Systems disclosed herein may be useful for use in a disk brake system. In this regard, a disk brake system may comprise a stator thickness that is less than 15% greater than an end plate thickness and/or pressure plate thickness. Additionally, a disk brake system may further comprise a combination of split friction disks comprising a damping feature and solid friction disks. These split friction disks and/or solid friction disks may be arranged together in any suitable pattern or position within the disk brake system.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Damped heatsink disk brake assembly


    Beteiligte:
    RIEBE GARY C (Autor:in)

    Erscheinungsdatum :

    27.03.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64C AEROPLANES , Flugzeuge



    DAMPED HEATSINK DISK BRAKE ASSEMBLY

    RIEBE GARY C | Europäisches Patentamt | 2017

    Freier Zugriff

    AIRCRAFT BRAKE HEATSINK WEAR LINER

    LINCK JOHN | Europäisches Patentamt | 2020

    Freier Zugriff

    DISK BRAKE ASSEMBLY

    RAVILLA PRASAD / K MATHEWS WINNEY / MOHAN SHANMUGAM et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    DISK BRAKE ASSEMBLY

    RAVILLA PRASAD / K MATHEWS WINNEY / MOHAN SARAVANAN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    DISK BRAKE ASSEMBLY

    RAVILLA PRASAD / K MATHEWS WINNEY / MOHAN SHANMUGAM et al. | Europäisches Patentamt | 2020

    Freier Zugriff