Gas turbine engine fan blade containment systems are disclosed. An example fan blade containment system includes a shield to be coupled to an aircraft structure and to at least partially surround a circumference of an aircraft engine. The shield is to be spaced from an outer surface the aircraft engine when the shield is coupled to the aircraft structure. The shield is to form a laminated clevis at an end of the shield. A retention rod is to be positioned in the laminated clevis of the shield. The retention rod is to engage a lug hook of the aircraft structure to anchor the shield to the aircraft structure.


    Access

    Download


    Export, share and cite



    Title :

    Gas turbine engine fan blade containment systems


    Contributors:

    Publication date :

    2019-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / 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



    GAS TURBINE ENGINE FAN BLADE CONTAINMENT SYSTEMS

    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | European Patent Office | 2022

    Free access

    Gas turbine engine fan blade containment systems

    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | European Patent Office | 2020

    Free access

    GAS TURBINE ENGINE FAN BLADE CONTAINMENT SYSTEMS

    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | European Patent Office | 2021

    Free access

    GAS TURBINE ENGINE FAN BLADE CONTAINMENT SYSTEMS

    FRACCHIA CARLOS ANGELO / JOST KAREN M / HIGGINS MARK DAVID et al. | European Patent Office | 2020

    Free access

    Fan blade containment system for gas turbine engine

    FINLAYSON JAMES A / REED JULIAN M | European Patent Office | 2021

    Free access