Locking device for a band or the like, subject to a tensile forc

Aeronautics and astronautics – Aircraft structure – Details

Patent

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Details

244158R, 244120, 102377, 292113, 292DIG49, 24 68BT, 24273, B64G 164

Patent

active

051976951

ABSTRACT:
A locking device for a band or the like comprising a housing having one end fastened to a first portion of the band. The housing extends in the direction of the prevailing tensile force and is formed with a guide for guiding a link means. This comprises a fastening element fastened at its first end to the second portion of the band and at its second end journally connected to a second link at a distance from its first end. The second link is, at its first end, journaled around an axis provided in the housing transverse to the longitudinal direction of the housing. The locking device also comprises a third link journaled at the first end of the housing and a dowel element which, l via the third link, is able to prevent the second link from being turned around the axis to a position where it is released from the axis so that the locking device is opened.

REFERENCES:
patent: 759305 (1904-05-01), Nunn
patent: 815558 (1906-03-01), Rosier
patent: 892197 (1908-06-01), Umpleby et al.
patent: 1230146 (1917-01-01), Frieze
patent: 3844594 (1974-10-01), Romberg
patent: 4715565 (1987-12-01), Wittmann

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