An aircraft including a fuselage having one or more surfaces. At least one engine is mounted in the fuselage. The at least one engine includes an exhaust outlet. A high velocity jet is arranged at the fuselage forward of the exhaust outlet. The high velocity jet is positioned to direct a stream of high velocity gases toward the exhaust outlet redirecting exhaust gases from the one or more surfaces.


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    Title :

    SYSTEM FOR PREVENTING EXHAUST GAS IMPINGEMENT ON AIRCRAFT SURFACES AND SURROUNDING AREAS


    Contributors:

    Publication date :

    2019-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    Dynamic loading of aircraft surfaces due to jet exhaust impingement

    Lansing, D. L. / Drischler, J. A. / Brown, T. J. et al. | NTRS | 1973


    Simulated VTOL Exhaust Impingement on Ground Surfaces

    Grotz, C. A. | SAE Technical Papers | 1961


    Exhaust-Plume Impingement Characteristics

    Smith, S. D. / Wojciehowski, C. J. | NTRS | 1983


    Impingement Of Rocket Exhaust

    Drake, Bret G. / Leahy, Kenneth S. | NTRS | 1988


    Progress in Measuring Water Impingement Characteristics on Aircraft Surfaces

    Papadakis, M. / Vu, G. T. / Hung, E. K. et al. | British Library Conference Proceedings | 1998