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    • 6. 发明授权
    • Omnidirectional spring mass initiator (u)
    • OMNIDIRECTIONAL SPRING MASS INITIATOR(U)
    • US3631804A
    • 1972-01-04
    • US3631804D
    • 1968-08-20
    • US NAVY
    • ANDERSON MATTHEW EDAVIS EDWARD J
    • F42C1/00F42C1/06F42C19/06
    • F42C19/06F42C1/00F42C1/06
    • An omnidirectional spring mass initiator system for use in a weapon system responsive to any direction of weapon-target impact comprising a chamber of any geometric shape, said chamber having at least one opening into said chamber; a flexible support means having a secured end and another end which is operatively positioned for insertion into the chamber through said at least one opening; and an accelerometer mass-contacting means attached to said other end of the support means. The contacting means is responsive to deceleration and, when inserted into the chamber, positioned in the center, thereof, so as to be capable of contacting some portion of the inner surface of the chamber in response to the deceleration of the system caused by any direction of weapon and target impact. The entire inner surface of the chamber is coated with a contact-sensitive lining such that when the contacting means comes into contact with the contact-sensitive lining a resultant response occurs which initiates the fuse mechanism.
    • 一种用于武器系统的全向弹簧质量引发器系统,其响应武器 - 目标撞击的任何方向,包括任何几何形状的腔室,所述腔室具有至少一个进入所述腔室的开口; 柔性支撑装置具有固定端,另一端可操作地定位成通过所述至少一个开口插入到所述室中; 以及附接到所述支撑装置的所述另一端的加速度计质量接触装置。 接触装置响应于减速,并且当插入到腔室中时,其位于其中心,以便响应于由任何方向引起的系统的减速度而能够接触室的内表面的一些部分 的武器和目标影响。 室的整个内表面涂覆有接触敏感衬里,使得当接触装置与接触敏感衬里接触时,产生引发熔丝机构的结果响应。
    • 8. 发明授权
    • Detonating fuse for bombs and the like
    • 用于炸药和类似物的保险丝
    • US3417701A
    • 1968-12-24
    • US63473567
    • 1967-04-28
    • FORGES DE ZEEBRUGGE SA
    • BODINAUX GASTON JEAN O
    • F42C1/00F42C1/06F42C9/10F42C15/18F42C15/24F42C15/31
    • F42C9/10F42C1/00F42C1/06F42C15/18F42C15/24F42C15/31
    • 1,179,298. Projectile fuzes. FORGES DE ZEEBRUGGE S.A. 29 June, 1967 [28 Oct., 1966], No. 30133/67. Heading F3A. Fuze for a bomb, comprises a detonator (not shown) carried in a pivotable carrier 14, a first locking element 13 which engages the carrier in a safety position but is displaced a predetermined time after release of the bomb, and a second locking element 26 which engages the carrier in the safety position but is displaced after impact of the bomb by the glass resulting from the combustion of a delay charge 39, the carrier then being swung by a spring into a position where combustion of the remaining part of the delay charge causes firing of the detonator. The first locking element is held against axial rotation by engagement with a pin but is displaced axially by a spring when a recess in the end face 11 of a rotatable striker guide 8 is aligned with the locking element, following shearing of a pin 19 which extends into a circumferential recess in the end face. The guide 8 is rotated by a striker 4 driven through reduction gearing 3. A spring loaded pin locks the first locking element in the inactive position. The striker is formed with an inertia mass 5 and is thrown against a primer 40 upon impact of the bomb. The second locking element is displaced by combustion gases fed into a chamber 29, and is held in the inactive position by engagement of its head 31 in a capsule 33.