Reduction of Particulate Emissions in Turbine Engines Using the +100 Additive PDF Download
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
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Book Description
The U.S. military spends approximately about $3.5 billion (2003 dollars) per year for aviation fuel. This corresponds to 3 to 4 billion gallons per year (~10% of total U.S. aviation fuel use). The fleet average emission index for particulate matter (PM) has been estimated to be approximately 0.04 g/kg of fuel burned. The total amount of particulate emissions for aircraft in the United States is estimated at 3 million kg per year. Although there is some uncertainty in these estimates, they are consistent with the magnitude being used to estimate global emissions from aircraft (Niedzwiecki, 1998). Airborne particles pose both health and environmental risks. The health effects of particulate matter are related to its ability to penetrate the respiratory system. Particulate matter 2.5 microns or less in diameter (PM2.5) can enter the lungs and end up in lung capillaries and air sacs (alveoli), causing a variety of respiratory problems. Particulate emissions contribute to environmental problems such as visibility impairment (haze) and may contribute to increased signature (infrared emissions) from military aircraft, thus increasing aircraft detectability/vulnerability in enemy territory. Gas turbine engines and ground support equipment are major local sources of PM2.5 particles. The health and environmental concerns from particulate emissions motivated this work to evaluate the use of the +100 (BetzDearborn SpecAid 8Q462) additive in jet fuel as a means to reduce the particulate emissions from military gas turbine engines. The +100 additive was developed to increase the thermal stability of JP-8 fuel in order to reduce carbon buildup in fuel system components and injection nozzles. Mostly military aircraft (~3,000) are currently using the +100 additive; however, the additive is also suitable for commercial aircraft due to the similarities of JP-8 and Jet A.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
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Book Description
The U.S. military spends approximately about $3.5 billion (2003 dollars) per year for aviation fuel. This corresponds to 3 to 4 billion gallons per year (~10% of total U.S. aviation fuel use). The fleet average emission index for particulate matter (PM) has been estimated to be approximately 0.04 g/kg of fuel burned. The total amount of particulate emissions for aircraft in the United States is estimated at 3 million kg per year. Although there is some uncertainty in these estimates, they are consistent with the magnitude being used to estimate global emissions from aircraft (Niedzwiecki, 1998). Airborne particles pose both health and environmental risks. The health effects of particulate matter are related to its ability to penetrate the respiratory system. Particulate matter 2.5 microns or less in diameter (PM2.5) can enter the lungs and end up in lung capillaries and air sacs (alveoli), causing a variety of respiratory problems. Particulate emissions contribute to environmental problems such as visibility impairment (haze) and may contribute to increased signature (infrared emissions) from military aircraft, thus increasing aircraft detectability/vulnerability in enemy territory. Gas turbine engines and ground support equipment are major local sources of PM2.5 particles. The health and environmental concerns from particulate emissions motivated this work to evaluate the use of the +100 (BetzDearborn SpecAid 8Q462) additive in jet fuel as a means to reduce the particulate emissions from military gas turbine engines. The +100 additive was developed to increase the thermal stability of JP-8 fuel in order to reduce carbon buildup in fuel system components and injection nozzles. Mostly military aircraft (~3,000) are currently using the +100 additive; however, the additive is also suitable for commercial aircraft due to the similarities of JP-8 and Jet A.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 81
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Book Description
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 506
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Author: W. Cornelius
Publisher: Springer Science & Business Media
ISBN: 1468419986
Category : Science
Languages : en
Pages : 474
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Book Description
This volume documents the proceedings of the Symposium on Emissions from Continuous Combustion Systems that was held at the General Motors Research Laboratories, Warren, Michigan on September 27 and 28, 1971. This symposium was the fifteenth in an annual series presented by the Research Laboratories. Each symposium has covered a different technical discipline. To be selected as the theme of a symposium, the subject must be timely and of vital interest to General Motors as well as to the technical community at large. For each symposium, the practice is to solicit papers at the forefront of research from recognized authorities in the technical discipline of interest. Approximately sixty scientists and engineers from academic, government and industrial circles in this country and abroad are then invited to join about an equal number of General Motors technical personnel to discuss freely the commissioned papers. The technical portion of the meeting is supplemented by social functions at which ample time is afforded for informal exchanges of ideas amongst the participants. By such a direct interaction of a small and select group of informed participants, it is hoped to extend the boundaries of research in the selected technical field.
Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 700
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Author: O. M. Loveland
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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This research, a joint Air Force/Navy study, evaluated the use of fuel additives to reduce the opacity of turbine engine test cell emissions. Automated smoke abatement system (ASAS) was used to inject ferrocene and XRG fuel additives into J57-43 turbine engines. Data obtained from this study indicate that ferrocene can be used to control test cell opacity without major impact on engine performance. The XRG fuel additive was not effective in reducing opacity. Major problems encountered with the ASAS were resolved during the project. Recommendations for further improvement of the ASAS were reported. (Author).
Author: National Research Council
Publisher: National Academies Press
ISBN: 0309102472
Category : Technology & Engineering
Languages : en
Pages : 288
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Rocket and air-breathing propulsion systems are the foundation on which planning for future aerospace systems rests. A Review of United States Air Force and Department of Defense Aerospace Propulsion Needs assesses the existing technical base in these areas and examines the future Air Force capabilities the base will be expected to support. This report also defines gaps and recommends where future warfighter capabilities not yet fully defined could be met by current science and technology development plans.
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 432
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 63
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The overall technical objective of the program was to develop an additive for JP-8, JP-5, and diesel fuels that will reduce both the mass Emissions Index (grams of PM2.5 emissions/kilogram of fuel) and the number density Emissions Index (particle number density of PM2.5 emissions/kilogram of fuel) in the exhaust of military gas turbine engines by 70 percent. This report summarizes the results of work performed at United Technologies Research Center. Baseline studies were performed with ethanol added to ethylene, as the method and procedures could be validated against the existing experimental database. Experiments were performed in laminar premixed burner-stabilized flat flames. Soot was reduced by factors of about 50% with ethanol. Subsequent tests were performed with mixtures of heptane/toluene/ethylene to provide a better simulation of real fuel chemistry. The most significant effects were observed with a proprietary additive which apparently contains a metal. The use of metals is not perceived to be an environmentally acceptable approach. The next most effective additive is a commercial fuel additive, Kleen, which contains a variety of oxygenated (nitro) compounds. Reductions of soot emissions on the order of 30% were observed. Mixed results were obtained with pyridine, and modeling results show negligible influence of this additive. Finally, advances to a fundamental soot formation model were accomplished by comparing simulations of coflow diffusion flames to experimental data sets. This work resulted in proposed changes to the gas-phase kinetics and soot inception models and identifying the importance of treating soot ageing and radiation losses. The overall goal of identifying an additive that can reduce soot emissions by 70% was not achieved, without use of a metal-containing additive or with very high levels of the additive (>10% by weight).
Author: John Edward Stevens
Publisher:
ISBN:
Category : Turbines
Languages : en
Pages : 360
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