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1. 发明申请

US20110023449A1 Insensitive Rocket Motor 有权
标题翻译：不敏感火箭发动机
公开(公告)号：US20110023449A1
公开(公告)日：2011-02-03
申请号：US12261905
申请日：2008-10-30
申请人： Richard D. Loehr , Gerald M. Turner , Jeremy C. Danforth
发明人： Richard D. Loehr , Gerald M. Turner , Jeremy C. Danforth
IPC分类号： F02K9/26
CPC分类号： F02K9/18 , F02K9/22 , F02K9/26
摘要： There is disclosed a solid fuel rocket motor including a center-perforated solid fuel grain. The solid fuel grain may be adapted to burn outwardly from a center surface facing the center perforation when ignited by a primary igniter during a normal mode of operation. The solid fuel grain may be further adapted to burn longitudinally from an end face when ignited by a secondary igniter during a safety mode of operation.
摘要翻译：公开了一种固体燃料火箭发动机，其包括中心穿孔的固体燃料颗粒。固体燃料颗粒可以适于在正常操作模式期间被主要点火器点燃时从面向中心穿孔的中心表面向外燃烧。固体燃料颗粒可以进一步适于在安全操作模式期间被二次点火器点燃时从端面纵向燃烧。

2. 发明申请

US20100282116A1 Base Drag Reduction Fairing 有权
标题翻译：基础减速整流罩
公开(公告)号：US20100282116A1
公开(公告)日：2010-11-11
申请号：US12463260
申请日：2009-05-08
申请人： Kevin R. Greenwood , James D. Streeter , Jeremy C. Danforth , Timothy A. Yoder
发明人： Kevin R. Greenwood , James D. Streeter , Jeremy C. Danforth , Timothy A. Yoder
IPC分类号： F42B10/44 , B32B1/08
CPC分类号： F42B10/50 , F42B10/38 , F42B10/42 , F42B10/44 , Y10T428/13
摘要： A projectile may include a base drag reduction fairing preform adapted to be plastically deformed into a base drag reduction fairing after the projectile is launched from a gun barrel.
摘要翻译：抛射体可以包括底座减阻整流罩预制件，其适用于在从枪管发射抛射体之后塑性变形成基座减速整流罩。

3. 发明申请

US20120269633A1 CLOSED GAS GENERATOR AND MICRO POWER UNIT INCLUDING THE SAME 有权
标题翻译：封闭式气体发生器和微功率单元，包括它们
公开(公告)号：US20120269633A1
公开(公告)日：2012-10-25
申请号：US13089441
申请日：2011-04-19
申请人： Jeremy C. Danforth , Richard D. Loehr , Kevin P. Murphy
发明人： Jeremy C. Danforth , Richard D. Loehr , Kevin P. Murphy
IPC分类号： B64D27/24 , H02K7/18 , H02J7/00 , F02K9/62 , F02K1/00
CPC分类号： F02K9/00 , B64C2201/042 , F02K9/42 , F02K9/425 , F02K9/50 , F02K9/52 , F02K9/68 , H02J7/00 , H02K7/1823
摘要： A gas generator assembly includes a propellant chamber housing an amine based propellant. A reaction chamber is coupled with the propellant chamber. The reaction chamber includes a reaction chamber housing, and a porous reaction matrix within the reaction chamber housing. The reaction matrix includes a catalyzing agent, and the catalyzing agent is configured to non-combustibly catalyze the amine based propellant into one or more pressurized gases. An injector is in communication with the propellant chamber. The injector is configured to deliver the amine based propellant to the porous reaction matrix. A discharge nozzle is coupled with the reaction chamber and is configured to accelerate and discharge the one or more pressurized gases. In one example, the gas generator is coupled with one or more of an impulse turbine assembly and an electric generator to form a micro power unit.
摘要翻译：气体发生器组件包括容纳胺基推进剂的推进剂室。反应室与推进剂室结合。反应室包括反应室壳体和反应室壳体内的多孔反应基质。反应基质包括催化剂，并且催化剂被配置为不可燃地将胺基推进剂催化成一种或多种加压气体。喷射器与推进剂室连通。喷射器构造成将胺基推进剂输送到多孔反应基质。排放喷嘴与反应室联接并且构造成加速和排出一个或多个加压气体。在一个示例中，气体发生器与脉冲涡轮机组件和发电机中的一个或多个耦合以形成微动力单元。

