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    Fuel Effects on the TF30 Engine (Alternate Test Procedure)

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 003::page 769
    Author:
    P. A. Karpovich
    ,
    A. I. Masters
    DOI: 10.1115/1.3239799
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of the Alternate Test Procedure (ATP) is to develop the capability to qualify new fuels for Navy aircraft use with a minimum of testing. The effect of fuel composition and properties on engine performance and component life has been show to vary significantly from one engine configuration to another. The P&WA approach to the ATP has been to define fuel effects on the TF30 engine and then apply the methodology to other engines of interest to the Navy. Investigations of the TF30 conducted under the ATP Program and other Navy and Air Force Contracts have produced one of the most complete fuel effect characterizations available for any gas turbine engine. Major fuel effects which have been quantified are the relationships of lubricity to main fuel control reliability, viscosity and volatility to main burner and augmentor ignition limits, and hydrogen content to smoke and combustor life. The effects of fuel properties and composition on combustion efficiency and elastomeric seal life were found to be of secondary importance. Remaining uncertainties are the effects of fuel properties on turbine life and fuel nozzle fouling rate.
    keyword(s): Engines , Fuels , Navy , Smoke , Air Force , Viscosity , Combustion , Volatility , Reliability , Combustion chambers , Gas turbines , Nozzles , Testing , Turbines , Aircraft , Hydrogen AND Ignition ,
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      Fuel Effects on the TF30 Engine (Alternate Test Procedure)

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/99796
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorP. A. Karpovich
    contributor authorA. I. Masters
    date accessioned2017-05-08T23:20:08Z
    date available2017-05-08T23:20:08Z
    date copyrightJuly, 1985
    date issued1985
    identifier issn1528-8919
    identifier otherJETPEZ-26622#769_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99796
    description abstractThe objective of the Alternate Test Procedure (ATP) is to develop the capability to qualify new fuels for Navy aircraft use with a minimum of testing. The effect of fuel composition and properties on engine performance and component life has been show to vary significantly from one engine configuration to another. The P&WA approach to the ATP has been to define fuel effects on the TF30 engine and then apply the methodology to other engines of interest to the Navy. Investigations of the TF30 conducted under the ATP Program and other Navy and Air Force Contracts have produced one of the most complete fuel effect characterizations available for any gas turbine engine. Major fuel effects which have been quantified are the relationships of lubricity to main fuel control reliability, viscosity and volatility to main burner and augmentor ignition limits, and hydrogen content to smoke and combustor life. The effects of fuel properties and composition on combustion efficiency and elastomeric seal life were found to be of secondary importance. Remaining uncertainties are the effects of fuel properties on turbine life and fuel nozzle fouling rate.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFuel Effects on the TF30 Engine (Alternate Test Procedure)
    typeJournal Paper
    journal volume107
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3239799
    journal fristpage769
    journal lastpage774
    identifier eissn0742-4795
    keywordsEngines
    keywordsFuels
    keywordsNavy
    keywordsSmoke
    keywordsAir Force
    keywordsViscosity
    keywordsCombustion
    keywordsVolatility
    keywordsReliability
    keywordsCombustion chambers
    keywordsGas turbines
    keywordsNozzles
    keywordsTesting
    keywordsTurbines
    keywordsAircraft
    keywordsHydrogen AND Ignition
    treeJournal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 003
    contenttypeFulltext
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