Latch and lock mechanism for an aircraft cargo door assembly
AssigneeThe Boeing Company
InventorsJames E. Deviny, Miloslav Puncoch
Life of this patent
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AssigneeThe Boeing Company
InventorsJames E. Deviny, Miloslav Puncoch
Estimating the term…
A latch and lock mechanism for an aircraft cargo door assembly is disclosed. The mechanism is adapted to a cargo door assembly of the type having an outwardly opening, nonplug-type cargo ramp and an inwardly opening, plug-type cargo door hinged to opposite sides of a doorway so as to form a two-part closure member in coplanar alignment with the airplane fuselage when the door assembly is closed. The latch and lock mechanism preferably includes a plurality of latch units that secure the cargo ramp in its closed position. The latch units are connected through a cam-actuated interlock mechanism to the plug-type cargo door. The interlock mechanism is such that the cargo ramp latches can only be actuated when the cargo door is in an open position, and further such that the cargo door cannot be closed unless the cargo ramp latches are in a latched position. The interlock mechanism precludes the possibility of inadvertent unlatching of the cargo ramp while the airplane is pressurized and in flight, and also prevents the possibility of inadvertently leaving the cargo ramp in a closed but unlatched state during pressurization of the cabin.
A latch and lock mechanism for a fuselage door assembly in a pressurizable aircraft, said door assembly having an inwardly opening plug-type closure member and an outwardly opening nonplug-type closure member, comprising:
A latch and lock mechanism for an aircraft fuselage door assembly wherein an outwardly opening nonplug-type closure member and an inwardly opening plug-type closure member are hinged to the aircraft fuselage along opposite sides of a fuselage doorway such that said closure members meet in the midsection of the doorway when the door assembly is closed, comprising:
A latch and lock mechanism for an aircraft cargo door assembly having an inwardly opening cargo door and an outwardly opening cargo ramp, wherein the cargo door and cargo ramp are hinged to the fuselage along opposite sides of a cargo doorway formed in the aircraft fuselage such that the free-swinging ends of the cargo door and cargo ramp approach one another so as to combine to form a closure member in said doorway, comprising a latch body affixed to and extending from fixed structure of the aircraft, said latch body including first and second bores passing therethrough, a lock rod slidably engaged in said first bore and a latch rod slidably enaged in said second bore, said latch body further including a transverse channel therein transecting said first and second bores, and a cylindrical interlock cam slidably engaged for reciprocal movement in said transverse channel, said latch and lock rods including opposing concave cam detents engageable with said interlock cam when said rods are positioned with their respective detents aligned with said channel, said latch rod being operatively connected to latch means for securing said cargo door to said latch body, said latch means and said latch rod being adapted such that said cam detent of said latch rod is aligned with said channel when said latch means is in a latched position, cam actuating means connected to said lock rod, said cam actuating means being responsive to said cargo door to move said lock rod to a position wherein said cam detent of said lock rod is not aligned with said interlock cam when said cargo door is in a closed position, and being further responsive to move said lock rod cam detent into alignment with said interlock cam when said cargo door is opened, the diameter of said interlock cam and the spacing between said bores of said latch body being such that said interlock cam is at all times engaged with at least one of said cam detents of said latch and lock rods.
In a pressurizable aircraft fuselage, mutually cooperable adjoining first and second closure members, the first closure member mounted for opening inwardly and the second closure member mounted for opening outwardly of said fuselage from closed positions sealing said fuselage against loss of pressurization, a latch bolt mechanism operable to secure said second closure member in a closed position, said latch bolt mechanism including push-pull latch actuator rod means operable to actuate said latch bolt mechanism between a latched position securing said second closure member and an unlatched position releasing said second closure member, and cam interlock means for mechanically interlocking said latch bolt mechanism with said first closure member, said cam interlock means being actuated by closure of said first closure member, said cam interlock means operating to prevent the release of said latch bolt mechanism until the first closure member is moved out of closed position.
Dependencies are inferred from the claim text.