公开(公告)号：US08616818B2

公开(公告)日：2013-12-31

申请号：US13029744

申请日：2011-02-17

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: F16B43/00

CPC classification number: F16B41/002 ,  F16B43/00

Abstract: A gripping washer includes a washer body having first and second rigid support surfaces. A fastener hole extends between the first and second rigid support surfaces. An inner washer perimeter extends around the fastener hole. One or more elastomeric gripping tabs are coupled with the inner washer perimeter. The one or more elastomeric gripping tabs extend inwardly into the fastener hole from the inner washer perimeter. The elastomeric gripping tabs are pliable relative to the first and second rigid support surfaces of the washer body and deform and grip the washer with a fastener passed through the fastener hole. By gripping a fastener with the elastomeric gripping tabs the gripping washer is anchored to the fastener and substantially prevents decoupling of the gripping washer from the fastener prior to installation (e.g., fastening with a work piece). Gripping of the fastener with the gripping washer thereby minimizes foreign object debris.

Abstract translation: 夹紧垫圈包括具有第一和第二刚性支撑表面的垫圈本体。 紧固件孔在第一和第二刚性支撑表面之间延伸。 内垫圈周边围绕紧固件孔延伸。 一个或多个弹性夹持片与内垫圈周边相连。 一个或多个弹性夹持突舌从内垫圈周边向内延伸到紧固件孔中。 弹性夹持片相对于垫圈主体的第一和第二刚性支撑表面是柔韧的，并且通过穿过紧固件孔的紧固件变形并夹紧垫圈。 通过用弹性夹持突片夹持紧固件，夹紧垫片锚固到紧固件上，并基本上防止在安装之前（例如用工件紧固）把持垫圈与紧固件脱钩。 用夹紧垫圈夹紧紧固件，从而使外来物体碎片最小化。

公开(公告)号：US08342070B2

公开(公告)日：2013-01-01

申请号：US12237338

申请日：2008-09-24

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: F41F3/052

CPC classification number: F42B10/14 ,  F41F3/042 ,  F42B39/22

Abstract: In an embodiment of methods and apparatus for a control surface restraint and release system comprises a restraint apparatus detachably coupled to the control surface, a guidance rail slidably engaging the restraint apparatus, and a stopping mechanism coupled to the guidance rail and configured to stop a movement of the restraint apparatus.

Abstract translation: 在用于控制表面约束和释放系统的方法和装置的实施例中，包括可拆卸地联接到控制表面的约束装置，可滑动地接合约束装置的引导轨道和联接到引导轨道并被构造成停止运动的止动机构 的约束装置。

公开(公告)号：US07634912B2

公开(公告)日：2009-12-22

申请号：US11420361

申请日：2006-05-25

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: F01B29/08

CPC classification number: F15B15/1447 ,  F15B15/19

Abstract: Methods and apparatus for an actuator system according to various aspects of the present invention include a housing; a sleeve having a deformable portion; and a mover for applying force to the sleeve. The sleeve, which is sealed to the housing, is configured to reside and move within the housing. The mover applies a force against a portion of the sleeve, causing the deformable portion to deform and move.

Abstract translation: 根据本发明的各个方面的用于致动器系统的方法和装置包括壳体; 具有可变形部分的套筒; 以及向套筒施加力的移动器。 密封到壳体的套筒构造成在壳体内驻留和移动。 移动器对套筒的一部分施加力，导致可变形部分变形和移动。

公开(公告)号：US08729443B2

公开(公告)日：2014-05-20

申请号：US13020276

申请日：2011-02-03

Applicant: Andrew B. Facciano ,  James A. Ebel ,  Michael Alkema ,  Robert D. Travis ,  Mike J. Saxton

Inventor： Andrew B. Facciano ,  James A. Ebel ,  Michael Alkema ,  Robert D. Travis ,  Mike J. Saxton

IPC: F42B15/01 ,  F42B10/32 ,  F42B15/00 ,  F42B10/00

CPC classification number: B64G1/002 ,  B64G1/401 ,  B64G1/403 ,  F42B10/32 ,  F42B15/01 ,  F42B15/10

Abstract: Some embodiments pertain to a projectile and method that includes a flight vehicle and a propulsion system attached to the flight vehicle. The propulsion system includes a plurality of motors that propel the projectile. A guidance system is connected to the propulsion system. The guidance system ignites an appropriate number of the motors to adjust the speed of the projectile based on the location of the projectile relative to a desired destination for the flight vehicle. In some embodiments, the flight vehicle is a kinetic warhead. The projectile may be an interceptor that includes a first propulsion stage, a second propulsion stage and a third propulsion stage that includes the third propulsion system. The number of booster motors that will be ignited by the guidance system depends on the speed that the projectile needs to be adjusted to in order to maneuver the projectile to a desired location.

