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1. 发明授权

US08733745B2 Load mount jounce rate cup 有权
标题翻译：加载安装镜头速率杯
公开(公告)号：US08733745B2
公开(公告)日：2014-05-27
申请号：US13471540
申请日：2012-05-15
申请人： Ravindra P Patil , Robert T. Jane , Michael A. Ray , Robert L. Geisler , Joseph A. Schudt
发明人： Ravindra P Patil , Robert T. Jane , Michael A. Ray , Robert L. Geisler , Joseph A. Schudt
IPC分类号： B60G13/00
CPC分类号： B60G15/068 , B60G15/07 , B60G2204/45021 , F16F9/58
摘要： A vehicle suspension system including a shock upper mount assembly mounted to vehicle structure, a jounce bumper being made of an elastomeric material and including a vertically extending rod bore around a rod of a shock absorber, and a jounce rate cup. The jounce rate cup is made of an elastomeric material and includes a horizontally extending support flange having a lower surface mounted on the jounce bumper, a horizontally extending dust boot attachment flange spaced from the support flange and having an upper surface located below and adjacent to the shock upper mount assembly, and a vertical flange extending between the support flange and the dust boot attachment flange to define a gap between the support flange and the dust boot attachment flange, with the jounce rate cup including a vertically extending rod bore mounted around the rod.
摘要翻译：一种车辆悬架系统，包括安装到车辆结构上的冲击上部安装组件，由弹性体材料制成的跳动保险杠，并且包括围绕减震器的杆的垂直延伸的杆孔和弯曲速率杯。跳动率杯由弹性体材料制成，并且包括水平延伸的支撑凸缘，其具有安装在弹簧保险杠上的下表面，与支撑凸缘间隔开的水平延伸的防尘罩附件凸缘，并且具有位于下方并且邻近减震上部安装组件，以及在支撑凸缘和防尘罩附件凸缘之间延伸的垂直凸缘，以限定支撑凸缘和防尘罩附件凸缘之间的间隙，其中跳动速率杯包括围绕杆安装的垂直延伸的杆孔。

2. 发明申请

US20130307204A1 LOAD MOUNT JOUNCE RATE CUP 有权
标题翻译：负载安装速率杯
公开(公告)号：US20130307204A1
公开(公告)日：2013-11-21
申请号：US13471540
申请日：2012-05-15
申请人： Ravindra P. Patil , Robert T. Jane , Michael A. Ray , Robert L. Geisler , Joseph A. Schudt
发明人： Ravindra P. Patil , Robert T. Jane , Michael A. Ray , Robert L. Geisler , Joseph A. Schudt
IPC分类号： B60G11/22 , B60G15/06
CPC分类号： B60G15/068 , B60G15/07 , B60G2204/45021 , F16F9/58
摘要： A vehicle suspension system including a shock upper mount assembly mounted to vehicle structure, a jounce bumper being made of an elastomeric material and including a vertically extending rod bore around a rod of a shock absorber, and a jounce rate cup. The jounce rate cup is made of an elastomeric material and includes a horizontally extending support flange having a lower surface mounted on the jounce bumper, a horizontally extending dust boot attachment flange spaced from the support flange and having an upper surface located below and adjacent to the shock upper mount assembly, and a vertical flange extending between the support flange and the dust boot attachment flange to define a gap between the support flange and the dust boot attachment flange, with the jounce rate cup including a vertically extending rod bore mounted around the rod.
摘要翻译：一种车辆悬架系统，包括安装到车辆结构上的冲击上部安装组件，由弹性体材料制成的跳动保险杠，并且包括围绕减震器的杆的垂直延伸的杆孔和弯曲速率杯。跳动率杯由弹性体材料制成，并且包括水平延伸的支撑凸缘，其具有安装在弹簧保险杠上的下表面，与支撑凸缘间隔开的水平延伸的防尘罩附件凸缘，并且具有位于下方并且邻近减震上部安装组件，以及在支撑凸缘和防尘罩附件凸缘之间延伸的垂直凸缘，以限定支撑凸缘和防尘罩附件凸缘之间的间隙，其中跳动速率杯包括围绕杆安装的垂直延伸的杆孔。

