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1. 发明申请

US20130208367A1 BI-POLYMER INFRARED OPTICS FOR HIGH-G APPLICATIONS 有权
标题翻译：用于高G应用的BI聚合物红外光学
公开(公告)号：US20130208367A1
公开(公告)日：2013-08-15
申请号：US13370543
申请日：2012-02-10
申请人： John A. Thomas , Thomas H. Lind , Ronald L. Roncone , Gary H. Johnson
发明人： John A. Thomas , Thomas H. Lind , Ronald L. Roncone , Gary H. Johnson
IPC分类号： G02B17/02 , B23P25/00
CPC分类号： G02B23/16 , F41G7/2253 , F41G7/2293 , F42B15/01 , G02B7/008 , G02B7/182 , G02B17/0808 , G02B23/12 , Y10T29/4998
摘要： Optical systems configured to withstand operation in high acceleration and varying temperature environments, and methods of assembling the same. In one example, an imaging optical apparatus includes a primary minor made of an unreinforced polymer, a secondary mirror made of the unreinforced polymer and optically coupled to the primary minor, a field lens optically coupled to the secondary minor, and a strut having a plurality of cross-struts and mounting features configured to mount the primary minor, the secondary mirror and the field lens. In some examples, the imaging optical apparatus further includes an outer retainer disposed behind the primary minor and coupled to the strut, and an inner retainer disposed behind the field lens and coupled to the strut, the outer and inner retainers configured to structurally support the primary minor and the field lens and to accommodate deflections of the primary minor.
摘要翻译：配置为承受在高加速度和变化的温度环境中操作的光学系统及其组装方法。在一个示例中，成像光学装置包括由非增强聚合物制成的主反射镜，由未加强聚合物制成的光学耦合到主反射镜的二次反射镜，与第二反射镜光学耦合的场透镜，以及具有多个的交叉支柱和安装特征，其被配置为安装主镜，副镜和镜头。在一些示例中，成像光学装置还包括设置在主反射镜后面并连接到支柱的外部保持器，以及设置在镜头后面并连接到支柱的内部保持器，外侧和内侧保持器构造成在主结构上支撑主镜镜子和场镜，并适应主镜的偏转。

2. 发明授权

US08567969B2 Bi-polymer infrared optics for high-G applications 有权
标题翻译：双高分子红外光学用于高G应用
公开(公告)号：US08567969B2
公开(公告)日：2013-10-29
申请号：US13370543
申请日：2012-02-10
申请人： John A. Thomas , Thomas H. Lind , Ronald L. Roncone , Gary H. Johnson
发明人： John A. Thomas , Thomas H. Lind , Ronald L. Roncone , Gary H. Johnson
IPC分类号： G02B7/182 , G02B17/00
CPC分类号： G02B23/16 , F41G7/2253 , F41G7/2293 , F42B15/01 , G02B7/008 , G02B7/182 , G02B17/0808 , G02B23/12 , Y10T29/4998
摘要： Optical systems configured to withstand operation in high acceleration and varying temperature environments, and methods of assembling the same. In one example, an imaging optical apparatus includes a primary minor made of an unreinforced polymer, a secondary mirror made of the unreinforced polymer and optically coupled to the primary minor, a field lens optically coupled to the secondary minor, and a strut having a plurality of cross-struts and mounting features configured to mount the primary minor, the secondary mirror and the field lens. In some examples, the imaging optical apparatus further includes an outer retainer disposed behind the primary minor and coupled to the strut, and an inner retainer disposed behind the field lens and coupled to the strut, the outer and inner retainers configured to structurally support the primary minor and the field lens and to accommodate deflections of the primary minor.
摘要翻译：配置为承受在高加速度和变化的温度环境中操作的光学系统及其组装方法。在一个示例中，成像光学装置包括由非增强聚合物制成的主反射镜，由未加强聚合物制成的光学耦合到主反射镜的二次反射镜，与第二反射镜光学耦合的场透镜，以及具有多个的交叉支柱和安装特征，其被配置为安装主镜，副镜和镜头。在一些示例中，成像光学装置还包括设置在主反射镜后面并连接到支柱的外部保持器，以及设置在镜头后面并连接到支柱的内部保持器，外侧和内侧保持器构造成在主结构上支撑主镜镜子和场镜，并适应主镜的偏转。

