A latch assembly for a reduced pressure panel in an aircraft includes a base and a rocker arm hinged to the base and pivotable relative to the base about a hinge axis between a latched position and an unlocked position. A load pin secured to the rocker arm has a pin axis at a fixed distance from the hinge axis. A spring secured to the base is positioned to apply a spring force against the rocker arm when the rocker arm is pivoted from the latched position to the unlocked position. A bracket securable to the pressure relief panel defines a slot that retains the load pin when the rocker arm is in the latched position. The load pin is movable in the slot in a latched position under relative movement of the bracket and the base with the rocker arm, and the load pin leaves the slot when the rocker arm pivots to an unlocked position.
一种闩锁组件,用于飞机中的减压面板,该闩锁组件包括底座和摇动臂,该摇动臂铰接到底座并可相对于底座围绕铰接轴线在闩锁位置和解锁位置之间枢转。固定至摇动臂的载荷销具有距铰接轴线一固定距离的销轴线。固定至底座的弹簧定位成当摇动臂从闩锁位置枢转至解锁位置时抵靠摇动臂施加弹簧力。可固定至减压面板的支架限定槽,当摇动臂处于闩锁位置时,该槽保持载荷销。载荷销能在闩锁位置中在支架和底座与摇动臂的相对运动下在槽中移动,并且当摇动臂枢转至解锁位置时,载荷销离开槽。
LATCH ASSEMBLY AND AIRCRAFT HAVING THE SAME
闩锁组件和具有该闩锁组件的飞机
2022-09-27
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT LATCH APPARATUS HAVING FLOATING STRIKE ASSEMBLY
European Patent Office | 2020
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