3. 发明授权

US08123203B2 Vehicular jounce bumper assembly 有权
标题翻译：车载跳闸保险杠总成
公开(公告)号：US08123203B2
公开(公告)日：2012-02-28
申请号：US12392706
申请日：2009-02-25
申请人： Ravindra P. Patil , Joseph A. Schudt , Daryl R. Poirier , Robert L. Geisler
发明人： Ravindra P. Patil , Joseph A. Schudt , Daryl R. Poirier , Robert L. Geisler
IPC分类号： B60G13/00
CPC分类号： F16F9/38 , B60G11/54 , B60G15/065 , B60G15/067 , B60G2202/312 , B60G2204/125 , B60G2204/45021 , B60G2206/73 , F16F9/58
摘要： A jounce bumper assembly for a vehicular suspension system, the suspension system having a first member and a second member, is provided. The assembly comprises a mount coupled to the first member, wherein the mount has a cylindrical portion comprising a first cylindrical outer surface. The assembly also comprises a jounce bumper coupled to the second member, and a striker cap having a first end comprising a first cylindrical inner surface circumferentially coupled over the first cylindrical outer surface, and having a second end configured for resilient engagement with the jounce bumper.
摘要翻译：一种用于车辆悬挂系统的跳动保险杠组件，具有第一构件和第二构件的悬挂系统。组件包括联接到第一构件的安装件，其中安装件具有包括第一圆柱形外表面的圆柱形部分。所述组件还包括联接到所述第二构件的跳动保险杠，以及具有第一端的撞针帽，所述第一端包括圆周地联接在所述第一圆柱形外表面上的第一圆柱形内表面，并且具有构造成用于与所述弯曲缓冲器弹性接合的第二端。

4. 发明申请

US20130328255A1 MOUNT ASSEMBLY FOR SUSPENSION DAMPER 有权
标题翻译：悬挂阻尼器的安装组件
公开(公告)号：US20130328255A1
公开(公告)日：2013-12-12
申请号：US13494168
申请日：2012-06-12
申请人： Robert L. Geisler , Ravindra P. Patil , Joseph A. Schudt , Daryl R. Poirier
发明人： Robert L. Geisler , Ravindra P. Patil , Joseph A. Schudt , Daryl R. Poirier
IPC分类号： B60G15/06
CPC分类号： B60G15/067 , B60G15/068 , B60G2204/41 , B60G2204/45021 , F16F9/54 , F16F9/58
摘要： A mount assembly for a suspension damper is provided which includes a piston rod extending about an axis and a mount housing. A jounce bumper is axially positioned about the piston rod and has an end surface and a radially outer surface. The jounce bumper is formed of a first deformable material selectable for absorbing energy from an axial force applicable through the piston rod. A jounce bumper cup formed of a second deformable material selectable for absorbing additional energy fits onto the end surface of the jounce bumper. The jounce bumper cup has a wall portion extending sufficiently around the radially outer surface of the jounce bumper to retain it in position and a load mount portion extending to the mount housing and being configured to absorb the additional energy.
摘要翻译：提供了一种用于悬挂阻尼器的安装组件，其包括围绕轴线延伸的活塞杆和安装壳体。弹簧保险杠围绕活塞杆轴向定位并且具有端表面和径向外表面。跳动保险杠由可由可通过活塞杆施加的轴向力吸收能量的第一可变形材料形成。由可选择用于吸收附加能量的第二可变形材料形成的跳动保险杠杯装配到跳动保险杠的端表面上。弹跳保险杠杯具有围绕弹簧缓冲器的径向外表面充分延伸的壁部分，以将其保持在适当位置，并且负载安装部分延伸到安装壳体并且构造成吸收附加能量。

