Automatic release and ejection locking mechanism
AssigneeR. Alkan & Cie
InventorsGeorges E. Bourrie, Robert Marc Lensel
Life of this patent
Estimating the term…
Abstract
This automatic release and ejection locking mechanism for said equipment boxes, notably for aircraft comprises locking balls releasable from their locked condition by means of a piston constantly urged by a coiled compression spring to its release position. The locking means are held against the force of the ejection spring by means of an effort scalingdown device, so that the force to be applied to said device for keeping the locking action may be very moderate and the release can be obtained by reducing or cancelling the low retaining force exerted on the effort scaling-down device, for example by means of electromagnetic release means, in combination or not with a permanent magnet. (FIG. 1)
Claims7
An automatic release and ejection mechanism, suitable particularly for the closure of safety equipment boxes on aircraft, comprising:
- i. a fixed member for securing to a box, said fixed member defining a cylinder space, said fixed member having in its wall a plurality of radial openings,
- ii. a latch member for securing to the closure of the box, said latch member having a recess adapted to receive a portion of said fixed member including said radial openings, said latching member having in its recess a radial groove which, when the latch member is fully engaged on the fixed member, is radially aligned with said plurality of openings,
- iii. a set of balls disposed one in each of said radial openings
- iv. a piston longitudinally slidable in the cylinder space of said fixed member, said piston having at its end adjacent said openings a first portion of a diameter which, when abutted by said balls, permits said balls to lie wholly within said fixed member, said piston having a second portion of a greater diameter which, when abutted by said balls, causes said balls to protrude from said fixed member into the radial groove of the latch member for locking the latch member against withdrawal longitudinally off the fixed member
- v. resilient loading means positioned to act between said latch member and said piston, said loading means being stressed by engagement of the latch member onto the fixed member, the force exerted by the loading means urging the piston in the direction to permit release of the balls from the groove of the latch member
- vi. control means movably mounted on said fixed member and coupled to said piston, said control means having a first locking position of movement in which it prevents longitudinal movement of the piston by said loading means, said control means having a second releasing position of movement in which said piston is freed to be moved longitudinally by said loading means
- vii. means for retaining said control means releasably in said locking position.
Dependencies are inferred from the claim text.