Abstract translation: 一些实施例涉及包括飞行车辆和附接到飞行器车辆的推进系统的射弹和方法。 推进系统包括推动射弹的多个马达。 引导系统连接到推进系统。 引导系统点燃适当数量的电机，以根据飞弹相对于飞行器的所需目的地的位置来调整射弹的速度。 在一些实施例中，飞行器是动力弹头。 抛射体可以是包括第一推进阶段，第二推进阶段和包括第三推进系统的第三推进阶段的拦截器。 引导系统将引燃的助力马达的数量取决于弹丸需要调整的速度，以便将弹丸操纵到所需的位置。

公开(公告)号：US20120137653A1

公开(公告)日：2012-06-07

申请号：US12958524

申请日：2010-12-02

Applicant: Andrew B. Facciano ,  Sandie Y. Worley ,  Robert D. Travis ,  Dale O. Widmer

Inventor： Andrew B. Facciano ,  Sandie Y. Worley ,  Robert D. Travis ,  Dale O. Widmer

IPC: F02K9/80 ,  H02G3/04

CPC classification number: F41F3/055 ,  F41F3/06

Abstract: A deployable raceway harness assembly for use with a multi-stage rocket includes a first cable bundle configured to extend across a second stage of a multi-stage rocket from a guidance unit to a first stage of the rocket. The deployable raceway harness assembly includes a deployable raceway cover configured for detachable coupling with the multi-stage rocket. The deployable raceway cover extends over at least the first cable bundle and a second cable bundle. The first cable bundle is fastened to the deployable raceway cover. The second cable bundle is configured to extend from the guidance unit to the second stage and is shorter than the first cable bundle. An in-flight deployment mechanism is configured to detach the deployable raceway cover and the first cable bundle extending across the second stage from the multi-stage rocket in-flight leaving the second cable bundle extending to the second stage in place.

Abstract translation: 与多级火箭一起使用的可部署的滚道线束组件包括被配置为延伸穿过多级火箭的第二级从引导单元到火箭的第一级的第一缆线束。 可部署的滚道线束组件包括配置成与多级火箭可拆卸联接的可展开滚道盖。 可部署的滚道盖至少延伸到第一缆线束和第二缆线束。 第一根电缆束固定在可部署的滚道盖上。 第二电缆束构造成从引导单元延伸到第二级并且比第一电缆束短。 飞行中部署机构被配置成从飞行中的多级火箭中分离可展开的滚道盖和穿过第二级延伸的第一缆线束，从而将第二缆线束延伸到第二级。

公开(公告)号：US08141491B1

公开(公告)日：2012-03-27

申请号：US12542783

申请日：2009-08-18

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: F42B15/38

CPC classification number: F42B15/38 ,  F42B15/36

Abstract: A separation device for separating parts along a seam includes a frangible structure and a pressure tube assembly within the frangible structure. The pressure tube assembly includes a pressure tube which contains an explosive detonation assembly/cord that can be initiated to expand the pressure tube, and break the frangible structure with a shock force. The pressure tube assembly also includes a explosive manifold that is recessed in the frangible structure, not protruding from an outer surface of the frangible structure. The explosive manifold receives the ends of the pressure tube, and includes a detonator for detonating the explosive detonation assembly/cord. The explosive manifold has circular-cross-section fittings for accepting a circular ends of the pressure tube. By not having any part of the pressure tube assembly protrude from the frangible structure, improved performance may be achieved. Having circular fittings also improves the seal between the pressure tube and the explosive manifold.

Abstract translation: 用于沿着接缝分离部件的分离装置包括在易碎结构内的易碎结构和压力管组件。 压力管组件包括压力管，该压力管包含爆炸性爆炸组件/绳索，其可以被起动以膨胀压力管，并且以冲击力破坏易碎结构。 压力管组件还包括凹陷在易碎结构中的不会从易碎结构的外表面突出的爆炸歧管。 爆炸歧管接收压力管的端部，并且包括用于引爆爆炸物爆炸组件/绳索的雷管。 爆炸歧管具有用于接受压力管的圆形端部的圆形横截面配件。 通过没有压力管组件的任何部分从易碎结构突出，可以实现改进的性能。 具有圆形配件还可改善压力管和爆炸歧管之间的密封。

公开(公告)号：US5810530A

公开(公告)日：1998-09-22

申请号：US947396

申请日：1997-10-08

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: F16B19/10 ,  F16B13/04 ,  F16B13/06

CPC classification number: F16B19/1054

Abstract: A blind fastener has an assembly including an inner sleeve, an outer sleeve and a pin member and is adapted to be located in workpiece openings with the pin member having an expansion portion adapted to be pulled through the inner sleeve radially expanding both the inner and outer sleeves to provide an interference fit with the workpiece openings.

