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2 edition of Turbine engine particulate emission characterization found in the catalog.

Turbine engine particulate emission characterization

D. L. Fenton

Turbine engine particulate emission characterization

by D. L. Fenton

  • 177 Want to read
  • 29 Currently reading

Published by Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service, for sale by the National Technical Information Service in Washington, Springfield, Va .
Written in English

    Subjects:
  • Aircraft exhaust emissions.,
  • Airplanes -- Turbojet engines.

  • Edition Notes

    StatementD. L. Fenton, E. W. Nordstrom, E. H. Luebcke.
    SeriesReport - Federal Aviation Administration, Systems Research and Development Service ; FAA-RD-77-165
    ContributionsNordstrom, Eric W., Luebcke, Erdmann H., United States. Federal Aviation Administration. Systems Research and Development Service.
    The Physical Object
    Paginationvi, 95 p. :
    Number of Pages95
    ID Numbers
    Open LibraryOL17818588M

    The Turbine Engine Hot Section Technology (HOST) Project of the NASA Lewis Research Center sponsored a workshop to discuss current research pertinent to turbine engine durability problems. Presentations were made concerning the hot section environment and the behavior of combustion liners, turbine blades, and turbine vanes. Materials for Gas Turbines – An Overview more than 25 years (Schilke, ). Both these alloys have been produced through the conventional ingot metallurgy route. Powder Metallurgy (PM) processing is being extensively used in production of superalloy components for gas turbines. PM processing is essentially used for Nickel-based Size: KB.

    Diesel and Gas Turbine Worldwide spoke with him about the focus the organization would take during his tenure as well as trends in emissions regulations and engine development. Worldwide: You took over the position of CIMAC president at the 28 th CIMAC World Congress in Helsinki, Finland. FUNDAMENTALS OF GAS TURBINE ENGINES INTRODUCTION The gas turbine is an internal combustion engine that uses air as the working fluid. The engine extracts chemical energy from fuel and converts it to mechanical energy using the gaseous energy of the working fluid (air) to drive the engine and propeller, which, in turn, propel the airplane.

    Exhaust gas or flue gas is emitted as a result of the combustion of fuels such as natural gas, gasoline, petrol, biodiesel blends, diesel fuel, fuel oil, or ing to the type of engine, it is discharged into the atmosphere through an exhaust pipe, flue gas stack, or propelling often disperses downwind in a pattern called an exhaust plume. Overall this is a good book on the basic theory and construction of a model gas turbine and I would recommend it to others with a similar interest. The book looks a little thin, but it is packed with lots of good information in small print. I could not give the book 4 stars because there are problems with the type setting of the equations/5(12).


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Turbine engine particulate emission characterization by D. L. Fenton Download PDF EPUB FB2

Turbine engine particulate emission characterization. Washington: Dept. of Transportation, Federal Aviation Administration, Systems Research and Development Service ; Springfield, Va.: For sale by the National Technical Information Service, (OCoLC) Material Type: Government publication, National government publication: Document.

Get this from a library. Turbine engine particulate emission characterization. [Donald L Fenton; United States. Federal Aviation Administration.

Systems Research and Development Service.]. Introduction. The fine particulate matter (PM) emissions from aircraft operations at large airports located in areas of the U. designated as non-attainment for the National Ambient Air Quality Standard (NAAQS) for PM (particles ≤ μm in aerodynamic diameter) are of major environmental concern (Waitz et al., ).Aircraft PM at cruise conditions is also important in the formation of Cited by: Bruce Miller, in Fossil Fuel Emissions Control Technologies, Fuel oil fly ash formation and characterization.

In general, particulate matter emissions depend predominately on the grade of the fuel oil fired. Combustion of lighter distillate fuel oils results in lower particulate matter formation than does combustion of heavier residual oils because the heavier fuels oils contain.

Growing concern over emissions from increased airport operations has resulted in a need to assess the impact of aviation related activities on local air quality in and around airports, and to develop strategies to mitigate these effects.

One such strategy being investigated is the use of alternative fuels in aircraft engines and auxiliary power units (APUs) as a means to diversify fuel.

This RTO lecture series reviews engine technologies suitable for supersonic and hypersonic propulsion: rocket propulsion units, turbine based combined cycles, ramjet/scramjet, and pulsed detonation.

find that the sections on visible emissions and particulate emission rates and Particulate mass emissions from a JCE-8 engine A-1 to \ Particulate mass emissions from a JCE-8D engine A to A (with ferrocene additive) The fuel flow through a military gas turbine engine is difficult to.

