Browse Topic: Sun and solar

Items (342)
Creation of an Icephobic Coating using Graphite Powder and PTFE Nanoparticles2019-01-19796/10/2019
Ice accretion can cause numerous inefficiencies, structural stresses, and failures in applications ranging from building design to power generation and aerospace applications. Currently, some of the leading de-icing technologies, such as the ICE-WIPS system, utilize a heating element coupled with a superhydrophobic surface. The high power consumption inherent in these systems can make them expensive and impractical, especially when coupled with power generating systems. Reduced power consumption in these de-icing technologies can be achieved through increased absorption of solar radiation in the visible range while maintaining hydrophobic performance of a coating. In this work, a Polytetrafluorethylene (PTFE) and graphite-based superhydrophobic surface is proposed, which maintains similar hydrophobic performance to standard superhydrophobic surfaces. The novel coating demonstrates contact angles of upwards of 130o and sliding angles of less than 4o, while increasing solar radiation absorption in the visible range by approximately 139% over PTFE-based hydrophobic coatings. Icing wind tunnel tests where the coatings were exposed to visible light in order to simulate solar radiation were performed in a variety of different conditions in order to verify the improved de-icing capabilities introduced by the added graphite. The melting time per unit ice mass was reduced by upwards of 50% for glaze ice and 8.0% for rime ice over a comparable de-icing coating without added graphite. There was also a qualitative difference in de-icing performance, as the coating with added graphite demonstrated removal of ice in a single sheet from the base layer, in contrast to the PTFE only coating, which allowed for the ice to melt in multiple pieces from the model.
Gonzales, JosephSakaue, Hirotaka
Custom Data Logger for Real-Time Remote Field Data Collections17AERP10_1010/1/2017
Compact, energy efficient instruments have the same functionality as a personal computer. Army Engineer Research and Development Center, Vicksburg, Mississippi The U.S. Army Corps of Engineers (USACE), CHL, FRF, had a need for a remote real-time data collection system to control instruments and log and communicate data from five observing stations in the Currituck Sound Estuary, NC1. These stations, referred to as the Currituck Sound Array (CSA), collect a suite of meteorological and oceanographic data including wind, air temperature, humidity, incoming solar radiation (above and below water), waves, currents, water level, salinity, and water temperature, as well as turbidity and many other water quality parameters. This array of instruments has a variety of control commands, sample routines, and output data formats. Additionally, the CSA was designed to act as a natural laboratory for estuarine research and as an instrument and model test bed. These capabilities required a reliable and flexible system that would allow easy modification of sampling schemes, the ability to log as many as 15 instruments with a single logger, and allow the incorporation of additional and novel instrumentation with minimal effort and expense. The custom loggers were built upon single board computers (SBC) running the Linux operating system. They effectively have the same functionality as a personal computer, overcoming many of the limitations of off-the-shelf loggers. Additionally, off-the-shelf loggers typically operate on a very limited set of commands. These custom Linux-based loggers have a much more diverse and powerful selection of commands, overcoming many of the unique challenges of real-time data collection with robust code and programmatic “watchdogs” that can automatically make sure the logger, instruments, and communications are operating as intended.
The Flying Carpet: Aerodynamic High-Altitude Solar Reflector Design Study2017-01-20269/19/2017
Our concept studies indicate that a set of reflectors floated in the upper atmosphere can efficiently reduce radiant forcing into the atmosphere. The cost of reducing the radiant forcing sufficiently to reverse the current rate of Global Warming, is well within reach of global financial resources. This paper summarizes the overall concept and focuses on one of the reflector concepts, the Flying Carpet. The basic element of this reflector array is a rigidized reflector sheet towed behind and above a solar-powered, distributed electric-propelled flying wing. The vehicle rises above 30,480 m (100,000 ft) in the daytime by solar power. At night, the very low wing loading of the sheets enables the system to stay well above the controlled airspace ceiling of 18,288 m (60,000 ft). The concept study results are summarized before going into technical issues in implementation. Flag instability is studied in initial wind tunnel experiments. This has forced evolution of the concept to one similar to a hang-glider, the sheet supporting the propelled wing at very low flight speed. Later designs may dispense with the wing altogether. Lift-induced drag can be minimized by joining several elements together in flight to create a large aspect ratio, and by staggering elements in flight as long-distance birds do, with swarm flight control. The primary parameter is the areal density that can be achieved for the reflector sheet under aerodynamic loads. Successful designs can be closed even with 2-mil Mylar sheets, but going to strengthened versions of solar sails would offer strong advantages. Mass-based cost estimation allows an upper bound on architecture cost by comparing equivalent number of launch masses of a well-known large space launch system. The next level of cost analysis shows that the manufacturing cost which is dominant, is best addressed through automotive industry techniques.