3. 发明授权

US07633691B2 Optical mounting for high-g environment 有权
标题翻译：光学安装用于高g环境
公开(公告)号：US07633691B2
公开(公告)日：2009-12-15
申请号：US10862279
申请日：2004-06-07
申请人： Gary H. Johnson , John A. Thomas , John A. Winkler
发明人： Gary H. Johnson , John A. Thomas , John A. Winkler
IPC分类号： G02B7/02
CPC分类号： G02B26/007 , G01S7/4813 , G02B7/006
摘要： An optical element mounting includes a frame, and a shuttle that is translatable relative to the frame. The shuttle includes inner and outer portions that are mechanically coupled together by a plurality of flexures that effectively bending and twisting of the shuttle from being transmitted to an optical element, such as an optical window, that is mounted on the inner portion of the shuttle. The flexures may be thin linking strips of material between the outer and inner portions. The flexures may have a thickness that is greater in an expected load direction, than in a direction perpendicular to the load direction. The optical mounting may include a locking mechanism, for example including a shape memory alloy wire, to lock the shuttle in a predetermined location relative to the frame.
摘要翻译：光学元件安装包括框架和可相对于框架平移的梭子。穿梭机包括内部和外部部分，其通过多个挠曲机械地联接在一起，其有效地弯曲和扭转梭不被传递到安装在梭子的内部上的诸如光学窗口的光学元件。挠曲件可以是在外部和内部之间的薄的材料条带。挠曲件可以具有在预期载荷方向上比在垂直于载荷方向的方向上更大的厚度。光学安装件可以包括锁定机构，例如包括形状记忆合金线，以将梭子相对于框架锁定在预定位置。

4. 发明授权

US07547865B2 Optical element mount and method thereof for a gun-launched projectile 有权
标题翻译：光学元件安装及其枪射弹的方法
公开(公告)号：US07547865B2
公开(公告)日：2009-06-16
申请号：US11761155
申请日：2007-06-11
申请人： Gary H. Johnson , Douglas M. Beard , John A. Thomas , Rene D. Perez
发明人： Gary H. Johnson , Douglas M. Beard , John A. Thomas , Rene D. Perez
IPC分类号： F42B15/01 , F42B15/10 , F41G7/00 , F42B15/00
CPC分类号： F42B30/006 , F41G7/2253 , F41G7/226 , F41G7/2293 , G02B7/00 , G02B7/007 , G02B7/02
摘要： An optical element mount is effective in high G environments to protect brittle optical elements in which tensile stresses are generated on surface S2 without degrading optical performance. A flexible spacer formed of a relatively low-stiffness material supports an optical element having a tapered outer periphery in an optical seat having a complementary tapered surface. When the optical assembly is exposed to the high G environment, the inertial loading drives the optical element in the aft direction into the flexible spacer and seat. This puts the optical element into a plate bending condition thereby inducing tensile stress on S2 which is at least partially offset by a compressive stress caused by the reaction force normal to the tapered interface. The stresses, both compressive and tensile, placed on the optical element in the high G environment can be very large. In the absence of the tapered mount and flexible spacer, the tensile stress placed on S2 would likely fracture or shatter the brittle optical element. When the inertial loading is removed, the optical element returns to its initial unstressed position.
摘要翻译：光学元件安装件在高G环境中是有效的，以保护脆性光学元件，其中在表面S2上产生拉伸应力而不降低光学性能。由相对低刚度材料形成的柔性间隔件支撑在具有互补锥形表面的光学座中具有锥形外周的光学元件。当光学组件暴露于高G环境时，惯性负载将光学元件向后驱动到柔性隔板和座椅中。这使得光学元件进入板弯曲状态，从而引起S2上的拉伸应力，该拉伸应力至少部分地被由锥形界面的反作用力引起的压缩应力偏移。放置在高G环境中的光学元件上的压缩和拉伸应力可能非常大。在没有锥形安装件和柔性隔离件的情况下，放置在S2上的拉伸应力可能会破坏或破碎脆性光学元件。当去除惯性负载时，光学元件返回到其初始无应力位置。

5. 发明申请

US20080302905A1 OPTICAL ELEMENT MOUNT AND METHOD THEREOF FOR A GUN-LAUNCHED PROJECTILE 有权
标题翻译：光学元件安装及其方法
公开(公告)号：US20080302905A1
公开(公告)日：2008-12-11
申请号：US11761155
申请日：2007-06-11
申请人： Gary H. Johnson , Douglas M. Beard , John A. Thomas , Rene D. Perez
发明人： Gary H. Johnson , Douglas M. Beard , John A. Thomas , Rene D. Perez
IPC分类号： F41G7/26 , F42B15/01
CPC分类号： F42B30/006 , F41G7/2253 , F41G7/226 , F41G7/2293 , G02B7/00 , G02B7/007 , G02B7/02
摘要： An optical element mount is effective in high G environments to protect brittle optical elements in which tensile stresses are generated on surface S2 without degrading optical performance. A flexible spacer formed of a relatively low-stiffness material supports an optical element having a tapered outer periphery in an optical seat having a complementary tapered surface. When the optical assembly is exposed to the high G environment, the inertial loading drives the optical element in the aft direction into the flexible spacer and seat. This puts the optical element into a plate bending condition thereby inducing tensile stress on S2 which is at least partially offset by a compressive stress caused by the reaction force normal to the tapered interface. The stresses, both compressive and tensile, placed on the optical element in the high G environment can be very large. In the absence of the tapered mount and flexible spacer, the tensile stress placed on S2 would likely fracture or shatter the brittle optical element. When the inertial loading is removed, the optical element returns to its initial unstressed position.
摘要翻译：光学元件安装件在高G环境中是有效的，以保护脆性光学元件，其中在表面S2上产生拉伸应力而不降低光学性能。由相对低刚度材料形成的柔性间隔件支撑在具有互补锥形表面的光学座中具有锥形外周的光学元件。当光学组件暴露于高G环境时，惯性负载将光学元件向后驱动到柔性隔板和座椅中。这使得光学元件进入板弯曲状态，从而引起S2上的拉伸应力，该拉伸应力至少部分地被由锥形界面的反作用力引起的压缩应力偏移。放置在高G环境中的光学元件上的压缩和拉伸应力可能非常大。在没有锥形安装件和柔性隔离件的情况下，放置在S2上的拉伸应力可能会破坏或破碎脆性光学元件。当去除惯性负载时，光学元件返回到其初始无应力位置。

