TODAY, aircraft gas turbine engines are being developed to give over 28,000 lb. thrust and, while low-pressure compressor casings can be made from a magnesium-alloy casting, the operating conditions of high-pressure compressors demand high-tcnsilc stainless steel. The operating temperature of a high-pressure compressor, for example, may be about 450 deg. C, and certain specifications call for minimum ultimate tensile strengths of 135,000 lb./sq. in. with 10 percent minimum elongation at room temperature, with appropriate stress-rupture and creep properties at elevated temperatures.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Producing Centrifugal Castings for Gas Turbine Compressor Casings


    Untertitel :

    Details of the Firth-Vickers' Programme, Sponsored by the Ministry of Aviation, Which Has Resulted in Substantial Savings of Time and Money Following the Adoption of the ‘Casting to Shape’ Techniques


    Erschienen in:

    Erscheinungsdatum :

    01.10.1962


    Format / Umfang :

    2 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    CENTRIFUGAL COMPRESSOR-TURBINE BACK-TO-BACK

    SADIK ASIF MOHAMMAD / FONTAINE JONATHAN LEOPOLD NUTZATI | Europäisches Patentamt | 2025

    Freier Zugriff


    CENTRIFUGAL COMPRESSOR

    OKUMA TAITO | Europäisches Patentamt | 2023

    Freier Zugriff

    Centrifugal compressor

    OKUMA TAITO | Europäisches Patentamt | 2025

    Freier Zugriff