In some aspects, an aircraft engine thrust reverser lock system includes a pin-capturing member. The pin-capturing member includes a body that is rotatable about an axis defined by a pivot extending through the body. The body includes an interior surface that defines a slot. The slot has an opening that is sized to receive a pin into the slot. One side of the slot includes a protruded sidewall surface that protrudes into the slot toward an another sidewall surface of the slot. The protruded sidewall surface defines an apex between the open and closed ends of the slot. Between the apex and the closed end of the slot, the protruded sidewall surface faces the rotational axis.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Engine thrust reverser lock


    Beteiligte:

    Erscheinungsdatum :

    2017-10-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Engine Thrust Reverser Lock

    WILLETT KENNETH / MEARS JOHN STEPHEN / CONWAY GEORGE et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft engine thrust reverser

    Emerald Group Publishing | 1998


    Thrust reverser actuator with primary lock

    WINGETT PAUL T / CHAKKERA KEVIN K / VAUGHAN RON et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    LOCK SYSTEM FOR A THRUST REVERSER

    TREZIERES MARLENE MARCELLE SIMONE | Europäisches Patentamt | 2023

    Freier Zugriff

    TRANSLATING LOCK FOR PIVOT DOOR THRUST REVERSER

    GHANDOUR IMAD / HUYNH KEN V | Europäisches Patentamt | 2019

    Freier Zugriff