6. 发明授权

US06764042B2 Precision guided extended range artillery projectile tactical base 有权
标题翻译：精准导向扩展射炮战术基地
公开(公告)号：US06764042B2
公开(公告)日：2004-07-20
申请号：US10435834
申请日：2003-05-12
申请人： James L. Moore , Gary H. Johnson , William S. Peterson , Rajesh H. Shah , Richard Dryer
发明人： James L. Moore , Gary H. Johnson , William S. Peterson , Rajesh H. Shah , Richard Dryer
IPC分类号： F42B1000
CPC分类号： F42B10/38 , F42B10/14
摘要： A tacital base for a guided projectile includes a base structure, and an adaptor structure for securing the base structure to a forward section of the projectile. The base further includes a plurality of fin slots. A plurality of deployable fins are pivotally mounted to the base structure and supported for movement between a stowed position and a deployed position.
摘要翻译：用于引导的抛射体的固定基座包括基部结构和用于将基部结构固定到射弹的前部的适配器结构。基座还包括多个鳍槽。多个可展开的翅片可枢转地安装到基座结构上并被支撑以在收起位置和展开位置之间移动。

7. 发明授权

US07566028B2 Integral locking mechanism for deployable device 有权
标题翻译：可部署设备的集成锁定机制
公开(公告)号：US07566028B2
公开(公告)日：2009-07-28
申请号：US11586893
申请日：2006-10-26
申请人： Gary H. Johnson
发明人： Gary H. Johnson
IPC分类号： F42B15/01
CPC分类号： F42B10/14 , F42B10/64
摘要： A guided projectile has a deployment system for deploying a deployable structure, such as a fin, another type of control surface, or an antenna. The deployment system includes a single-piece body that has a hub body and a resilient tab. The resilient tab presses against a stepped surface of a guided projectile body. As the deployable structure is extended, the deployable structure body rotates about a shaft in a central hole or aperture in the hub body. The resilient tab presses against the stepped surface on one side of an edge of the stepped surface during a first (relatively stowed) part of this deployment. At a certain point, as the contact between the tab and the stepped surfaces reaches the edge (the step of the stepped surface), the resilient tab changes position. The change in position of the resilient tab keeps the deployable structure from retracting again.
摘要翻译：引导抛射体具有用于部署可部署结构的部署系统，例如翅片，另一类型的控制表面或天线。部署系统包括具有轮毂体和弹性片的单件本体。弹性突片压靠被引导的射弹体的台阶表面。随着可展开结构的延伸，可展开的结构体围绕毂体中的中心孔或孔中的轴转动。在该部署的第一（相对收起）部分期间，弹性突片在台阶表面的边缘的一侧压靠台阶表面。在某一点上，当突片和阶梯表面之间的接触到达边缘（台阶表面的台阶）时，弹性片改变位置。弹性片的位置变化使得可展开结构不再缩回。

