Thermal barrier coatings for substrates comprising titanium. The thermal barrier coating may include a bond layer, an insulating layer, and a sealant layer. The bond layer may include titanium, a titanium alloy, an intermetallic compound of titanium, and/or a titanium metal matrix composite. The bond layer may have a superlattice structure having a periodically repeating group of layers. Methods for producing the thermal barrier coatings and articles of manufacture employing the thermal barrier coatings.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Thermal protection system for lightweight hypersonic missile fin


    Beteiligte:

    Erscheinungsdatum :

    2022-04-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64G Raumfahrt , COSMONAUTICS / C23C Beschichten metallischer Werkstoffe , COATING METALLIC MATERIAL



    THERMAL PROTECTION SYSTEM FOR LIGHTWEIGHT HYPERSONIC MISSILE FIN

    STINNETT THOMAS | Europäisches Patentamt | 2021

    Freier Zugriff

    Thermal protection system for lightweight hypersonic missile fin

    STINNETT THOMAS CHRISTIAN | Europäisches Patentamt | 2022

    Freier Zugriff

    THERMAL PROTECTION SYSTEM FOR LIGHTWEIGHT HYPERSONIC MISSILE FIN

    STINNETT THOMAS CHRISTIAN | Europäisches Patentamt | 2021

    Freier Zugriff

    Thermal protection system for lightweight hypersonic missile fin

    THOMAS CHRISTIAN STINNETT | Europäisches Patentamt | 2023

    Freier Zugriff

    Hypersonic Missile Propulsion System

    R. R. Kazmar | NTIS | 1998