Locking system

Aeronautics and astronautics – Landing gear – Retractable

Reexamination Certificate

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C244S1020SS

Reexamination Certificate

active

08061654

ABSTRACT:
A locking system, in particular a locking system for aircraft landing gears. A space-saving, simple construction and little maintenance requirement of the locking system is achieved by at least one electromechanical drive unit, whose torque is transmitted to a drive shaft with a cam disk via axle-crossing transmitting. With the torque, the cam disk can move the locking system from the locked into the unlocked condition.

REFERENCES:
patent: 3652039 (1972-03-01), Lucien
patent: 5288037 (1994-02-01), Derrien
patent: 6811118 (2004-11-01), Collet et al.
patent: 2006/0163426 (2006-07-01), Smith, III

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