Abstract translation: 盲紧固件具有包括内套筒，外套筒和销构件的组件，并且适于位于工件开口中，销构件具有膨胀部分，该膨胀部分适于被拉动穿过内套筒径向地扩展内和外 以提供与工件开口的过盈配合。

公开(公告)号：US09541235B2

公开(公告)日：2017-01-10

申请号：US13029769

申请日：2011-02-17

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: B65D88/04 ,  F17C1/00

CPC classification number: F17C1/00 ,  B65D88/04 ,  F02K9/605 ,  F02K9/88 ,  F05D2250/231 ,  F05D2250/25 ,  F05D2250/292 ,  F05D2250/75 ,  F17C2201/0133 ,  F17C2203/0619 ,  F17C2203/0639 ,  F17C2203/0643 ,  F17C2203/0648 ,  F17C2203/067 ,  F17C2209/21 ,  F17C2209/2109 ,  F17C2221/014 ,  F17C2223/0123 ,  F17C2223/036 ,  F17C2270/0197 ,  Y10T29/49346

Abstract: A toroid pressure vessel includes a toroid body having an inner shell and an outer shell. The toroid body includes a toroid outer perimeter. The outer shell extends along the toroid outer perimeter. A planar exterior face extends along at least a portion of the outer shell and the toroid outer perimeter. A support belt circumscribes the toroid outer perimeter and is coupled along the planar exterior face. The support belt braces and supports the pressure vessel along the toroid outer perimeter against bulging force (and hoop stress) generated by pressurized fluids within the vessel. The support belt facilitates the use of thinner pressure vessel shells and thereby decreases the weight of the pressure vessel while providing a support to the outer shell that substantially prevents deformation of the planar exterior face.

Abstract translation: 环形压力容器包括具有内壳和外壳的环形体。 环形体包括环形外周边。 外壳沿环形外周延伸。 平面外表面沿外壳和环形外周的至少一部分延伸。 支撑带围绕环形外周，并沿着平面外表面联接。 支撑带沿着环形外周边支撑和支撑压力容器，防止由容器内的加压流体产生的膨胀力（和环向应力）。 支撑带有利于使用更薄的压力容器壳，从而减小压力容器的重量，同时为外壳提供基本上防止平面外表面变形的支撑。

公开(公告)号：US20120145028A1

公开(公告)日：2012-06-14

申请号：US12967973

申请日：2010-12-14

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: F42B15/36 ,  F42B15/00

CPC classification number: F42B15/36 ,  F42B10/66

Abstract: Projectiles that include a propulsion system and a launch motor which are located on opposing sides of a payload and a method of directing a projectile toward a target are generally described herein. Placing the propulsion system and the launch motor on opposing sides of the payload may provide many potential advantages when designing the projectile. These design advantages may make it easier to create a projectile that includes more propellant and/or payload while still permitting the projectile to be stored within existing containers having a fixed size.

Abstract translation: 这里通常描述包括位于有效载荷的相对侧上的推进系统和发射马达的射弹以及将射弹引向目标的方法。 将推进系统和发射电机放置在有效载荷的相对侧可能在设计射弹时提供许多潜在的优点。 这些设计优点可以使得更容易地创建包括更多推进剂和/或有效载荷的弹丸，同时仍然允许将弹体存储在具有固定尺寸的现有容器中。

公开(公告)号：US20120085222A1

公开(公告)日：2012-04-12

申请号：US12542783

申请日：2009-08-18

Applicant: Robert D. Travis

Inventor： Robert D. Travis

IPC: F42D99/00 ,  C06B21/00

CPC classification number: F42B15/38 ,  F42B15/36

Abstract: A separation device for separating parts along a seam includes a frangible structure and a pressure tube assembly within the frangible structure. The pressure tube assembly includes a pressure tube which contains an explosive detonation assembly/cord that can be initiated to expand the pressure tube, and break the frangible structure with a shock force. The pressure tube assembly also includes a explosive manifold that is recessed in the frangible structure, not protruding from an outer surface of the frangible structure. The explosive manifold receives the ends of the pressure tube, and includes a detonator for detonating the explosive detonation assembly/cord. The explosive manifold has circular-cross-section fittings for accepting a circular ends of the pressure tube. By not having any part of the pressure tube assembly protrude from the frangible structure, improved performance may be achieved. Having circular fittings also improves the seal between the pressure tube and the explosive manifold.

Abstract translation: 用于沿着接缝分离部件的分离装置包括在易碎结构内的易碎结构和压力管组件。 压力管组件包括压力管，该压力管包含爆炸性爆炸组件/绳索，其可以被起动以膨胀压力管，并且以冲击力破坏易碎结构。 压力管组件还包括凹陷在易碎结构中的不会从易碎结构的外表面突出的爆炸歧管。 爆炸歧管接收压力管的端部，并且包括用于引爆爆炸物爆炸组件/绳索的雷管。 爆炸歧管具有用于接受压力管的圆形端部的圆形横截面配件。 通过没有压力管组件的任何部分从易碎结构突出，可以实现改进的性能。 具有圆形配件还可改善压力管和爆炸歧管之间的密封。