Aeronautical conveying and dropping device
AssigneeARESIA-Valenton
InventorsValentin LEBRU, Frédéric GANDON
Life of this patent
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Abstract
An aeronautical conveying and dropping device for a missile to be released, comprising at least a frame, a hook capable of retaining the missile to be released, a deformable parallelogram mechanism having an axis secured to the frame, two axes secured to the hook and a free axis arranged in the frame, a first cam mounted so as to rotate about an axis fixed in the frame and having a position for locking the deformable parallelogram mechanism by contact with a bearing mounted on the free axis of the deformable parallelogram mechanism, and an unlocking position, and a member for preloading the first cam in the locking position.
Claims15
An aeronautical conveying and dropping device for an aeronautical vehicle to be released, comprising:
- a frame,
- a hook capable of holding the aeronautical vehicle to be released,
- a deformable parallelogram mechanism having an axis secured to the frame, two axis secured to the hook and a free axis, arranged in the frame
- a first cam mounted so as to rotate about an axis fixed in the frame and having a position for locking the deformable parallelogram mechanism contact with a bearing mounted on the free axis of the deformable parallelogram mechanism, and an unlocking position, and
- a member for preloading the first cam in the locking position.
Dependencies are inferred from the claim text.