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公开(公告)号：US5565645A
公开(公告)日：1996-10-15
申请号：US427616
申请日：1995-04-24
CPC分类号： F42B4/26
摘要： An infrared decoy flare having enhanced infrared intensity is disclosed. The flare includes a case in which an infrared illuminant composition is disposed. The bore diameter and length of the case are advantageously selected to be compatible with preexisting chaff dispensers and their cartridges located on aircraft. The illuminant composition, the nozzle throat area, the geometry of the illuminant composition, and the volume of the combustion chamber are selected such that combustion of the illuminant composition results in an unstable combustion condition during the first second of combustion, thereby increasing the peak intensity of the radiation emitted by the propellant. Preferably, the flare is configured such that the unstable combustion occurs during the first 0.2 to 0.5 seconds of combustion of the illuminant composition.
摘要翻译： 公开了具有增强的红外线强度的红外诱饵火炬。 火炬包括设置红外光源组合物的情况。 壳体的孔直径和长度有利地被选择为与位于飞机上的预先存在的谷壳分配器及其盒相容。 选择发光体组合物，喷嘴喉部区域，发光体组合物的几何形状和燃烧室的体积，使得发光体组合物的燃烧在燃烧的第一秒期间导致不稳定的燃烧状态，从而增加峰值强度 的推进剂发射的辐射。 优选地，所述火炬配置成使得在所述发光体组合物的燃烧的前0.2至0.5秒期间发生不稳定的燃烧。
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公开(公告)号：US5996502A
公开(公告)日：1999-12-07
申请号：US863399
申请日：1997-05-27
摘要： An aerodynamically stable, kinematic flare having an enhanced plume signature is disclosed. The flare includes a housing with a flare illuminant disposed within the housing. A primary nozzle is configured in the aft wall of the housing. Four secondary nozzles are configured in the aft end of the side wall of the housing and are positioned aft of the center of gravity of the flare. At least two of the secondary nozzles comprise off-center nozzles having a longitudinal axis which does not extend through the longitudinal axis of the flare. A shroud is attached to the housing and deploys to an extended position upon combustion of the illuminant. The shroud is configured with holes which correspond in size and position to each of the secondary nozzles when the shroud is in its extended position. The primary and secondary nozzles are sized and positioned to spin stabilize the flare during combustion of the illuminant.
摘要翻译： 公开了具有增强的羽流签名的空气动力学稳定的运动火炬。 火炬包括具有设置在壳体内的耀斑光源的壳体。 主喷嘴配置在壳体的后壁上。 四个二次喷嘴构造在壳体的侧壁的后端，并且位于火炬重心的后方。 至少两个次级喷嘴包括偏心中心喷嘴，其具有不延伸穿过火炬的纵向轴线的纵向轴线。 护罩附接到壳体并且在发光体燃烧时展开到延伸位置。 当护罩处于其延伸位置时，护罩被配置有在尺寸和位置上对应于每个次级喷嘴的孔。 主喷嘴和次喷嘴的尺寸和位置可以在发光体的燃烧期间旋转稳定火炬。
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公开(公告)号：US5763818A
公开(公告)日：1998-06-09
申请号：US705193
申请日：1996-08-29
CPC分类号： F42C19/0838 , F42B4/26 , F42C15/34
摘要： A decoy flare ignition system is disclosed which includes an ignition initiator disposed at the aft end of the flare housing. An illuminant igniter is positioned in direct contact with the flare illuminant. The illuminant igniter includes at least one illuminant igniter pellet selected such that the firing of the ignition initiator triggers combustion of the illuminant igniter pellet if the safe-and-initiation device has been actuated. The igniter pellet is preferably configured as a circular cylindrical shell and is positioned over the bore of the flare illuminant.
