Closure fasteners – Bolts – Hooked end
Patent
1977-12-05
1979-06-26
Moore, Richard E.
Closure fasteners
Bolts
Hooked end
292DIG49, 292DIG60, E05C 308, E05C 330
Patent
active
041591372
ABSTRACT:
An adjustable, multipivot aircraft panel latch featuring a means for adjusting the latch tension after the panel is installed without the necessity of opening the latch. This is accomplished by an adjustment screw mounted on a yoke member in operative engagement with the latch arm. By the particular arrangement of components, the latch arm may be adjusted relative to a keeper on the aircraft structure by rotating the screw with a conventional drive tool inserted through a small opening in the top of the latch housing.
REFERENCES:
patent: 2750217 (1956-06-01), Landholt
patent: 2927812 (1960-03-01), Smith et al.
patent: 4053177 (1977-10-01), Stammreich et al.
Moore Richard E.
Seeman Thomas A.
Tridair Industries
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