Browse Topic: Recycling

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ABSTRACT The complexity of ground vehicle mission systems has evolved significantly over the last few years resulting in over-taxed platforms with federated mission suites. Department of Defense (DoD) is pursuing platform evolution toward integrated mission suites. Opportunities exist to apply aspects of previously developed methodologies from the aviation sector to ground platforms. This paper describes the parallels of the evolution of aviation platforms with the similarities to ground platforms. Solutions from the military aviation community will be discussed that could reduce development risks, schedules and costs and improve mission capabilities for ground applications. Specific discussion will be on opportunities and techniques to transition performance driven, high cost, low volume technologies into mission suitable and affordable high volume solutions. Discussion of the feedback opportunities into the aviation community will be addressed. This paper is not intended to be a tutorial on systems engineering but rather a stimulus for industry and the DoD to discuss commonality and design reuse opportunities between the ground and aviation communities resulting in a “system of systems” bridging aviation and ground solutions.
Hensley, Marion P.
Deos includes an industry standard lightweight TCP/IP stack (LwIP) with a DAL-A sockets library so it can provide data transport during in flight or on ground as part of its standard package. While it may have high data integrity (e.g., through CRC or other such mechanisms), TCP/IP over Ethernet is a non-deterministic protocol. As such, it is not suitable for avionics applications that require determinism or high robustness. In contrast, there are several are several redundant and deterministic data network technologies such as ARINC-664/AFDX, time triggered ethernet (TTE), and time sensitive networking (TSN). These interfaces are based on switched Ethernet technologies and can include system redundancy such that they are applicable for aircraft data network applications. Their feature set enables them to be used as a digital backbone for aircraft control and other applications where both integrity and availability are essential. Each of these solutions generally requires specific end point hardware to implement the protocols in firmware in order to meet the required communication timing and throughput. The implementation of the software device drivers for these technologies on Deos can leverage Deos' I/O Infrastructure (IOI) data distribution service for data decoupling. IOI is a DO-178 DAL-A module that can distribute data based on XML configuration files that specify the data paths, access control and optionally data formatting. It implements an inter-partition communications data interface between avionics applications including ARINC-653 partitions using the ARINC-653 APEX API sampling/queueing ports. Together, these features allow developers to readily adapt to changes in communication structures all through XML configuration files, versus recompiling which would impact the verification evidence of the module. This paper will talk about the different networking standards and how the use of Deos' IOI provides a way for the system to easily adapt to different network configurations without causing the driver library or end application(s) to be modified and thereby minimize change impact for reuse/reverification.
Gilliland, Gary
The purpose of this SAE Standard is to establish the specific minimum equipment requirements for recovery/recycling/recharge equipment intended for use with both R-1234yf and R-134a in a common refrigerant circuit that has been directly removed from, and is intended for reuse in, mobile air-conditioning (A/C) systems. This document does not apply to equipment used for R-1234yf and R-134a having a common enclosure with separate circuits for each refrigerant, although some amount of separate circuitry for each refrigerant could be used.
Interior Climate Control Service Committee
Collins Aerospace recognizes the value the warfighter gets from reducing the Size, Weight and Power (SWAP) of the avionics systems. The war fighter also sees benefit from reuse of existing avionics and mission software modules, which frequently vary in software framework and thus are allocated to separate processors. A solution, as seen in the commercial IT industry would be the use of multi-core processing and hypervisors allowing the mixing of frameworks providing rapid integration with minimal SWAP. In avionics we must additionally provide assurance. This paper will explore our application of the FACE™ Technical Standard (Ref. [1]) to obtain framework variability, used in conjunction with a hypervisor to allow the resulting frameworks to exist in a single multi-core processing environment with safety assurance to the solution. The concept proposed was validated through demonstration of US Army and Collins software running on the same multi-core processor.
