190 research outputs found

    Network tariffs applicable to households in Australia: empirical evidence

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    Presents information and analysis of the network tariffs applicable to household electricity consumers in the southern and eastern states of Australia covered by the National Energy Market. Executive summary: This report presents information and analysis of the network tariffs applicable to household electricity consumers in the southern and eastern states of Australia covered by the National Energy Market (NEM). The paper is the first of four papers focused on network tariffs from the perspective of households. Key findings include: A range of network tariff structures are used throughout the NEM. Inclining block rate tariffs (with small price increments) and two-part tariffs are common. The most expensive network tariff in Australia is almost four times higher than the least expensive. The average network charge to households in Victoria is about a third of that elsewhere in the NEM The gap between least expensive and most expensive network tariff has doubled over the last seven years. Network service providers in Queensland have the highest charges and also the greater proportion of their charge is fixed. The Queensland distributors and Ausnet Services in Victoria have increased their fixed charges significantly recently. In the 2015/16 year (not covered in this report Citipower and Powercor have both increased their fixed charges significantly). Network service providers are typically increasing fixed charges more quickly than variable charges. The international comparison shows that network tariffs in Britain are generally much lower than anywhere in Australia. The average network charge in Denmark and New Zealand is roughly comparable to those in Victoria, the lowest network cost jurisdiction in the NEM. The proportion of revenue recovered from fixed charges charged to most consumers in the NEM is higher than that in Britain, Denmark and New Zealand. Some distributors in Victoria have relatively smaller fixed charges, while those in Queensland and Essential Energy in New South Wales have fixed charges that are much higher than those found elsewhere. In NZ, network tariffs with higher fixed charges apply to households with high levels of consumption (> 9 MWh per year)

    A critique of the Victorian retail electricity market

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    The Brotherhood of St Laurence commissioned Bruce Mountain from Carbon and Energy Markets (CME) to investigate the Victorian retail electricity market.  Electricity costs have been rising across Australia’s National Electricity Market since 2007. In most Australian states rising network costs – the poles and wires – have been the primary cause of these price increases.   However, the Victorian case is different. Network costs are lower than in other states, and haven’t risen as much. High retail charges appear to be the cause. The report and accompanying summary, released 7 July 2015, investigate the dynamics of the retail energy market and how that impacts on householders bills

    A temperature-controlled device for volumetric measurements of Helium adsorption in porous media

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    We describe a set-up for studying adsorption of helium in silica aerogels, where the adsorbed amount is easily and precisely controlled by varying the temperature of a gas reservoir between 80 K and 180 K. We present validation experiments and a first application to aerogels. This device is well adapted to study hysteresis, relaxation, and metastable states in the adsorption and desorption of fluids in porous media

    Project ARES 2: High-altitude battery-powered aircraft

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    A high-altitude, battery-powered, propeller-driven aircraft was designed and is being built by undergraduate students at California State University, Northridge. The aircraft will fly at an altitude of 104,000 ft at Mach 0.2 (190 ft/sec) and will be instrumented to record flight performance data, including low Reynolds number propeller and airfoil information. This project will demonstrate the feasibility of electric-powered flight in a low-density, low-temperature Earth environment that models the atmosphere of Mars. Data collected will be used to design a Mars aircraft to investigate the surface of Mars prior to manned missions. The instrumented payload and the mission profile for the high-altitude Earth flight were determined. Detailed aerodynamic and structural analyses were performed. Control, tracking, and data recording subsystems were developed. Materials were obtained and fabrication begun. The aircraft has a 32-ft wing span, a wing area of 105 sq ft, is 17.5 ft long, has a 12-in payload bay, and weighs 42 lb. It is composed primarily of lightweight materials, including Mylar, and composite materials, including graphite/epoxy and aramid core honeycomb sandwich. Low-altitude flight testing to check guidance and control systems and to calibrate data-gathering instruments will take place this summer, followed shortly by the 104,000-ft flight

