An aircraft cowl arrangement may comprise a first half, and a second half rotatable between an open position and a closed position, a first seal coupled to the first half, a second seal coupled to the second half, and a latch arrangement for preventing relative movement between the first half and the second half. The latch arrangement may comprise a tie rod comprising a first end coupled to the first half, a second end, and a frame having an opening for receiving the second end of the tie rod, a latch handle rotatably mounted to the frame, and a hook operably coupled to the latch handle, wherein the latch handle is configured to move between a first position wherein the hook is engaged with the second end of the tie rod and a second position wherein the hook is disengaged from the second end of the tie rod.


    Access

    Download


    Export, share and cite



    Title :

    Fan cowl latch concept for fuselage mounted power plant


    Contributors:

    Publication date :

    2020-09-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / E05B LOCKS , Schlösser / E05C Riegel oder Feststellvorrichtungen für Flügel, insbesondere für Türen oder Fenster , BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS



    FAN COWL LATCH CONCEPT FOR FUSELAGE MOUNTED POWER PLANT

    RATAJAC ALEKSANDAR | European Patent Office | 2023

    Free access

    FAN COWL LATCH CONCEPT FOR FUSELAGE MOUNTED POWER PLANT

    RATAJAC ALEKSANDAR | European Patent Office | 2019

    Free access

    FAN COWL LATCH

    SITSON KRISTIAN / LEE JOHN J / DENG YIBIN | European Patent Office | 2016

    Free access

    Fan cowl latch

    SITSON KRISTIAN / LEE JOHN J / DENG YIBIN | European Patent Office | 2018

    Free access

    Fan cowl balking latch

    LEE JOHN J / SITSON KRISTIAN / DENG YIBIN | European Patent Office | 2018

    Free access