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公开(公告)号：USD470458S1
公开(公告)日：2003-02-18
申请号：US29140472
申请日：2001-04-17
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公开(公告)号：US08895908B2
公开(公告)日：2014-11-25
申请号：US13376846
申请日：2011-04-07
摘要： A low cost, lightweight frangible wing slot seal can be applied to a guidance wing slot of a folding fin aerial rocket or missile, providing a barrier against exposure of internal missile components to external contaminants, while allowing unhindered deployment of missile guidance wings simply by bursting through the seals. The simple design is nearly foolproof, and has no impact the likelihood of weapon failure. The seal is a flexible sheet which is sufficiently thin so as not to exceed the required volume envelope of the missile. The sheet includes a burst seam, which is breached when impacted by the leading edge of a deploying wing. No additional wing deployment force is required, and after deployment the seal has minimal impact on the aerodynamic performance of the wing.
摘要翻译： 低成本，轻量级的易碎翼槽密封件可应用于折叠式飞机空中火箭或导弹的导向翼槽，提供防止内部导弹部件暴露于外部污染物的屏障，同时允许简单地通过爆裂而不受阻挡地部署导弹引导翼 通过印章。 简单的设计几乎是万无一失的，对武器失效的可能性没有影响。 密封件是足够薄的柔性片材，以便不超过导弹的所需体积包络线。 该片材包括爆裂缝，当爆炸缝由部署翼的前缘撞击时，该缝隙被破坏。 不需要额外的机翼部署力，在部署之后，密封件对机翼的空气动力性能影响最小。
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公开(公告)号：US5785229A
公开(公告)日：1998-07-28
申请号：US79338
申请日：1993-06-18
申请人： John R. Franzini
发明人： John R. Franzini
CPC分类号： B25C1/10 , B23D15/145 , B25B27/0085 , B25C1/14 , B25C1/18
摘要： An adapter is provided that includes a housing, a striker, a spring, a lever, and a hook. The striker is movably mounted in the housing and biased by the spring towards a firing position with a front end extending into an aperture at the front of the housing. The lever is pivotally connected to the exterior of the housing and the hook. The hook extends through an aperture in the housing and is connected to the striker such that movement of the lever will move the striker. The front end of the housing has a connector for connecting the housing to a rear end of a powder actuated connecting tool.
摘要翻译： 提供了一种适配器，其包括壳体，撞针，弹簧，杠杆和钩。 撞击器可移动地安装在壳体中并且被弹簧偏压到击发位置，前端延伸到壳体前部的孔中。 杠杆枢转地连接到壳体和钩的外部。 钩延伸穿过壳体中的孔并且连接到撞针，使得杠杆的运动将移动撞针。 壳体的前端具有用于将壳体连接到粉末致动连接工具的后端的连接器。
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公开(公告)号：US20140312575A1
公开(公告)日：2014-10-23
申请号：US13376846
申请日：2011-04-07
IPC分类号： F16J15/00
摘要： A low cost, lightweight frangible wing slot seal can be applied to a guidance wing slot of a folding fin aerial rocket or missile, providing a barrier against exposure of internal missile components to external contaminants, while allowing unhindered deployment of missile guidance wings simply by bursting through the seals. The simple design is nearly foolproof, and has no impact the likelihood of weapon. failure. The seal is a flexible sheet which is sufficiently thin so as not to exceed the required volume envelope of the missile. The sheet includes a burst seam, which is breached when impacted by the leading edge of a deploying wing. No additional wing deployment force is required, and after deployment the seal has minimal impact on the aerodynamic performance of the wing.
摘要翻译： 低成本，轻量级的易碎翼槽密封件可应用于折叠式飞机空中火箭或导弹的引导翼槽，提供防止内部导弹部件暴露于外部污染物的屏障，同时允许简单地通过爆裂而不受阻挡地部署导弹引导翼 通过印章。 简单的设计几乎是万无一失的，对武器的可能性没有影响。 失败。 密封件是足够薄的柔性片材，以便不超过导弹的所需体积包络线。 该片材包括爆裂缝，当爆炸缝由部署翼的前缘撞击时，该缝隙被破坏。 不需要额外的机翼部署力，在部署之后，密封件对机翼的空气动力性能影响最小。
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