The objective of this eighteen-month program were to further develop two low-emission combustors-the prechamber combustor and the modified conventional combustor to install them in a Detroit Diesel Allison Model 250-C20B engine, and to evaluate their performance in an engine environment. The combustors were to retain the 50% overall reduction in gas turbine mass emissions with no increase in any individual pollutant when tested over a typical Army light observation helicopter (LOH) duty cycle.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Low-Emissions Combustor Demonstration


    Contributors:
    D. L. Troth (author)

    Publication date :

    1977


    Size :

    405 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    COMBUSTOR BURNTHROUGH PLUMES: DEMONSTRATION AND PROTECTION

    Mullender, A. J. / Coney, M. H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2003


    Flex cycle combustor development and demonstration

    Harris, M.M. / Marsh, D.N. / Vos, E.A. et al. | Tema Archive | 1993



    Low emissions trapped vortex combustor

    Deng, Yangbo / Su, Fengmin | Emerald Group Publishing | 2016