The reduction of oxides of nitrogen (NO(x)) emissions from aircraft gas turbine engines is a vital part of the NASA High Speed Research Program. Emissions reductions are critical to the feasibility of future High Speed Civil Transports which operate at supersonic speeds in the stratosphere. It is believed that large fleets of such aircraft using conventional gas turbine engines would emit levels of NO(x) that would be harmful to the stratospheric ozone layer. Previous studies have shown that NO(x) emissions can be reduced from stationary powerplant exhausts by the addition of additives such as ammonia to the exhaust gases. Since the exhaust residence times, pressures and temperatures may be different for aircraft gas turbines, a study has been made of additive effectiveness for high speed, high altitude flight.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    NO(x) reduction additives for aircraft gas turbine engines


    Beteiligte:

    Kongress:

    AIAA, SAE, ASME, and ASEE, Joint Propulsion Conference and Exhibit ; 1993 ; Monterey, CA, United States


    Erscheinungsdatum :

    1993-06-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    NO(x) reduction additives for aircraft gas turbine engines

    ADELMAN, HENRY / MENEES, GENE / CAMBIER, JEAN-LUC | AIAA | 1993


    Aircraft gas turbine engines

    Engineering Index Backfile | 1948


    Control of aircraft turbine engines

    Ravagli, A. / Noel, P. | Engineering Index Backfile | 1968


    Starting of Aircraft Gas Turbine Engines

    M. A. Alabin / B. M. Kats / Y. A. Litvinov | NTIS | 1972