Myren, JasonGroen, Mitch
The purpose of this SAE Standard is to establish the specific minimum equipment performance requirements for recovery and recycling of HFC-134a that has been directly removed from, and is intended for reuse in, mobile air-conditioning (A/C) systems. It also is intended to establish requirements for equipment used to recharge HFC-134a to an accuracy level that meets Section 9 of this document and SAE J2099. The requirements apply to the following types of service equipment and their specific applications. a Recovery/recycling equipment b Recovery/recycling-refrigerant charging c Refrigerant recharging equipment only
Interior Climate Control Service Committee
Spray Parameters of Fuel Blends of Recycled Lubricating Oil and Diesel2018-01-16939/10/2018
The use of alternative fuels consisting of mineral and synthetic waste substances such as recycled lubricating oil blended with diesel is a measure to mitigate the environmental impact of the fossil fuels. However, to inject these fuel blends into contemporary engines without changes to their components, it must maintain or improve the fuel injection characteristics compared to neat diesel, in order to maintain or improve the engine performance. In the present research, the spray parameters of injected fuel, such as length, angle and atomization particle diameter in terms of the Sauter mean diameter (SMD), are modeled depending on the characterization of different concentration of the recycled lubricating oil blended with diesel. It was found that the same nozzle geometry of the injectors can provide an equivalent fuel spray performance for different concentrations of these alternative fuel blends, and that the increase of the recycled lubricating oil in the fuel blend reduced the wear of the needle and nozzle of the injector. The densities and viscosities between each fuel type are very similar and any correction of injection duration or pressure is not required. Due to simple distillation and blending process, alternative and environmentally friendly fuel blends can be obtained to reduce the combustion of fossil diesel and reuse waste pollutant substances as a sustainable and immediately applicable solution for modern engines and fuel injection systems.
Gutierrez, MarcosCastillo, AndresIniguez, JuanReyes, Gorky
Recycling of the platinum of vehicle catalysts at end of life2018-36-01069/3/2018
Due to the large number of end of life vehicles in our country, our work is aimed at recycling a very important material present in all cars, which is the platinum found in automotive catalysts. Platinum is a rare metal and high value-added, recovery from secondary sources is crucial to ensure its supply for various applications in the market, especially in regions with scarce resources. For this reason, the recycling of platinum, particularly of automotive catalysts becomes very important for the market. The methodology to be applied along the development of the work approaches from the characterization of the catalyst (by technical analysis of microscopy), recycling of platinum (by hydro-metallurgical processes), finally the tests and analysis of the recycled platinum, through physical tests, chemicals. Through the platinum recycling process, it is expected that an economically feasible form has been determined as well as the process method for platinum recycling, in addition to achieving a sample of recycled platinum with physical and chemical characteristics that provide for its reuse. However, the process of recycling platinum comes as an ecological alternative for the extraction, and through this research they propose a recycling method to return it to the market, suppressing its scarcity.
da Silva, Lucas Gonçalvesde Almeida, Rodolpho Faria DiasSilva Faustino, Vinícius MarinhoJúnior, Pedro Américo Almeida Magalhãe
ABSTRACT The goals of sustainable manufacturing, as articulated by Organization for Economic Co-operation and Development (OECD), are to reduce the intensity of material use, energy consumption, emissions and unwanted by-products - while maintaining or improving the value of products to society and to organizations. Benefits that can be achieved through this practice include improved working conditions, public image, staff morale, customer loyalty, brand value, profits, sales turnover, product performance, reduction in waste generation and staying ahead of regulatory concerns. Achieving such goals begins early in the product design phase with consideration toward materials used and processes invoked in manufacturing. Ultimately, a full sustainability assessment must include the product's End-of-life (EOL) impact, factoring environmental impacts of landfill and recycling emissions. This paper focuses on using an End-Of-Life impact assessment for a set of materials and processes commonly used in the aerospace industry. Available data and best practices are used to forecast the final EOL impact of an aerospace product for a given set of materials and processes. The approach is able to quantify costs incurred to advance manufacturing processes and can be used to inform top management on sustainability decisions. The approach could be extended to assess the complete aircraft, including its Beginning of Life.
Das, EmonK, Raldo
Laboratory Test Means Scalable to the Test2015-01-25469/15/2015
To perform a complete aircraft certification plan, civil aviation test centres use specific flight test installations and ground test means. In this scope tests specialists operate ground test means which have a generic name Laboratory Tests Means (LTM) to validate aircraft functions. Today these functions are becoming more and more complex, moreover certification deadlines and tests campaign costs are becoming increasingly challenging and demand LTM use optimization. In this context current LTM development approach is no longer suitable to cover these new constraints. Currently LTMs start to be designed when testing strategy for a new aircraft is defined and design is quite specific. Drawbacks of such an approach are: tunnel effect for LTM development, no simple sharing of testing resources, LTM reuse is not easy, LTM upgrade requires re-engineering and many LTMs have to be maintained even if only partially used. As a result future LTMs shall be scalable to the tests and tests shall not be dedicated to a specific LTM. A modular, distributed and open architecture based on standards will be an enabler to run tests in an efficient way. Agility in the testing process and LTM configuration will allow adjusting test means to the test procedure. LTM will become easily adaptable to A/C changes and testing strategy priorities. Tests can be run in parallel using only the required resources. Interconnection of distributed LTMs will improve testing capabilities and functionalities. Combined with remote and virtual testing capabilities the next generation of LTMs will become less a standalone device and more a network connected device. Shared by the design office, test centre and A/C suppliers, the LTM will also set more synergies between each stakeholder providing appropriate services, to complete the certification in an efficient and timely manner.