I File Size: 5MB. Two field campaigns were performed to collect an extensive set of particle and gaseous emission data for on-wing gas turbine engines.

The tests included CFM56, RBE4-B, AE, PW, and CJ engines, providing the opportunity to compare emissions from a wide range of engine by: Stationary turbine engines in peak power installations or jet engine test cells produce particulate emissions, noise, and NOX.

The opacity of the emissions ranges from 0 to'80%, the particulate loading, gr/scf at engine exhaust point, and noise level after sound abatement of deci-bels.

With cooling of the exhaust gas, the. Staged tests were conducted to measure the particle and vapor emissions from a CFMB1 gas-turbine engine mounted on a KCT Stratotanker airframe at different engine loads. oxides, cannot.

Characterization of the pollu-tants requires careful measurement and semi-theoretical analysis. The pollutants shown in Table 1are a function of gas turbine operating conditions and fuel composition.

In the following sections, each pollutant will be considered as a function of Gas Turbine Emissions and Control GE Power Systems.

Particulate sizing and emission indices for a jet engine exhaust sampled at cruise Effective Density and Mass-Mobility Exponent of Aircraft Turbine Particulate Matter, Journal of Propulsion and Power, 31, 2,Physical Characterization or Aerosol Emissions from a Commercial Gas Turbine Engine, Journal of Propulsion and Power, 23, 5.

@article{osti_, title = {Characterization of exhaust emissions from diesel-powered passenger cars with particular reference to unregulated components}, author = {Lies, K H and Postulka, A and Gring, H}, abstractNote = {Besides regulated components VW's research program in the field of characterization of diesel emissions comprises a detailed analysis of the particulates and a.

Aircraft exhaust contains nonvolatile (soot) particulate matter (PM), trace gas pollutants, and volatile PM precursor material. Nonvolatile soot particles are predominantly present at the engine exit plane, but volatile PM precursors form new particles or add mass to Cited by: 4.

The object of the work described in this report has been the characterization of particulate-bound chemicals emitted from military aircraft, both as they are emitted and as the exhaust ages.

Three Air Force turbine engines (TFP3, TFP7, and J79C) were examined in this study, using engine test cells at Tinker AFB OK. The microscopic characteristics of soot particulate matter (PM) in gas turbine exhaust are critical for an accurate assessment of the potential impacts of the aviation industry on the environment and human health.

The morphology and internal structure of soot particles emitted from a CFM B26/3 turbofan engine were analyzed in an electron microscopic study, down to the nanoscale, for ∼ Cited by: Section 3.

Technology Characterization – Combustion Turbines. Introduction. Gas turbines have been in use for stationary electric power generation since the late s. Turbines went on to revolutionize airplane propulsion in the s, and since the s through today, they haveFile Size: 1MB.

Step 4: Turbine The turbine is another series of 'fans', which work like a windmill, absorbing energy from the high speed air passing through it.

The turbine blades are connected to and turn a shaft, which is also connected to the compressor blades at the front of the engine. emission combustion system used in the Mercury 50 engine that was produced under a joint contract between Solar Turbines and the Department of Energy.

Prior to joining Solar Turbines (in ) he spent 30 years working in the field of combustion system design and development for all types of File Size: KB. Stationary Gas Turbines For Electricity Generation General1 A gas turbine is an internal combustion engine that operates with rotary rather than reciprocating motion.

Gas turbines are used in a broad scope of applications including electric power generators, and in various process industries. Differences in the mechanism of soot formation, between a wick lamp and a gas turbine combustor, as evidenced by the effect of hydrocarbon structure, are discussed in detail.

Relevant information is reviewed on both the effect of smoke-abatement fuel additives and the morphology of Cited by: A gas turbine, also called a combustion turbine, is a type of continuous and internal combustion main elements common to all gas turbine engines are: an upstream rotating gas compressor; a combustor; a downstream turbine on the same shaft as the compressor.; A fourth component is often used to increase efficiency (on turboprops and turbofans), to convert power into mechanical or.Gas Turbine Engine Performance Monitor for Reduced Emissions | Final Report Top of Page The perspectives, information and conclusions conveyed in research project abstracts, progress reports, final reports, journal abstracts and journal publications convey the viewpoints of the principal investigator and may not represent the views and policies.