| 摘要 |
The present invention relates to an aircraft bomb fuse. The fuse comprises a safety finger 240 which, in the storage position, prevents the rotation of a wind-power machine 46, primary elastic means urging a displacement of the safety finger 240 from the storage position towards a position of use, in which the finger 240 releases the wind-power machine 46, a flyweight 210 mounted axially slidably in the housing 28 of the fuse between an initial safety position, towards which the flyweight is urged by secondary elastic means 243, and a released position induced during a deceleration phase of the fuse which overcomes the effect of the secondary elastic means and in which the flyweight releases the safety finger. <IMAGE>
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