Preloaded latch
AssigneeThe Boeing Company
InventorAlfred W. Harris
Life of this patent
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AssigneeThe Boeing Company
InventorAlfred W. Harris
Estimating the term…
A housing (14, 24) is mounted on each of two bodies. Each housing (14, 24) has an inwardly extending strut portion (16, 26) with an inner mating surface (18, 28). The mating surfaces (18, 28) are urged together to react a preload on the latch (12). The preload is provided by the tensioned engagement of a draw hook (62) and a catch pin (106). The draw hook (62) is pivotably mounted on a lever (42) that is pivotably mounted on housing (14). The catch pin (106) is slidably mounted on housing (24). The pivot axes of hook (62) and lever (42) are positioned to provide over-center latching action. A carrier (100) for the catch pin (106) has a shaft (102) that is threadedly engaged by a hollow internally threaded bolt (112). The outer end of the bolt (112) is axially engaged by a screw driver to adjust the longitudinal position of the carrier (100) along the load path to adjust the preload tensioning. Rotation of the carrier (100) is prevented by engagement of the carrier (100) in slots (142) in housing (24). The load path is generally perpendicular to the mounting surfaces of the bodies.
For use in an aircraft component having spaced-apart walls that include opposed movable panels, latching apparatus for securing the panels in flush positions, comprising:
Over-center latching apparatus for securing first and second bodies together, at least one of said bodies being movable with respect to the other, comprising:
In a latch mechanism of the type having a latch hook and a catch that engages the latch hook, with the engagement of the hook and catch being tensioned along a load path, the improvement comprising:
Dependencies are inferred from the claim text.