5. 发明授权

US08931768B2 Mount assembly for suspension damper 有权
标题翻译：悬挂阻尼器安装组件
公开(公告)号：US08931768B2
公开(公告)日：2015-01-13
申请号：US13494168
申请日：2012-06-12
申请人： Robert L. Geisler , Ravindra P. Patil , Joseph A. Schudt , Daryl R. Poirier
发明人： Robert L. Geisler , Ravindra P. Patil , Joseph A. Schudt , Daryl R. Poirier
IPC分类号： B60G21/00
CPC分类号： B60G15/067 , B60G15/068 , B60G2204/41 , B60G2204/45021 , F16F9/54 , F16F9/58
摘要： A mount assembly for a suspension damper is provided which includes a piston rod extending about an axis and a mount housing. A jounce bumper is axially positioned about the piston rod and has an end surface and a radially outer surface. The jounce bumper is formed of a first deformable material selectable for absorbing energy from an axial force applicable through the piston rod. A jounce bumper cup formed of a second deformable material selectable for absorbing additional energy fits onto the end surface of the jounce bumper. The jounce bumper cup has a wall portion extending sufficiently around the radially outer surface of the jounce bumper to retain it in position and a load mount portion extending to the mount housing and being configured to absorb the additional energy.
摘要翻译：提供了一种用于悬挂阻尼器的安装组件，其包括围绕轴线延伸的活塞杆和安装壳体。弹簧保险杠围绕活塞杆轴向定位并且具有端表面和径向外表面。跳动保险杠由可由可通过活塞杆施加的轴向力吸收能量的第一可变形材料形成。由可选择用于吸收附加能量的第二可变形材料形成的跳动保险杠杯装配到跳动保险杠的端表面上。弹跳保险杠杯具有围绕弹簧缓冲器的径向外表面充分延伸的壁部分，以将其保持在适当位置，并且负载安装部分延伸到安装壳体并且构造成吸收附加能量。

6. 发明申请

US20110011295A1 Kinetic Fireball Incendiary Munition 有权
标题翻译：动力火球燃烧弹药
公开(公告)号：US20110011295A1
公开(公告)日：2011-01-20
申请号：US12748795
申请日：2010-03-29
申请人： Robert L. Geisler , Kevin E. Mahaffy
发明人： Robert L. Geisler , Kevin E. Mahaffy
IPC分类号： F42B12/44
CPC分类号： F42B12/44 , F42B12/52 , F42B12/58
摘要： A kinetic fireball incendiary munition is provided having an outer shell or bomb casing, one or more incendiary submunitions therein, and an igniter therefore. Each of the submunitions includes an incendiary portion, at least one rocket motor that propels the submunition inside of a target volume, and an oxidizer for the incendiary portion and rocket motor. The submunitions liberate sufficient heat to produce elevated temperatures inside of a target structure to thermalize the contents thereof without creating a substantial overpressure or explosive effect. The incendiary portion includes a solid propellant and, optionally, one or more energetic materials selected from the group consisting of phosphorous, boron, magnesium, aluminum, Fluorinert™-aluminum and BKNO3. The incendiary submunition may be in the shape of a ball or a circular disk with a rocket motor therein. The circular disk-shaped incendiary munition is provided with an outer layer of an insulation which is bonded to the propellant/incendiary material. A portion of the insulation on the top and bottom of the disk is weakened so as to break away when the top and bottom surfaces are ignited. In place of the rocket motor, the submunition may incorporate one or more barrels embedded in the incendiary material with a powder charge and projectile in each barrel. Ignition of the incendiary material results in detonation of the powder charge which propels projectiles radially outwardly and upwardly causing damage to containers of chemical/biological materials.
摘要翻译：提供了一种动力火球燃烧弹药，其中具有外壳或炸弹外壳，其中包括一个或多个燃烧子弹药和点火器。每个子弹药包括燃烧部分，至少一个将目标体积内的子弹药推进的火箭发动机，以及用于燃烧部分和火箭发动机的氧化剂。子弹药释放足够的热量以在目标结构内产生升高的温度，以使其内容物热化，而不产生显着的超压或爆炸效应。燃烧部分包括固体推进剂和任选的一种或多种选自磷，硼，镁，铝，氟化铝 - 铝和BKNO 3的高能材料。燃烧的子弹药可以是其中具有火箭发动机的球或圆盘的形状。圆形盘状燃烧弹药具有与推进剂/燃烧材料结合的绝缘层的外层。盘顶部和底部的绝缘部分被削弱，以便在顶部和底部表面被点燃时脱落。代替火箭发动机，子弹药可以将一个或多个嵌入在燃烧材料中的桶与每个桶中的粉末装料和抛射体混合。燃烧材料的点火导致粉末装料的爆炸，其将径向向外和向上推动射弹，导致对化学/生物材料的容器的损坏。

