An aircraft cowl arrangement (300) may comprise a first half (310), and a second half (320) rotatable between an open position and a closed position, a first seal coupled to the first half (310), a second seal coupled to the second half (320), and a latch arrangement (350) for preventing relative movement between the first half (310) and the second half (320). The latch arrangement (350) may comprise a tie rod (360) comprising a first end (362) coupled to the first half (310), a second end (364), and a frame (370) having an opening (395) for receiving the second end (364) of the tie rod (360), a latch handle (376) rotatably mounted to the frame (370), and a hook (375) operably coupled to the latch handle (376), wherein the latch handle (376) is configured to move between a first position wherein the hook (375) is engaged with the second end (364) of the tie rod (360) and a second position wherein the hook (375) is disengaged from the second end (364) of the tie rod (360).


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    Title :

    FAN COWL LATCH CONCEPT FOR FUSELAGE MOUNTED POWER PLANT


    Additional title:

    LÜFTERHAUBENVERRIEGELUNGSKONZEPT FÜR EIN RUMPFMONTIERTES TRIEBWERK
    CONCEPT DE VERROUILLAGE DE CAPOT DE VENTILATEUR POUR TURBORÉACTEUR MONTÉE SUR FUSELAGE


    Contributors:

    Publication date :

    2023-01-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / 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



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