting. Once the core melts, the sample absorbs microwave energy more readily. This molten lunar regolith would then exit the sample tube, and the lunar regolith could then be introduced into molds for forming a desired structure or building block.
Development of Lens Condition Diagnosis for Lane Departure Warning by Using Outside Camera2014-01-01674/1/2014
Driver safety continues to be improved by advances in active safety technologies. One important example is Lane Departure Warning (LDW). European regulators soon will require LDW in big cars to reduce traffic accidents and New Car Assessment Programs in various countries will include LDW in a few years. Our focus is on rear cameras as sensing devices to recognize lane markers. Rear cameras are the most prevalent cameras for outside monitoring, and new Kids and Cars legislation will make them obligatory in the United States from 2014. As an affordable sensing system, we envision a rear camera which will function both as a rear-view monitoring device for drivers and as an LDW sensing device. However, there is a great difficulty involved in using the rear camera: water-droplets and dirt are directly attached to the lens surface, creating bad lens condition. The purpose of this study is to improve the durability of lane recognition systems when water-droplets and dirt are deposited on the lens surface. First, we developed various diagnostic logics under various lens conditions. We then analyzed the results of various diagnosis and expressed the lens conditions by using two evaluation axes. After that, we improve the durability of the lane recognition system including a judgment function that determines whether to stop the LDW system under heavy dirt and water-droplets. We conducted driving tests and captured evaluation movies in the United States, Europe, and Japan. We evaluated the lane recognition rate for a total of 8 hours of evaluation movies under various weather conditions. We achieved a lane recognition rate of 95% and improved the durability of the lane recognition system.
Takemura, MasayukiImai, MasatoKiyohara, MasahiroIrie, KotaSakata, MasaoMuramatsu, Shoji
Miniaturization in microelectronics is beginning to reach its physical limits, say researchers at the Helmholtz-Zentrum Dresden-Rossendorf Institute of Ion Beam Physics and Materials Research, who are seeking new methods for device fabrication.
Until the time of this reporting, when a space vehicle required a reference signal for inertial pointing, the choices were a signal beacon from an Earth location, the Earth radiance in the visible spectrum, or a star tracker. However, limitations can arise from using these techniques. For example, the signal beacon suffers from limited signal power (either in RF or optical) and will constrain the application to limited ranges, errors due to stray-light and centroiding limit the accuracy of a star tracker, and the spatial/temporal variability of the Earth’s albedo and its illumination by the Sun introduces limitations when used in the visible or near infrared light.
The water-vapor continuum absorption plays an important role in the radiative balance in the Earth’s atmosphere. It has been experimentally shown that for ambient atmospheric conditions, the continuum absorption scales quadratically with the H2O number density and has a strong, negative temperature dependence (T dependence). Over the years, there have been three different theoretical mechanisms postulated: far-wings of allowed transition lines, water dimers, and collision-induced absorption. The first mechanism proposed was the accumulation of absorptions from the farwings of the strong allowed transition lines. Later, absorption by water dimers was proposed, and this mechanism provides a qualitative explanation for the continuum characters mentioned above. Despite the improvements in experimental data, at present there is no consensus on which mechanism is primarily responsible for the continuum absorption.
Development of Rare Earth-saving Magnet Using Localized Diffusion Method2013-01-17574/8/2013
Nd₂Fe₁₄B sintered magnets are used in the drive motors of hybrid, electric and other vehicles. A magnet in which rare earth content is reduced by means of a localized diffusion method has been developed in order to reduce the volume of dysprosium. The distribution of the demagnetization fields in a motor is not uniform, so the necessary coercivity distribution for the magnets was quantified using Computer-Aided Engineering (CAE). Then material specifications of the localized dysprosium diffusion satisfied with this coercivity distribution was determined, and optimal manufacturing conditions including the position of dysprosium diffusion were set. The coercivity distribution in every position of the magnet using localized diffusion method was inspected. As a result, the magnet was satisfied with coercivity distribution demanded by CAE. Furthermore, evaluation of motor characteristics, especially the demagnetizing characteristic concerned with dysprosium reduction, showed this developed magnet to possess identical characteristics to a conventional magnet. Dysprosium resources represent a particular issue among the rare earths more generally, and the technology developed in this project is able to reduce dysprosium use in magnets by approximately 30% without compromising motor performance.
Higashi, TakayukiMiyoshi, TakehiroKato, RyutaroKono, MichihisaInoue, MasashiNagumo, ToshiyukiFukui, TakahiroOhsaki, KojiroIwasaki, Makoto
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