公开(公告)号：US6121882A

公开(公告)日：2000-09-19

申请号：US246199

申请日：1999-01-04

申请人： Warren K. Jaul ,  Gerhard W. Thielman ,  Michael C. Vogt ,  Rodney M. Harris ,  Jack M. Pakulak

发明人： Warren K. Jaul ,  Gerhard W. Thielman ,  Michael C. Vogt ,  Rodney M. Harris ,  Jack M. Pakulak

IPC分类号： F42B39/20 ,  G08B17/00

CPC分类号： F42B39/20

摘要： A process for indicating the likelihood of cook-off for energetic materials by calculating the heat flux and chemical venting relative to known crial parameters for the energetic materials. The process further may include an alarm.

摘要翻译： 通过计算相对于高能材料的已知关键参数的热通量和化学排放来指示排出高能材料的可能性的过程。 该过程还可以包括警报。

公开(公告)号：US08087229B2

公开(公告)日：2012-01-03

申请号：US11970231

申请日：2008-01-07

申请人： Kenneth J. Wilson ,  Warren K. Jaul ,  Robert G. Burman ,  Shannon L. Fitzpatrick

发明人： Kenneth J. Wilson ,  Warren K. Jaul ,  Robert G. Burman ,  Shannon L. Fitzpatrick

IPC分类号： F02K1/00 ,  F02K1/28

CPC分类号： F42C15/32

摘要： A supersonic combustion apparatus including a fixed geometric nozzle having a converging area, throat, and a diverging area, at least one movable combination of a fuel injector and an oxygen injector where the combined fuel injector and the oxygen injector is located within the divergent area of the fixed geometric nozzle, and an exit plane adjacent and downstream to the diverging area. The exit plane Mach speed is varied by heat addition in the diverging area by introduction of a combustible fuel through the fuel injector and oxygen through the oxygen injector and then axially aligning and positioning the combination of the fuel injector and the oxygen injector along the length of the diverging area to obtain a stabilized flame at the exit plane.

摘要翻译： 一种超音速燃烧设备，包括具有会聚区域，喉部和发散区域的固定几何喷嘴，燃料喷射器和氧气喷射器的至少一个可移动组合，其中组合燃料喷射器和氧气喷射器位于 固定的几何喷嘴，以及与发散区域相邻和下游的出口平面。 通过通过燃料喷射器引入可燃燃料并通过氧气喷射器引入氧气，然后沿燃料喷射器和氧气喷射器的长度轴向对准和定位燃料喷射器和氧气喷射器的组合，使出口平面马赫速度通过在发散区域中的热量加法而变化 发散区域在出口平面处获得稳定的火焰。