4. 发明授权

US08636247B2 Closed gas generator and micro power unit including the same 有权
标题翻译：封闭式气体发生器和微型动力装置相同
公开(公告)号：US08636247B2
公开(公告)日：2014-01-28
申请号：US13089441
申请日：2011-04-19
申请人： Jeremy C. Danforth , Richard D. Loehr , Kevin P. Murphy
发明人： Jeremy C. Danforth , Richard D. Loehr , Kevin P. Murphy
IPC分类号： B64C15/00
CPC分类号： F02K9/00 , B64C2201/042 , F02K9/42 , F02K9/425 , F02K9/50 , F02K9/52 , F02K9/68 , H02J7/00 , H02K7/1823
摘要： A gas generator assembly includes a propellant chamber housing an amine based propellant. A reaction chamber is coupled with the propellant chamber. The reaction chamber includes a reaction chamber housing, and a porous reaction matrix within the reaction chamber housing. The reaction matrix includes a catalyzing agent, and the catalyzing agent is configured to non-combustibly catalyze the amine based propellant into one or more pressurized gases. An injector is in communication with the propellant chamber. The injector is configured to deliver the amine based propellant to the porous reaction matrix. A discharge nozzle is coupled with the reaction chamber and is configured to accelerate and discharge the one or more pressurized gases. In one example, the gas generator is coupled with one or more of an impulse turbine assembly and an electric generator to form a micro power unit.
摘要翻译：气体发生器组件包括容纳胺基推进剂的推进剂室。反应室与推进剂室结合。反应室包括反应室壳体和反应室壳体内的多孔反应基质。反应基质包括催化剂，并且催化剂被配置为不可燃地将胺基推进剂催化成一种或多种加压气体。喷射器与推进剂室连通。喷射器构造成将胺基推进剂输送到多孔反应基质。排放喷嘴与反应室联接并且构造成加速和排出一个或多个加压气体。在一个示例中，气体发生器与脉冲涡轮机组件和发电机中的一个或多个耦合以形成微动力单元。

5. 发明授权

US08191351B2 Insensitive rocket motor 有权
标题翻译：不敏感火箭发动机
公开(公告)号：US08191351B2
公开(公告)日：2012-06-05
申请号：US12261905
申请日：2008-10-30
申请人： Richard D. Loehr , Gerald M. Turner , Jeremy C. Danforth
发明人： Richard D. Loehr , Gerald M. Turner , Jeremy C. Danforth
IPC分类号： F02K9/08 , F02K9/38
CPC分类号： F02K9/18 , F02K9/22 , F02K9/26
摘要： There is disclosed a solid fuel rocket motor including a center-perforated solid fuel grain. The solid fuel grain may be adapted to burn outwardly from a center surface facing the center perforation when ignited by a primary igniter during a normal mode of operation. The solid fuel grain may be further adapted to burn longitudinally from an end face when ignited by a secondary igniter during a safety mode of operation.
摘要翻译：公开了一种固体燃料火箭发动机，其包括中心穿孔的固体燃料颗粒。固体燃料颗粒可以适于在正常操作模式期间被主要点火器点燃时从面向中心穿孔的中心表面向外燃烧。固体燃料颗粒可以进一步适于在安全操作模式期间被二次点火器点燃时从端面纵向燃烧。

6. 发明授权

US07997205B2 Base drag reduction fairing 有权
标题翻译：底盘减速整流罩
公开(公告)号：US07997205B2
公开(公告)日：2011-08-16
申请号：US12463260
申请日：2009-05-08
申请人： Kevin R. Greenwood , James D. Streeter , Jeremy C. Danforth , Timothy A. Yoder
发明人： Kevin R. Greenwood , James D. Streeter , Jeremy C. Danforth , Timothy A. Yoder
IPC分类号： F42B15/01
CPC分类号： F42B10/50 , F42B10/38 , F42B10/42 , F42B10/44 , Y10T428/13
摘要： A projectile may include a base drag reduction fairing preform adapted to be plastically deformed into a base drag reduction fairing after the projectile is launched from a gun barrel.
摘要翻译：抛射体可以包括底座减阻整流罩预制件，其适用于在从枪管发射抛射体之后塑性变形成基座减速整流罩。

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