8. 发明申请

US20080099598A1 Integral locking mechanism for deployable device 有权
标题翻译：可部署设备的集成锁定机制
公开(公告)号：US20080099598A1
公开(公告)日：2008-05-01
申请号：US11586893
申请日：2006-10-26
申请人： Gary H. Johnson
发明人： Gary H. Johnson
IPC分类号： F42B10/14
CPC分类号： F42B10/14 , F42B10/64
摘要： A guided projectile has a deployment system for deploying a deployable structure, such as a fin, another type of control surface, or an antenna. The deployment system includes a single-piece body that has a hub body and a resilient tab. The resilient tab presses against a stepped surface of a guided projectile body. As the deployable structure is extended, the deployable structure body rotates about a shaft in a central hole or aperture in the hub body. The resilient tab presses against the stepped surface on one side of an edge of the stepped surface during a first (relatively stowed) part of this deployment. At a certain point, as the contact between the tab and the stepped surfaces reaches the edge (the step of the stepped surface), the resilient tab changes position. The change in position of the resilient tab keeps the deployable structure from retracting again.
摘要翻译：引导抛射体具有用于部署可部署结构的部署系统，例如翅片，另一类型的控制表面或天线。部署系统包括具有轮毂体和弹性片的单件本体。弹性突片压靠被引导的射弹体的台阶表面。随着可展开结构的延伸，可展开的结构体围绕毂体中的中心孔或孔中的轴转动。在该部署的第一（相对收起）部分期间，弹性突片在台阶表面的边缘的一侧压靠台阶表面。在某一点上，当突片和阶梯表面之间的接触到达边缘（台阶表面的台阶）时，弹性片改变位置。弹性片的位置变化使得可展开结构不再缩回。

9. 发明授权

US08931738B2 Releasable radome cover 有权
标题翻译：可释放天线罩盖
公开(公告)号：US08931738B2
公开(公告)日：2015-01-13
申请号：US13401768
申请日：2012-02-21
申请人： Phillip Craige White , Robert L. Sisk, III , Brian S. Scott , Larry A. Coleman , Gary H. Johnson
发明人： Phillip Craige White , Robert L. Sisk, III , Brian S. Scott , Larry A. Coleman , Gary H. Johnson
IPC分类号： B64C1/10
CPC分类号： B64C7/00 , F42B10/46 , F42B15/10
摘要： A protective cover (10) for an instrument dome (12) extending from a body (20) of a vehicle, such as a missile. The cover (10) includes multiple segments (14 and 16) having trailing ends (18) connectable to the body (20) at joints (22) that allow for rotational movement. The cover (10) further includes a releasable holder (26) that includes a retention device (28) that holds leading ends (24) of the segments (14 and 16) together, and a release mechanism (30) for causing the retention device (28) to release the leading ends (24). The joints (22) hold the trailing ends (18) of the segments (14 and 16) to the body (20) through a predetermined range of motion beyond which the segments (14 and 16) will be released to separate from the body (20) when the segments (14 and 16) rotate beyond the predetermined range.
摘要翻译：一种用于从诸如导弹的车辆的本体（20）延伸的仪表盘（12）的保护盖（10）。盖（10）包括多个段（14和16），其具有在允许旋转运动的接头（22）处可连接到主体（20）的后端（18）。盖（10）还包括可释放保持器（26），其包括将段（14和16）的前端（24）保持在一起的保持装置（28）和用于使保持装置（28）以释放前端（24）。接头（22）将节段（14和16）的尾端（18）保持在主体（20）上一段预定的运动范围之外，分段（14和16）将被释放以与主体分离（14）和16（16）旋转超过预定范围。

10. 发明申请

US20130214093A1 RELEASABLE RADOME COVER 有权
标题翻译：可释放的雷射罩
公开(公告)号：US20130214093A1
公开(公告)日：2013-08-22
申请号：US13401768
申请日：2012-02-21
申请人： Phillip Craige White , Robert L. Sisk, III , Brian S. Scott , Larry A. Coleman , Gary H. Johnson
发明人： Phillip Craige White , Robert L. Sisk, III , Brian S. Scott , Larry A. Coleman , Gary H. Johnson
IPC分类号： B64C7/00
CPC分类号： B64C7/00 , F42B10/46 , F42B15/10
摘要： A protective cover (10) for an instrument dome (12) extending from a body (20) of a vehicle, such as a missile. The cover (10) includes multiple segments (14 and 16) having trailing ends (18) connectable to the body (20) at joints (22) that allow for rotational movement. The cover (10) further includes a releasable holder (26) that includes a retention device (28) that holds leading ends (24) of the segments (14 and 16) together, and a release mechanism (30) for causing the retention device (28) to release the leading ends (24). The joints (22) hold the trailing ends (18) of the segments (14 and 16) to the body (20) through a predetermined range of motion beyond which the segments (14 and 16) will be released to separate from the body (20) when the segments (14 and 16) rotate beyond the predetermined range.
摘要翻译：一种用于从诸如导弹的车辆的本体（20）延伸的仪表盘（12）的保护盖（10）。盖（10）包括多个段（14和16），其具有在允许旋转运动的接头（22）处可连接到主体（20）的后端（18）。盖（10）还包括可释放保持器（26），其包括将段（14和16）的前端（24）保持在一起的保持装置（28）和用于使保持装置（28）以释放前端（24）。接头（22）将节段（14和16）的尾端（18）保持在主体（20）上一段预定的运动范围之外，分段（14和16）将被释放以与主体分离（14）和16（16）旋转超过预定范围。

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