7. 发明授权

US07278356B1 Kinetic fireball incendiary munition 有权
标题翻译：动力火球燃烧弹药
公开(公告)号：US07278356B1
公开(公告)日：2007-10-09
申请号：US11434045
申请日：2006-05-15
申请人： Robert L. Geisler , Kevin E. Mahaffy
发明人： Robert L. Geisler , Kevin E. Mahaffy
IPC分类号： F42B12/44
CPC分类号： F42B12/44
摘要： A kinetic fireball incendiary munition is provided having an outer shell or bomb casing, one or more incendiary submunitions therein, and an igniter therefore. Each of the submunitions includes an incendiary portion and at least one rocket motor that propels the submunition inside of a target volume. The submunitions liberate sufficient heat to produce elevated temperatures inside of a target structure, without creating a substantial overpressure or explosive effect. The incendiary portion includes a solid propellant and, optionally, one or more energetic materials selected from the group consisting of phosphorous, boron, magnesium, aluminum, Fluorinert™-aluminum and BKNO3. The incendiary submunition may be in the shape of a ball or a circular disk with a rocket motor therein.
摘要翻译：提供了一种动力火球燃烧弹药，其中具有外壳或炸弹外壳，其中包括一个或多个燃烧子弹药和点火器。每个子弹药包括燃烧部分和至少一个将子弹药推进目标体积内的火箭发动机。子弹药释放足够的热量以在目标结构内部产生升高的温度，而不产生显着的超压或爆炸作用。燃烧部分包括固体推进剂和任选的一种或多种选自磷，硼，镁，铝，氟化铝 - 铝和BKNO 3的高能材料。燃烧的子弹药可以是其中具有火箭发动机的球或圆盘的形状。

8. 发明申请

US20090320443A1 Propulsion system, opposing grains rocket engine, and method for controlling the burn rate of solid propellant grains 失效
标题翻译：推进系统，相对谷物火箭发动机，以及控制固体推进剂颗粒燃烧速率的方法
公开(公告)号：US20090320443A1
公开(公告)日：2009-12-31
申请号：US12151900
申请日：2008-05-09
申请人： Robert L. Geisler , Kevin E. Mahaffy
发明人： Robert L. Geisler , Kevin E. Mahaffy
IPC分类号： C06D5/00
CPC分类号： F02K9/26 , F02K9/22 , F02K9/28
摘要： A solid propellant thrust control system, method, and apparatus for controlling combustion of solid propellants in an opposing grains solid propellant rocket engine (OGRE) is provided. In particular, an opposing grains rocket engine and propulsion system is provided, in which actuator means connected are connected to solid propellant grains disposed in the pressure vessel of the engine. The actuator means are operable to selectively move the solid propellant grains together or apart relative to one another, such that the burning ends of the solid propellant grains decrease or increase relative to one another. This action controls the rate of combustion of the solid propellant grains by varying spacing distance between the burning ends of the solid propellant grains, and enables extinguishment and reignition of the OGRE. Further, a method is providing for controlling the burn rate of solid propellant grains undergoing combustion in an opposing grains rocket engine.
摘要翻译：提供了一种用于控制相对颗粒固体推进剂火箭发动机（OGRE）中固体推进剂燃烧的固体推进剂推力控制系统，方法和装置。特别地，提供了相对的谷物火箭发动机和推进系统，其中连接的致动器装置连接到设置在发动机的压力容器中的固体推进剂颗粒。致动器装置可操作以将固体推进剂颗粒相对于彼此选择性地移动或分开，使得固体推进剂颗粒的燃烧端相对于彼此减小或增加。该动作通过改变固体推进剂颗粒的燃烧端之间的间隔距离来控制固体推进剂颗粒的燃烧速率，并且能够使OGRE熄灭和重新点燃。此外，一种方法是提供用于控制在相对的谷物火箭发动机中经历燃烧的固体推进剂颗粒的燃烧速率。