Delrieu, Sylvain
SW DONKI is a comprehensive Web application for space weather forecasters, scientists, and the general space weather community. It serves as an archive for space weather activities including solar flares, coronal mass ejections (CMEs), solar energetic particles, and geomagnetic storms. An innovative feature of the system is the ability to generate, modify, and store complex linkages between space weather events — creating a comprehensive network of relationships between activities, and identifying potential cause-and-effect paradigms for each space weather event. SW DONKI also provides public access to all human-generated event analysis and notifications produced by the Space Weather Research Center (SWRC) forecasting team at CCMC (Community Coordinated Modeling Center).
The Energy Management for Solar Powered Vehicle Parking Ventilation System2015-01-01494/14/2015
In summer, when vehicle parks in direct sunlight, the closed cabin temperature would rise sharply, which affects the occupants step-in-car comfort Solar powered vehicle parking ventilation system adopts the solar energy to drive the original ventilator. Thus, the cabin temperature could be dramatically decreased and the riding comfort could be also improved. This research analyzed the modified crew cabin thermal transfer model. Then the performance of the solar powered ventilation system is analyzed and optimized combined with the power supply characteristics of the photovoltaic element. The storage and reuse of the solar power is achieved on condition that the cabin temperature could be steadily controlled. The research shows that, the internal temperature is mainly affected by the solar radiation intensity and the environment temperature. Within the environmental conditions area where the environmental temperature is set from 30°C to 45°C and the solar radiation intensity is set from 200 W/m2 to 1000 W/m2, the ventilation system without the energy management can keep the temperature inside the car higher than the highest environmental temperature by 5 to 10 degrees under about 80% of the environmental conditions. Under the condition of reaching same effect on controlling internal temperature as above, the energy management system can distribute electrical energy reasonably, making the ventilation system adapt to more than 90% of the environmental conditions. Under normal weather condition in the summer, the system works from 7 am to 5 pm, while the internal temperature is well controlled, it collects electrical energy of around 0.02KW·h. The system can collect electrical energy of about 0.1KW·h after the car with the system has driven for 2 hours under the condition that the sun radiation intensity is about 900W/m2. The saving electrical energy can effectively guarantee the system to adapt to changing environmental conditions.
Wang, CanTan, GangfengGuo, XuexunTian, ZhewenTian, ZhanweiLi, Jiafan
A Conceptual Framework for Value Chain Analysis of End of Life Aircraft Treatment in the Context of Sustainable Development2014-01-22329/16/2014
The End of Life phase of Aircraft is a relatively complex phase in life cycle of this product. The retired Aircrafts need to be parked in certain conditions. Some valuable parts are disassembled and the rest of them are dismantled. Materials are separated and upgraded, waste is burned or deserted and toxic materials restrained or incinerated. All of these activities should be performed in an ecologically right manner; however, collectively produced added values for all stakeholders need to be considered. This paper aims to provide a conceptual framework for value chain analysis of Aircraft recycling process in the context of sustainable development. The value chain related to recycling aircraft at the end of life was chosen to generate an in-depth analysis of the value chain, considering environmental and socio-economic concerns. The value chain framework for recycling of fleets is identified. The key processes with environmental and social impacts are determined. The decision making process along the value chain and the policy framework including codes, regulations and standards are addressed. Finally, the proposed approach with providing a basis for evaluation of effectiveness, efficiency and stability across the value chain aids decision makers to design a sustainable framework for End of Life aircrafts treatment.
