公开(公告)号：US4273048A

公开(公告)日：1981-06-16

申请号：US24132

申请日：1979-03-26

Applicant: Michael H. Aley ,  James A. Bowen ,  Cecil A. Glass

Inventor： Michael H. Aley ,  James A. Bowen ,  Cecil A. Glass

IPC: F41H11/12 ,  F42B10/56 ,  F42B12/52 ,  F42B3/00

CPC classification number: F42B10/56 ,  F41H11/12 ,  F42B12/52

Abstract: A fuel-air explosive weapon launched from a remote distance is used for clearing minefields. A set timing pattern in the operation of the minefield clearance round permits varied range through retarding the length of time that a programed sequence of events occurs at the launch site. Upon flight, the round follows a predetermined pattern in deployment of a parachute, firing cloud detonators and initiation of a burster charge. An extendable probe at the front of the round permits detonation at a predetermined level above ground. The descent by parachute provides a relatively stable launching platform for cloud detonators if they are fired prior to the burster charge detonation for dispersal of the fuel-air cloud.

Abstract translation: 从远处发射的燃油爆炸武器用于清雷雷区。 排雷周期运行中的设定时间模式允许通过延迟发射现场发生的编程顺序事件的时间长短来改变范围。 在飞行中，圆形按照预定的方式进行降落伞的部署，发射云雷管并引发爆胎。 在圆形前部的可伸缩探头允许在地面以上预定水平的爆震。 降落伞的下降为云雷管提供了一个相对稳定的发射平台，如果它们在燃烧空气云散布爆炸炸药爆炸之前被射击。

公开(公告)号：US4297949A

公开(公告)日：1981-11-03

申请号：US62395

申请日：1979-07-31

Applicant: Cecil A. Glass ,  Dallas D. Burns

Inventor： Cecil A. Glass ,  Dallas D. Burns

IPC: F41H11/12 ,  F42B12/52 ,  F42C15/184 ,  F42B25/12 ,  F42B15/12

CPC classification number: F42C15/184 ,  F41H11/12 ,  F42B12/52

Abstract: A detonation system for explosive rounds, such as a fuel air explosive, is made by providing a sealed launch tube detonator assembly arrangement. The cloud detonator provides for a booster charge which is attached to a pyro delay detonator. The pyro delay detonator permits the booster charge to be hurled a discrete distance into the fuel air cloud to insure proper cloud detonator position while at the same time waiting an appropriate time interval to permit complete cloud formation. The detonator assembly is self-sealing in its launch tube to prevent gases, which hurl the detonator assembly out of the launch tube, from burning the fuel air cloud. The cloud detonator assembly itself contains unique safety features which will prevent premature partial burning of booster charge.

Abstract translation: 通过提供密封的发射管雷管组件装置来制造用于爆炸性的轮的爆炸系统，例如燃料空气炸药。 云雷管提供附加到火焰延迟雷管的增压装置。 火焰延迟雷管允许增压装置投入到燃料空气云中的离散距离，以确保适当的云雷管位置，同时等待适当的时间间隔以允许完全的云形成。 雷管组件在其发射管中是自密封的，以防止将雷管组件从发射管中推出的气体燃烧燃料空气云。 云雷管组件本身包含独特的安全功能，可防止增压器过早部分燃烧。