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).
FAN COWL LATCH CONCEPT FOR FUSELAGE MOUNTED POWER PLANT
LÜFTERHAUBENVERRIEGELUNGSKONZEPT FÜR EIN RUMPFMONTIERTES TRIEBWERK
CONCEPT DE VERROUILLAGE DE CAPOT DE VENTILATEUR POUR TURBORÉACTEUR MONTÉE SUR FUSELAGE
2023-01-25
Patent
Electronic Resource
English