Keivanpour, SamiraMascle, ChristianAit Kadi, Daoud
Aeronautical Passive Energy Recovery System based on LHP Technology Extended Test Results2014-01-21919/16/2014
As aviation enters the future, new technologies and philosophies are required to keep up with ever changing demands and increased market competition. Aircraft designers are required to come up with new and innovative ways to optimise systems and improve efficiencies. Onboard thermal management is an area that can take advantage of several new technologies to do just that. This paper is based on the development project “Advanced Thermal Management in Aeronautics” (ATMIA). Project ATMIA focuses on the use of Loop Heat Pipes (LHPs) in the aeronautical industry, specifically their onboard feasibility and the unique requirements found on an aeronautical platform such as those due to vibrations, gravitational forces and the need for disassembly due to maintenance. LHPs are passive two-phase devices that allow free-energy heat transportation between certain subsystems without needing additional power consumption. Their use in aeronautics is interesting as they can passively transport seemingly “waste” heat to areas where it can be reused. The use of LHPs onboard aircraft platforms can potentially reduce the amount of electrical power that must be extracted from the engines. This improved efficiency and when taken together with LHPs flexible design and low weight compared to traditional systems such as bleeding, directly affects fuel consumption. This can lead to a reduction in the amount of fuel used, an increased range, improved payload capacity and a reduction of CO2.
Donovan, MarkDel valle, Pedro
Development of High Efficiency and Compact Bumper Recycling Equipment2014-01-19734/1/2014
This paper describes the development of high efficiency and compact bumper recycling equipment for facilitating bumper recycling globally. Various equipment to remove paint coat from bumper has been developed since 90s', using mechanical, physical or chemical method. However, it is difficult to promote bumper recycling without realizing cost effective overall system from paint coat removal to pelletizing. Our company jointly developed method of mechanically removing paint coat and has committed to bumper recycling in the form of outsourcing since 2000. In 2010, a dedicated plant for recycling bumpers was launched on the premises of our Oppama Assembly Plant in Japan. In the future, promoting bumper recycling at other overseas assembly plants is necessary as vehicle production will expand globally. Having more compact and cost effective recycling system compared to the one at the Oppama plant is required since the scale of the system including bumper crushing, paint coat removal, and pelletizing has to match processing capacity at these plants rather than equipping large one like Oppama's. With this reason, the newly developed equipment includes renewed machines for bumper crushing, paint coat removal and pelletizing. The paint coat removal process was developed on the basis of an environmentally friendly mechanical technology that Nissan developed approximately ten years ago. This process makes use of differences in material property changes of the polypropylene base material, paint coat and primer that occur accompanying a temperature rise during the churning of crushed bumper fragments. Optimum temperature control in the churning vessel enabled the equipment to be downsized and to achieve highly efficient paint removal. The geometry of the extruder screw used in the pelletizing process was optimized along with optimizing the conditions for suppressing vent-up resin flow due to a pressure rise in the vessel. These improvements made possible more compact equipment than the existing bumper recycling system. The newly developed equipment combined with more simplified auxiliary units enabled the entire recycling process from bumper crushing through paint removal to pelletizing to be substantially downsized.
Mizutani, Atsushi
Experimental Investigations on a Diesel Engine Using Coconut Shell Pyro Oil (CSPO) - Diesel Blends as Fuel2014-01-13774/1/2014
This paper aims at investigating the performance, emission and combustion characteristics of a diesel engine fuelled with CSPO (coconut shell pyro oil)-diesel blends as fuel. In the first phase of work CSPO was produced from fast pyrolysis of raw coconut shell at a reaction temperature of 700°C. Attempts were made to obtain homogeneous mixtures of different amounts (such as 5%, 10%, 15% and 20% by volume) of CSPO with diesel. Beyond 15% separation of the fuel was observed. Hence it was decided to use the blends of 5%, 10% and 15% of CSPO with diesel as fuels. Experiments were carried out on a single cylinder, water cooled, direct injection diesel engine using different blends of CSPO with diesel as fuel. Performance, emission and combustion parameters were obtained at different power outputs for all the tested fuels and analyzed. Engine test results indicated reduced thermal efficiency, increased smoke density, unburned hydrocarbon and carbon monoxide emissions with the blends of CSPO as compared to conventional diesel fuel at all power outputs. The maximum thermal efficiency was found as 30.5% with diesel where as it was 29%, 27.5% and 26% for the CSPO blends of 5%, 10% and 15% respectively with diesel at the rated power output of 3.7 kW. Smoke emission was found as higher with all the blends of CSPO as compared to neat diesel at all power outputs. However, NO emission was reduced with all the blends. 15% CSPO showed the minimum NO emission at all power outputs. Combustion studies indicated increased ignition delay and combustion duration with all the blends as compared to neat diesel at all power outputs. The maximum ignition delay was found as 13°CA with the blend of 15% CSPO at peak power where as it was 10°CA with neat diesel. Cylinder pressure and maximum rate of pressure rise were observed as lower with all the blend of CSPO as compared to neat diesel operation. Among the blends tested the blend of 5% CSPO with diesel gave increase in smoke emission within 12.5%, unburned hydrocarbon within 5% and CO within 10% of diesel fuel. The reduction in thermal efficiency was within 5% of neat diesel fuel.