9. 发明授权

US5274998A Rocket pollution reduction system 失效
标题翻译：火箭污染减少系统
公开(公告)号：US5274998A
公开(公告)日：1994-01-04
申请号：US911184
申请日：1992-07-06
申请人： Robert L. Geisler
发明人： Robert L. Geisler
IPC分类号： F02K9/72 , F02K9/00
CPC分类号： F02K9/72
摘要： A system is provided for reducing the emissions of hydrochloric acid (HCl) from solid fuel rockets, especially during ground disposal. An aqueous solution (40, FIG. 2 ) of an alkali metal hydroxide is injected as a mist (50) into the rocket chamber (32) as the rocket fuel (30) is burned. The reaction of the alkali metal with hydrogen chloride (HCl) produces a salt and thereby minimizes the presence of hydrochloric acid in the rocket exhaust. An injected neutralizing material which reduces hydrochloric acid, but which produces less thrust than an equal weight of rocket fuel, can be injected into an operating rocket which carries a payload high above the earth, with the injected material being injected only while the rocket is at a lower altitude when hydrochloric acid is most undesirable. The injected material can be produced by a small auxiliary rocket device (82, FIG. 4 ) whose exhaust (84) is delivered directly to the main rocket chamber (86), and with the exhaust of the auxiliary rocket device including a high proportion of magnesium to react with the hydrochloric acid with minimal degradation of rocket performance.
摘要翻译：提供一种系统，用于减少固体燃料火箭的盐酸（HCl）排放，特别是在地面处置过程中。当火箭燃料（30）燃烧时，碱金属氢氧化物的水溶液（40，图2）以雾（50）的形式被注入到火箭室（32）中。碱金属与氯化氢（HCl）的反应产生盐，从而使火箭尾气中盐酸的存在最小化。注入的中和材料，其减少盐酸，但是产生比同等重量的火箭燃料更少的推力，可以注入到运载火箭中，该火箭携带高于地球的有效载荷，注入的物质仅在火箭处于当盐酸最不希望时，较低的高度。喷射的材料可以通过其排气（84）直接输送到主火箭室（86）的小型辅助火箭装置（82）产生，并且辅助火箭装置的排气包括高比例的镁与盐酸反应，火箭性能降低最小。

10. 发明授权

US4017342A Method for improving metal combustion in solid rocket propellants 失效
标题翻译：固体火箭推进剂改善金属燃烧的方法
公开(公告)号：US4017342A
公开(公告)日：1977-04-12
申请号：US674020
申请日：1976-04-05
申请人： Robert L. Geisler , Arnold M. Crelier , Francisco Q. Roberto
发明人： Robert L. Geisler , Arnold M. Crelier , Francisco Q. Roberto
IPC分类号： C06B21/00 , C06B45/30
CPC分类号： C06B45/30 , C06B21/0083
摘要： A method for improving the ballistic properties of aluminum powder based rocket propellants by treating the aluminum powder with hydrogen fluoride gas prior to its incorporation into a propellant formulation.
摘要翻译：一种通过在掺入推进剂制剂之前用氟化氢气体处理铝粉末来改善铝粉基火箭推进剂的弹道性能的方法。

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