Komerath, NarayananHariharan, ShravanShukla, DhwanilPatel, SahajRajendran, VishnuHale, Emily
A Distributed Simulation of a Martian Fuel Production Facility2017-01-20229/19/2017
The future of human exploration in the solar system is contingent on the ability to exploit resources in-situ to produce mission consumables. Specifically, it has become clear that the success of a manned mission to Mars will likely depend on fuel components created on the Martian surface. While several architectures for an unmanned fuel production surface facility on Mars exist in theory, a simulation of the performance and operation of these architectures has not been created. In this paper, the framework describing a simulation of one such architecture is defined. Within this architecture, each component of the base is implemented as a state machine, with the ability to communicate with other base elements as well as a supervisor. An environment supervisor is also created which governs low level aspects of the simulation such as movement and resource distribution, in addition to higher-level aspects such as location selection with respect to operations specific behavior. This simulation will be implemented as an HLA (IEEE 1516e High Level Architecture) application, where each component of the base exists as a federate. A visualization of this simulation is created using a NASA visualization tool called DON (Distributed Observer Network). Metrics, such as fuel production throughput, are then cross validated against result data produced by a concurrent simulation project aiming to model the same scenario using different tools and methodology.
Loundy, KatherineSchaefer, LouisForan, AndrewNinah, CatherineBandong, KhristopherBrown, RobertHeston, HunterSteed, John-PaulYoung, WilliamHeinrich, MarkRabelo, Luis
Tradeoff Study of High Altitude Solar Reflector Concepts2017-01-21439/19/2017
A direct solution to Global Warming would be to reflect a part of sunlight back into Space. A system tradeoff study is being developed with three of the concepts that are being evaluated as long-endurance high-altitude reflectors. The first concept is a high aspect ratio solar powered flying wing towing reflector sheets. This concept is named “Flying Carpet”. Second is a centrifugally stretched high altitude solar reflector (CSHASR). The CSHASR has 4 rotors made of reflector sheets with a hub stretching to 60 percent of the radius, held together by an ultralight quad-rotor structure. Each rotor is powered by a solar-electric motor. A variation on this concept, forced by nighttime descent rate concerns, is powered by tip-mounted solar panels and propellers with some battery storage augmenting rotational inertia as well as energy storage. The third concept is an Aerostatically Balanced Reflector (ABR) sheet, held up by hydrogen balloons. A set of co-axial counter-rotating rotors provides trim, directional control and migration with the summer Sun. This concept also offers the ability to hold up the reflector at arbitrary orientations to achieve maximum reflection, normal to the slanted rays of the polar summer sun. This paper presents concept evaluation and comparisons, explaining the concepts and high-level features of each concept in this extreme and little-explored regime of rotorcraft aeromechanics as well as aerostatics.
Komerath, NarayananShukla, DhwanilHariharan, ShravanPatel, SahajHiremath, Nandeesh
The Development of Direct Drive Motors for Solar Cars2017-01-12323/28/2017
Solar car races are held worldwide, aiming to promote vehicles that help reduce environmental loads on the roads. In order to gain superiority in solar car racing, it is essential to develop a high efficiency brushless direct drive motor that optimizes the energy use to the fullest and allows high speed driving when needed. To achieve these goals, two development approaches of solar car motors are proposed: the high efficiency motor which improves electrical characteristics and significantly reduces energy loss; and the variable field magnet motor that offers instant speed boost for a temporary period of time for overtaking opponents. We have developed a high efficiency motor through the application of an amorphous core and laminated magnets. Instead of the standard method of the W-EDM (Wire-Electric Discharge Machining) for amorphous cores, we utilized water jet cutting, through which we succeeded in achieving insulation between laminated cores. In general, a sheet of magnet is used in each slot and its dimension is determined according to the lamination height of the core. In this project, multiple magnet segments shorter in the direction of the shaft are stacked vertically to achieve the desired height, which successfully resulted in the reduction of iron loss. The application of these methods led to the achievement of motor efficiency exceeding 98%. For the instant speed increase, we have developed the optimized design configuration for a variable field magnet module that can change T-N characteristics, utilizing our unique method for varying the effective magnetic flux. The result shows that our variable field magnet motor achieved a 1.57 times higher rotational speed than conventional types. The proposed technologies can contribute to the efficient use of energy in solar car applications, promoting the development of novel solar car systems.