Masimalai, Senthil KumarVenkatesan, Kuppusamy
Challenges for Reuse in a Safety-Critical Context: A State-of-Practice Study2014-01-02184/1/2014
The need for cost efficient development and shorter time to market requires reuse of safety-critical embedded systems. One main challenge for reuse approaches in a safety-critical context is to provide evidence that assumptions of the safety artifacts for the reused component are still valid in the new system definition. This paper summarizes the major findings from an explorative study conducted in order to identify the state of practice of reuse in the context of different functional safety standards. The explorative study consists of a set of questions, which have been discussed with interviewees from companies of various domains. The companies act in safety-critical domains with diverse product portfolios. We covered several points of view by interviewing persons with different background. The results of the study reveal industrial challenges, which built the input for the derivation of possible future work based on the identified practical needs. Our main findings show the current predominance of ad-hoc reuse techniques and the need for more systematic approaches for reuse. We propose a systematic approach to cover the industrial challenges: establishing a safety culture in the company, an integrated system and safety development process, the introduction of model-based development for an improved support of reuse concepts, and metrics for impact analysis.
Martin, HelmutBaumgart, StephanLeitner, AndreaWatzenig, Daniel
Composing Tradeoff Studies under Uncertainty based on Parameterized Efficient Sets and Stochastic Dominance Principles2012-01-09134/16/2012
Tradeoff studies are a common part of engineering practice. Designers conduct tradeoff studies in order to improve their understanding of how various design considerations relate to one another and to make decisions. Generally a tradeoff study involves a systematic multi-criteria evaluation of various alternatives for a particular system or subsystem. After evaluating these alternatives, designers eliminate those that perform poorly under the given criteria and explore more carefully those that remain. One limitation of current practice is that designers cannot combine the results of preexisting tradeoff studies under uncertainty. For deterministic problems, designers can use the Pareto dominance criterion to eliminate inferior designs. Prior work also exists on composing tradeoff studies performed under certainty using an extension of this criterion, called parameterized Pareto dominance. The capability to compose preexisting tradeoff studies is advantageous to the designers of complex systems, such as aircraft, military equipment, and automobiles. For example, automotive systems engineers could combine tradeoff studies from the engine and transmission subsystems quickly to produce a comprehensive tradeoff study for the power train. This level of knowledge reuse is in keeping with good systems engineering practices. However, existing procedures for generating tradeoff studies involve assumptions that preclude the valid composition of tradeoff studies under uncertainty. In this paper we describe a new approach that permits engineers to compose preexisting subsystem-level tradeoff studies under uncertainty into mathematically valid system-level tradeoff studies. The approach is based on two key ideas: the use of stochastic dominance methods to enable the tradeoff evaluation when the values of the design criteria are not known with certainty (i.e., tradeoff studies under uncertainty) and the use of parameterized efficient sets to enable reuse and composition of subsystem-level tradeoff studies. The key ideas and their mathematical validity are described. The overall approach is demonstrated in the context of a tradeoff study for a motor vehicle.
Bily, ChristopherMalak, Richard
The Shock Absorber of Energy Recovery Using Electrorheological Fluid2012-01-09814/16/2012
When vehicle traveling on the bumpy road or vehicle acceleration and deceleration, which will cause the body vibration of vehicle, at the same time, a large part of energy would be absorbed by the shock absorber transforms the mechanical energy into heat energy dissipated. In order to recycle the energy of vibration and keep the stability of running car, this paper provides the shock absorber of energy recovery that recycling the energy dissipated from the traditional absorber. The shock absorber includes rod and rodless chamber cavity, the two parts contain oil outlet and oil inlet, which connected to a bridge type loop of hydraulic to make pulsating oil pressure towards one direction, when the shock absorber vibration causes pulsating oil pressure, it drives hydraulic pump operation. Because the output shaft of the hydraulic pump fixedly attached to the input shaft of generator, so the generator produces electricity for recycling energy[1]. According to the simulation and test bench indicates that this system can make use of the energy of automotive vibration. On the one hand, it overcomes fit clearance caused by the mechanical energy regenerative shock absorber in the period of high-frequency response. On the other hand, it achieves the active control of vehicle suspension system which proves the feasibility of this system[2] [3].
Wang, JunGuo, Xuexunsu, yanxia
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