Abstract This study addresses a specific boron combustion aspect, revealing that thermodynamic conditions associated with highly boron-loaded ramjet combustors, may lead to blockage of the reaction between boron and air, causing termination of the combustion process, incomplete chemical reaction, and only partial realization of the potential boron combustion energy. Sustained boron combustion may take place when the evaporation rate of the protective liquid boron oxide layer B 2 O 3 ( l ) on the boron particles exceeds its generation rate by the oxidation reaction, typically at temperatures above 1900–2000K. However, if the actual partial pressure of gaseous boron oxide B 2 O 3 ( g ) produced in the combustion process attains the equilibrium vapor pressure of boron oxide at the conditions existing in the combustion chamber, condensation of the boron oxide to form a liquid layer on the boron particle surfaces may take place, extinguishing the particle combustion by blocking the reaction between the boron and the surrounding oxidizing gas. The study predicts conditions for blockage and incomplete boron combustion over a range of chamber pressures and temperatures. This effect may be characteristic to combustors employing boron-containing fuels, but may not be encountered in the combustion of individual boron particles in air.

    Highlights Boron has a remarkable theoretical heat of reaction with air. In boron loaded combustor saturation of boron oxide vapor may take place. Condensation of boron oxide on the boron particles causes extinguishment. Thermodynamic blocking of reaction may cause poor combustion efficiency in ramjets.


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    Titel :

    Thermodynamic limitation on boron energy realization in ramjet propulsion


    Beteiligte:
    Gany, Alon (Autor:in)

    Erschienen in:

    Acta Astronautica ; 98 ; 128-132


    Erscheinungsdatum :

    2014-01-25


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    AIAA-2005-1070 THERMODYNAMIC EFFECT ON BORON COMBUSTION IN RAMJET PROPULSION

    Scheuer, R. / Gany, A. / American Institute of Aeronautics and Astronautics; International Society for Air Breathing Engines | British Library Conference Proceedings | 2005




    Application ranges of ramjet propulsion

    Saenger-Bredt, I. | Engineering Index Backfile | 1961