Yamazakii, TsubasaUchiyama, HidekazuNakazawa, KazuakiIsomura, TsubasaOgata, Hisashi
Development Solar Charging System of Vehicle2017-01-15983/28/2017
Fuel consumption and CO2 emission regulations for vehicles, such as the Zero Emission Vehicle (ZEV) Regulation, motivate renewable energy technologies in the automotive industry. Therefore, the automotive industry is focused on adopting solar charging systems. Some vehicles have adopted solar energy to power the ventilation system, but these vehicles do not use solar energy to power the drivetrain. One important issue facing the design of solar charging systems is the low power generated by solar panels. Compared to solar panels for residential use, solar panels for vehicles can’t generate as much power because of size and weight limitations. Also, the power generated by solar panels can be extremely affected depending on differences in solar radiation among the cells. Therefore, Toyota has developed a solar charging system that can use solar energy for driving the Prius PHV. This system can efficiently charge the hybrid battery with the low power generated by the solar panel. The power generated can charge the hybrid battery while the vehicle is parked. Power can also be supplied from the hybrid battery to the auxiliary battery system during driving. The solar power contributes to the improvement of the electric driving range and the fuel consumption. This paper shows a solar charging system applied to a plug-in hybrid vehicle, a system configuration, operating modes, improving the standby power consumption of the system, and structure of solar panel.
Go, KoichiHirano, TakahiroMiyoshi, TatsuyaSato, Daisuke
SUV Solar Roof with Photo-Thermal Effect for Ventilation ORC System2016-01-02404/5/2016
The Organic Rankine Cycle System (ORC) is an effective means to use the solar energy. The system adopts the solar energy on the car roof as the heat source to make the ORC work and drive the thermoelectric air-conditioner. It can improve the entering comfort on the parking condition and the vehicle energy utilization efficiency. In this research, the system comprehensively applied the principle of sunshine concentration, heat collection and photo electricity. Then considering the working condition and performance features of ORC system, the car roof was designed to have a compact structure, through which the efficiency of the solar vehicle system could be improved. Firstly, the research analyzed the heat source temperature and the heat flux impact on the output power of the ORC system. After that, the performance of heat collection was identified according to the given thermoelectric air-condition’s power requirements. After building the model of three kinds of solar collectors, through the analysis and frequency division utilization of it, the basic requirements about stable output power by the solar energy could meet on the condition of different illumination. By the research and analysis, the ORC system could run normally and the output power was changed by sunlight’s condition with a certain scope of illuminance and a certain incident angle. Besides, the use of roof’s solar power could supply energy for a part of vehicle’s electric system and reduce energy consumption.
Zhan, RuobingTan, GangfengYang, BoZhang, ZhiweiWang, TieLiu, CenyiWu, XintongRen, YanjunXu, Haobo
Solar Heat Load on the Vehicle Occupants2016-01-02464/5/2016
Vehicle occupants, unlike building occupants, are exposed to continuously varying, non-uniform solar heat load. Automotive manufacturers use photovoltaic cells based solar sensor to measure intensity and direction of the direct-beam solar radiation. Use of the time of the day and the position - latitude and longitude - of a vehicle is also common to calculate direction of the direct-beam solar radiation. Two angles - azimuth and elevation - are used to completely define the direction of solar radiation with respect to the vehicle coordinate system. Although the use of solar sensor is common in today’s vehicles, the solar heat load on the occupants, because of their exposure to the direct-beam solar radiation remains the area of in-car subjective evaluation and tuning. Since the solar rays travel in parallel paths, application of the ray tracing method to determine solar insolation of the vehicle occupants is possible. Calculating the solar exposure however requires the knowledge of geometry of the passenger compartment of a vehicle in addition to the direction of the direct-beam solar radiation. Geometry information includes 3D coordinates of the vehicle glasses and the passenger seating location. Planar surface approximation is used to represent both the glasses and the seats. Further the seat coordinates are shifted to obtain exposure of the occupants than the seats. Shifting of the seat coordinates is performed according to the thickness of chest and lap of an average adult. The solar exposure calculation also requires correction to the measured solar intensity. The correction is to account for attenuation of the solar radiation by the transmittance of the vehicle glasses. The solar heat load is then obtained by multiplying the occupant’s solar exposure area in m2 and the transmitted solar intensity in W/m2 for the given solar angles and vehicle geometry. The results of solar heat load so obtained are compared with the CFD Fluent data for a compact SUV.
