CONSIDERATIONS of aircraft-engine installation singular to the inverted, in-line, aircooled type of engine are presented here in the light of current engineering development in this field. Items of this installation technique discussed are: cooling aspects, cowling arrangements, oil cooling systems, induction systems, engine mounts, and exhaust systems.Much of the information presented is based upon experience gained from wind tunnel and flight tests with Ranger engines.The application of design considerations discussed under the cooling aspects of the aircooled engine has been proved satisfactory in flight test operations.Latest methods of treatment of these factors are described. Substantial advancement has been made in handling the ever-present cooling problem common to all types of engines. This has been achieved by applying the design knowledge gained through considerable wind tunnel and flight research.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Factors Pertaining to Installation of Inverted, In-Line AIRCOOLED AIRCRAFT ENGINES


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    HAMMEN, T. F. (Autor:in) / ROWLEY, W. H. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    01.01.1946




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Aircooled engines for vehicles

    Bachle, C.F. | Engineering Index Backfile | 1949


    AIRCOOLED ENGINES for Automotive Vehicles

    RICKER, CHESTER S. | SAE Technical Papers | 1944


    EUROPEAN DEVELOPMENTS IN SMALL AIRCOOLED ENGINES

    MEYER, W. E. | SAE Technical Papers | 1957


    Aircooled diesel engines for amphibious hovercraft

    Sonthey,J. | Kraftfahrwesen | 1984


    European developments in small aircooled engines

    Meyer, W.E. | Engineering Index Backfile | 1957