    A high resolution spectroscopic study of the oxygen molecule

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    A high resolution spectrometer which incorporates a narrow line width tunable dye laser was used to make absorption profiles of 57 spectral lines in the Oxygen A-Band at pressures up to one atmosphere in pure O2. The observed line profiles are compared to the Voigt, and a collisionally narrowed, profile using a least squares fitting procedure. The collisionally narrowed profile compares more favorable to the observed profiles. Values of the line strengths and self broadening coeffiencients, determined from the least square fitting process, are presented in tabular form. It is found that the experssion by Watson are in closest agreement with the experimentally determined strengths. The self broadening coefficients are compared with the measurements of several other investigators

    A throat-bypass stability system for a YF-12 aircraft research inlet using self-acting mechanical valves

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    Results of a wind tunnel investigation are presented. The inlet was modified so that airflow can be removed through a porous cowl-bleed region in the vicinity of the throat. Bleed plenum exit flow area is controlled by relief type mechanical valves. Unlike valves in previous systems, these are made for use in a high Mach flight environment and include refinements so that the system could be tested on a NASA YF-12 aircraft. The valves were designed to provide their own reference pressure. The results show that the system can absorb internal-airflow-transients that are too fast for a conventional bypass door control system and that the two systems complement each other quite well. Increased tolerance to angle of attack and Mach number changes is indicated. The valves should provide sufficient time for the inlet control system to make geometry changes required to keep the inlet started

    The Role of Cancer Stem Cells and MicroRNAs in Human Prostate Cancer

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    High-glucose feeding of gilthead seabream (Sparus aurata) larvae: effects on molecular and metabolic pathways

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    Nutritional programming has begun to arouse interest as a novel tool to alter specific metabolic pathways or functions in farmed animals. The aim of the present study was to explore the potential of early glucose stimuli to induce changes in nutrient metabolism of gilthead seabream. Nutritional conditioning was performed by delivering glucose-rich feed at three distinct recurrent periods of larval feeding regime: during first-feeding with rotifers (3 days after hatching, DAH) and mid-feeding with Artemia metanauplii (20DAH) and the beginning of inert diet feeding (30DAH), called the Recurrent treatment (REC). As opposed, the control treatment (CTRL) did not experience any glucose stimuli. At post-larval stage (from 50 to 60DAH), both treatments were challenged with a high-carbohydrate diet (50%). The immediate response to the early stimuli was assessed through gene expression of metabolic markers and by nutrient metabolism using [C-14] tracers. Each dietary stimulus induced metabolic changes on REC larvae, shown by altered expression of some genes, including those involved in glycolysis, and by a different pattern of glucose utilization. However, none of the molecular adaptations (except G6PDH gene) were persistent in the viscera and muscle of challenged post-larvae from REC group. In contrast, the glucose metabolism of challenged REC post-larvae revealed a shift towards a higher catabolism and lower glucose retention in tissues, compared to the CTRL group, suggesting an improvement of glucose oxidation pathways. In addition, the REC group showed a higher bio-conversion of glucose into lipids, indicating enhanced hepatic lipogenesis. The early stimuli did not affect the relative retention or use of amino acids or the growth and survival of challenged fish, up to 60DAH. In summary, although not substantiated at a molecular level, our data reveal that a recurrent high-glucose stimulus during larval stages affects the short-term modulation of pathways for glucose utilization in gilthead seabream. (C) 2015 Elsevier B.V. All rights reserved

    A rotor-mounted digital instrumentation system for helicopter blade flight research measurements

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    A rotor mounted flight instrumentation system developed for helicopter rotor blade research is described. The system utilizes high speed digital techniques to acquire research data from miniature pressure transducers on advanced rotor airfoils which are flight tested on an AH-1G helicopter. The system employs microelectronic pulse code modulation (PCM) multiplexer digitizer stations located remotely on the blade and in a hub mounted metal canister. As many as 25 sensors can be remotely digitized by a 2.5 mm thick electronics package mounted on the blade near the tip to reduce blade wiring. The electronics contained in the canister digitizes up to 16 sensors, formats these data with serial PCM data from the remote stations, and transmits the data from the canister which is above the plane of the rotor. Data are transmitted over an RF link to the ground for real time monitoring and to the helicopter fuselage for tape recording. The complete system is powered by batteries located in the canister and requires no slip rings on the rotor shaft
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