Kakade, Rupesh SonuMer, Prashant
The goal of the High Energy Replicated Optics to Explore the Sun (HEROES) mission was to adapt an existing balloon payload, known as High Energy Replicated Optics (HERO), for solar observation. HERO used an on-axis star camera for fine aspect sensing, but this camera was too sensitive to be used when pointed near or toward the Sun. The pitch and yaw aspect system (PYAS) replaced the star camera during solar pointing. The PYAS used a computer vision algorithm to generate aspect solutions based on observations of a carefully constructed scene.
The development of a conformal nanotube process is enabling for many applications in solar physics and space astrophysics (e.g., direct detection and imaging of exoplanets). Coronagraphs are key heliophysics instruments because they image coronal mass ejections (CMEs), which are the most energetic phenomena on the Sun. CMEs have wide-ranging impact on the heliosphere, from interplanetary spacecraft to Earthorbiting satellites, communications, and astronaut safety; in short, they are major drivers of space weather. In a typical space-based coronagraph, an external occulter blocks light from the disk of the Sun so that the corona (about a million times dimmer) can be imaged. The occulter must suppress both diffracted light and stray light.
Modelling and Evaluation of Aircraft Contrails for 4-Dimensional Trajectory Optimisation2015-01-25389/15/2015
Contrails and aircraft-induced cirrus clouds are reputed being the largest components of aviation-induced global warming, even greater than carbon dioxide (CO2) exhaust emissions by aircraft. This article presents a contrail model algorithm specifically developed to be integrated within a multi-objective flight trajectory optimization software framework. The purpose of the algorithm is to supply to the optimizer a measure of the estimated radiative forcing from the contrails generated by the aircraft while flying a specific trajectory. In order to determine the precise measure, a comprehensive model is employed exploiting the Schmidt-Appleman criterion and ice-supersaturation regions. Additional parameters such as the solar zenith angle, contrail lifetime and spread are also considered. The optimization of flight trajectories encompassing such contrail model allows for selective avoidance of the positive radiative forcing conditions, such as only avoiding persistent contrails, or contrails which lead to negative radiative forcing. The model assesses the radiative forcing associated with 4-Dimensional (4D) trajectories in a 4D weather field, encompassing both the local time-of-day and the contrail lifetime. Some preliminary algorithm validation activities are presented, including a simulation case study involving a medium-range domestic flight of a turbofan aircraft from Melbourne to Brisbane.
Lim, YixiangGardi, AlessandroSabatini, Roberto
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.
The dynamics in the vicinity of small bodies are highly nonlinear. Trajectory design in small-body environments requires accurate gravity and solar radiation pressure models to guarantee the satisfaction of spacecraft operational constraints such as thruster silent times, state, and control constraints. The G-PROX guidance algorithm generates fuel-optimal trajectories in the vicinity of asteroids and small bodies. The non-convexity in the control constraints is handled with the lossless convexification technique, which is a convex relaxation of the control constraints. G-PROX uses sequential convex programming and solves a convergent sequence of convex optimization problems generated via sequential linearization of both the dynamics and control bounds, synergistically combined with lossless convexification. The sequence of convex optimization problems converges to a locally optimal solution of the original nonlinear non-convex problem.
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).
