alternative fuels for commercial aircraft

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    SEMINAR ON

    Alternative fuels for commercialaircrafts

    By

    Shashishekarayya.R.Hiremath

    M.Tech. 1 sem Aeronautical Engg.

    M.V.J.C.E Bangalore

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    OVERVIEW

    yNeed for alternative fuels

    y Types of alternatives

    yNear term

    y Mid term

    y Far term

    y Conclusion

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    NEED FOR ALTERNATIVESy Diminishing discovery of new petroleum sources and

    ever increasing demand.

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    yNext generation aircrafts will see 15%-20 % fuel efficient,

    making air travel one of the most efficient means oftransportion,so aircraft industries will still require an

    increasing amount of fuel

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    NEAR TERM ALTERNATIVESy Drop in fuels

    y Synthetic Jet fuel:

    Prepared from Fischer Tropsch process (FT)

    Natural gas and coal are main feedstocks

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    Positive Attributes:y Cleaner burning fuels with no sulfur

    y Higher Thermal Stability

    y Lower particulate Engine Emission

    y Show excellent low temperature properties

    y Maintaining low viscosity at lower temperature

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    Negative Attributes:

    y Poorer lubrication properties

    y Lower volumetric heat content

    y Possible contributor to elastomer leakagey Increased CO2 emission during its manufacture

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    MID TERM ALTERNATIVES

    y 10-25 years from now

    y Blending biofuels with synjets

    y Some changes in existing engine configuration

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    Challenges to be overcome:

    y Propensity to freeze at normal operating cruise

    temperatures

    y Poor high thermal stability characteristics in engine

    y Limited excess farm land

    One Promising feedstock for bio fuels is Algae.

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    FAR TERM ALTERNATIVESyNeed to reduce emissions of greenhouse gases, therefore

    low to zero carbon fuels has to be used.

    Liquid Methane

    Liquid Hydrogen

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    Methane Gas

    y Huge amounts of methane gas is trapped in the forms of

    methane hydrates.

    y 0.3 X 1012 m3 in middle east and soviet-union

    y 21.1012 m3 in Americas

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    Major issues to be considered

    y Economics of recovery under unfamiliar & inconvenient

    deep under sea conditions.y Environmental and Technical feasibility

    y Safety aspects during extraction.

    y Extraction in permafrost areas may cause global

    warming.

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    Liquid Hydrogen

    Historical and Technological Evolution of LH2

    y The first aircraft that flew with hydrogen was a US Air Force B-57 twin

    bomber that in 1956

    y In 1988, the Soviets experimented with a modified TU-154 (renamed TU-155), with one engine (out of the two) operated on hydrogen alone.

    y Retired Pan American pilot Bill Conrad converted a four seater Grutnnab

    Cheetah to run on hydrogen in 1988.

    y During the 1989 Paris Air Show, the German partner in the European

    Airbus, Messerschmidt-Boelkkov-lBlohm (MBB), showed an interest indeveloping a hydrogen fueled twin of the Airbus A310.

    y Samara Trud Project (Samara State Scientific and Production Enterprise

    (SSSPE) TRUD),

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    y cryoplane design adopted by

    Russian-German

    Cooperative Venture on the

    basis of an existing Airbus

    A310

    y NASA-Langley Research

    Center

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    LH2 advantage

    y Higher specific energy (119 190 kJ/kg) than conventional fuel (43 60

    kJ/kg). Higher fuel efficiency. Wider range of flammability.

    y Higher flame speed. Higher combustion temperature.

    y Reduced gross weight (26%). Reduced wing area (18%). Smaller engines

    and noise reduction. High heat sink capacity. Cruise lift-to-drag ratio

    reduced by 10-18%.

    y NO missions of CO, CO*, particles, HC, S compounds and odor. Reduced

    NO, (33% or less of that produced by todays turbofan engines using

    combustion chambers with premixing)

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    LH2 disadvantage

    y Four times lower energy per unit volume.

    y More voluminous fuselage. Necessity of cryogenic fuel

    system.y Airport hydrogen plant with following units needed:

    Electrolyzer, purification, liquefier, storage and

    distribution system About 2.5 times more H2O

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    Environmental considerations

    y Production of Nox

    y Green house effect of water vapor increases enormously.

    y Hydrogen is the most advantageous environmental optionover carbon based fuels, since it does not produce CO2CO, SO2, HC, etc., and lowers NOx emission.

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    afety and handling

    y Hydrogen is an extremely volatile fuel, which has to be

    handled with great care. Never the less it is not unsafe.

    yplacement of fuel tanks.

    y Hydrogen has a wide flammability range.

    y Liquid hydrogen, along with other cryogens, has a high

    liquid-to-gas volume expansion ratio, so that liquid

    hydrogen piping should always include a pressure reliefdevice.

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    Economics ofLH 2 aircraft

    y LH2 aircraft, the most influential factor is the fuel cost,

    representing 50% of the total DOC.

    yLH2price will decrease as large scale industrial facilitiesare installed.

    yNeed to build industrial facilities for LH2production.

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    CONCLUSIONy The short-term option of synthetic fuels processed in the

    FT process meets the first target, , it will not reduce CO2

    emissions over the entire life cycle.y Algae seem to be a promising future feedstock option

    which could provide a much higher oil yield per hectare

    than present bio-fuels.

    yThe large scale introduction of hydrogen into aviation

    presents no unsolvable technical problems, but it does

    involve the need for the following work items:

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    y A thorough study of the components of a cryogenic fuel

    system, mainly as regards the structural materials for

    tanks, pipes and insulation systems.y Developing monitoring systems to detect hydrogen leaks

    in hydrogen installations.

    y Research on reducing NOx emissions.

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    QUESTIONSuu

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    THANK YOU