Compact thrust bearing assemblies, mechanical assemblies including the compact thrust bearing assemblies, and methods of providing limited rotational motion in a compact thrust bearing assembly are disclosed herein. The thrust bearing assemblies (100) include a plurality of rigid load-bearing structures (110) arranged in a layered stack (120) that defines a first end (130) and an opposed second end (140). The thrust bearing assemblies further include a plurality of rotation-limiting structures (170) configured to restrict relative rotation between adjacent pairs of rigid load-bearing structures. The thrust bearing assemblies also include a first load-receiving surface (132) configured to receive a first thrust load (32) and a second load-receiving surface (142) configured to receive a second thrust load (42). The methods include methods of providing limited rotational motion in a thrust bearing assembly.


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    Title :

    COMPACT THRUST BEARING ASSEMBLIES, MECHANICAL ASSEMBLIES INCLUDING COMPACT THRUST BEARING ASSEMBLIES, AND METHODS OF PROVIDING LIMITED ROTATIONAL MOTION IN A COMPACT THRUST BEARING ASSEMBLY


    Additional title:

    KOMPAKTE AXIALDRUCKLAGERANORDNUNGEN, MECHANISCHE ANORDNUNGEN MIT KOMPAKTEN AXIALDRUCKLAGERANORDNUNGEN UND VERFAHREN ZUR BEREITSTELLUNG VON BEGRENZTER DREHBEWEGUNG IN EINER KOMPAKTEN AXIALDRUCKLAGERANORDNUNG
    ENSEMBLES DE PALIER DE BUTÉE COMPACTS, ASSEMBLAGES MÉCANIQUES COMPRENANT DES ENSEMBLES DE PALIER DE BUTÉE COMPACTS ET PROCÉDÉS DE FOURNITURE D'UN MOUVEMENT DE ROTATION LIMITÉ DANS UN ENSEMBLE DE PALIER DE BUTÉE COMPACT


    Contributors:

    Publication date :

    2019-08-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16C SHAFTS , Wellen / B64C AEROPLANES , Flugzeuge