One-Dimensional Solar Heat Load Simulation Model for a Parked Car2015-01-03564/14/2015
Passenger comfort and safety are major drivers in a typical automotive design and optimization cycle. Addressing thermal comfort requirements and the thermal management of the passenger cabin within a car, which involves accurate prediction of the temperature of the cabin interior space and the various aggregates that are present in a cabin, has become an area of active research. Traditionally, these have been done using experiments or detailed three-dimensional Computational Fluid Dynamics (CFD) analysis, which are both expensive and time-consuming. To alleviate this, recent approaches have been to use one-dimensional system-level simulation techniques with a goal to shorten the design cycle time and reduce costs. This paper describes the use of Modelica language to develop a one-dimensional mathematical model using Modelica language for automotive cabin thermal assessment when the car is subjected to solar heat loading. The developed model has the capability to predict the thermal response of a car cabin and its internal aggregates, such as seats, dashboards, roof, etc. for hot day solar loading conditions. A solar radiation model is established to capture the solar radiation that included movement of the sun position with time. In addition, the model included natural convection heat transfer and solid conduction effects for precise prediction of cabin aggregates temperature. The developed one-dimensional model is validated by comparing its predictions against the prediction of a high-resolution three-dimensional CFD model for a range of boundary and operating conditions. The results show an excellent agreement with CFD results with the temperatures being predicted to within ±2 K of that predicted by the CFD model.
Patil, AniketRadle, ManojShome, BiswadipRamachandran, Sankar
Solar Powered Vehicle Parking Ventilation System Pre-Cooling Analysis2015-01-03674/14/2015
The cabin air temperature increases quickly and can reach 80°C when the vehicle parks in the summer sunlight which has the bad influence on the occupants entering comfort. Some luxury vehicles, like Audi A8[1], reduce the internal temperature through operating air-condition in advance or using on-board battery to drive the cabin ventilator, which requires relatively complex control system and limits the system's operating time because of energy consumption. This research adopts the solar wing as the ventilation power supply and accomplishes the cabin real-time heat rejection by achieving the steady air circulation for both inside and outside environment. First, the static thermal transfer model of the crew cabin is established. Then, on the basis of the parameters of the prototype ventilation pipe, the ventilation model for the outside circulation is built. After that, the parameters of the solar wing are determined according to the control target of the cabin internal air temperature. Besides, combination of the working conditions for both the solar wing and the ventilator are analyzed. Experiments have been conducted for verifying the static thermal transfer model and the ventilation model. The results show that the system can reduce the cabin air temperature with a maximum of 15°C, therefore, the occupant entering comfort is improved when vehicle is parking under the hot sun.
Hu, ZhiqiangTan, GangfengLi, ZhileiXu, HaoboHuang, WenhuiYe, Yifan
Sleeper Cab Climate Control Load Reduction for Long-Haul Truck Rest Period Idling2015-01-03514/14/2015
Annual fuel use for long-haul truck rest period idling is estimated at 667 million gallons in the United States. The U.S. Department of Energy's National Renewable Energy Laboratory's CoolCab project aims to reduce heating, ventilating, and air conditioning (HVAC) loads and resulting fuel use from rest period idling by working closely with industry to design efficient long-haul truck climate control systems while maintaining occupant comfort. Enhancing the thermal performance of cab/sleepers will enable smaller, lighter, and more cost-effective idle reduction solutions. In order for candidate idle reduction technologies to be implemented at the original equipment manufacturer and fleet level, their effectiveness must be quantified. To address this need, a number of promising candidate technologies were evaluated through experimentation and modeling to determine their effectiveness in reducing rest period HVAC loads. For this study, load reduction strategies were grouped into the focus areas of solar envelope, occupant environment, and conductive pathways. The technologies selected for a complete-cab package of technologies were “ultra-white” paint, advanced insulation, and advanced curtains. To measure the impact of these technologies, a nationally-averaged solar-weighted reflectivity long-haul truck paint color was determined and applied to the baseline test vehicle. Using the complete-cab package of technologies, electrical energy consumption for long-haul truck daytime rest period air conditioning was reduced by at least 35% for summer weather conditions in Colorado. The National Renewable Energy Laboratory's CoolCalc model was then used to extrapolate the performance of the thermal load reduction technologies nationally for 161 major U.S. cities using typical weather conditions for each location over an entire year.
Lustbader, Jason A.Kreutzer, CoryAdelman, StevenYeakel, SkipZehme, John
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
Items per page:
1 – 50 of 342