摘要翻译： 公开了一种诱饵火炬点火系统，其包括设置在火炬舱后端的点火启动器。 光源点火器与火炬照明器直接接触。 照明点火器包括至少一个选择的照明器点火器颗粒，使得如果已启动安全启动装置，点火启动器的点火会触发照明器点火器颗粒的燃烧。 点火器颗粒优选地构造为圆柱形壳体并且被定位在火炬照明器的孔上。
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公开(公告)号：US5654522A
公开(公告)日：1997-08-05
申请号：US495716
申请日：1995-06-27
摘要： An aerodynamically stable, kinematic flare having an enhanced plume signature is disclosed. The flare includes a housing with a flare illuminant disposed within the housing. A primary nozzle is configured in the aft wall of the housing. Four secondary nozzles are configured in the aft end of the side wall of the housing and are positioned aft of the center of gravity of the flare. At least two of the secondary nozzles comprise off-center nozzles having a longitudinal axis which does not extend through the longitudinal axis of the flare. A shroud is attached to the housing and deploys to an extended position upon combustion of the illuminant. The shroud is configured with holes which correspond in size and position to each of the secondary nozzles when the shroud is in its extended position. The primary and secondary nozzles are sized and positioned to spin stabilize the flare during combustion of the illuminant.
摘要翻译： 公开了具有增强的羽流签名的空气动力学稳定的运动火炬。 火炬包括具有设置在壳体内的耀斑光源的壳体。 主喷嘴配置在壳体的后壁上。 四个二次喷嘴构造在壳体的侧壁的后端，并且位于火炬重心的后方。 至少两个次级喷嘴包括偏心中心喷嘴，其具有不延伸穿过火炬的纵向轴线的纵向轴线。 护罩附接到壳体并且在发光体燃烧时展开到延伸位置。 当护罩处于其延伸位置时，护罩被配置有在尺寸和位置上对应于每个次级喷嘴的孔。 主喷嘴和次喷嘴的尺寸和位置可以在发光体的燃烧期间旋转稳定火炬。
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5.发明授权
公开(公告)号：US4137255A
公开(公告)日：1979-01-30
申请号：US870773
申请日：1978-01-19
IPC分类号： C07C77/02
CPC分类号： C07C201/02 , C06B21/0091
摘要： A process for the separation of nitroglycerin from mixtures of nitroglycerin and diethylene glycol diluent which avoids the presence of undiluted nitroglycerin is disclosed. The process avoids the hazards inherent in handling undiluted nitroglycerin.
摘要翻译： 公开了一种从硝酸甘油和二甘醇稀释剂的混合物中分离硝酸甘油的方法，其避免了未稀释的硝酸甘油的存在。 该过程避免处理未稀释的硝酸甘油所固有的危害。
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公开(公告)号：US5610364A
公开(公告)日：1997-03-11
申请号：US497277
申请日：1995-06-30
CPC分类号： F42C19/0807 , F42B12/70 , F42B4/26
摘要： A decoy flare is disclosed which includes illuminant disposed within a housing. A shroud is slidably attached to the housing for deployment from a retracted position to an extended position. A plug is attached to the aft end of the shroud and is configured with a radially beveled, nozzle-contacting surface. The plug is positioned and configured to sealingly engage the nozzle when the shroud is in the retracted position and to disengage the nozzle upon deployment of the shroud to the extended position. The plug is configured with a plume-contacting surface positioned at an angle to the path of the plume when the shroud is in the extended position for enhancing the cross-sectional area of the plume of the flare.
摘要翻译： 公开了一种引诱装置，其包括设置在壳体内的发光体。 护罩可滑动地附接到壳体，用于从缩回位置展开到延伸位置。 插头附接到护罩的后端，并且构造为具有径向倾斜的喷嘴接触表面。 塞子定位和构造成当护罩处于缩回位置时密封地接合喷嘴，并且在将护罩展开到延伸位置时使塞子脱离接头。 当护罩处于延伸位置时，塞子构造有与羽流的路径成一定角度的羽流接触表面，以增强火炬的羽流的横截面积。
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