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1. 发明申请

WO2012112208A1 BELTED TOROID PRESSURE VESSEL AND METHOD FOR MAKING THE SAME 审中-公开
标题翻译：相关的TOROID压力容器及其制造方法
公开(公告)号：WO2012112208A1
公开(公告)日：2012-08-23
申请号：PCT/US2011/064929
申请日：2011-12-14
申请人： RAYTHEON COMPANY , TRAVIS, Robert D.
发明人： TRAVIS, Robert D.
IPC分类号： B65D90/02
CPC分类号： 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
摘要： 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.
摘要翻译：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）。支撑带有助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的变形的支撑。

2. 发明申请

WO2012082222A1 PROJECTILE THAT INCLUDES PROPULSION SYSTEM AND LAUNCH MOTOR ON OPPOSING SIDES OF PAYLOAD AND METHOD 审中-公开
标题翻译：包括推进系统和启动电机在运行和方法对策方面的计划
公开(公告)号：WO2012082222A1
公开(公告)日：2012-06-21
申请号：PCT/US2011/056133
申请日：2011-10-13
申请人： RAYTHEON COMPANY , TRAVIS, Robert D.
发明人： TRAVIS, Robert D.
IPC分类号： F42B15/10
CPC分类号： F42B15/36 , F42B10/66
摘要： 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.
摘要翻译：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。

3. 发明申请

WO2012112207A1 GRIPPING WASHER HAVING ONE OR MORE DEFORMABLE GRIPPING TABS AND METHOD FOR REDUCING FOREIGN OBJECT DEBRIS 审中-公开
标题翻译：具有一个或多个可变轨迹的移动垫圈和减少外来物件的方法
公开(公告)号：WO2012112207A1
公开(公告)日：2012-08-23
申请号：PCT/US2011/064901
申请日：2011-12-14
申请人： RAYTHEON COMPANY , TRAVIS, Robert D.
发明人： TRAVIS, Robert D.
IPC分类号： F16B43/00
CPC分类号： F16B41/002 , F16B43/00
摘要： 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.
摘要翻译：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。

4. 发明申请

WO2020251649A1 SINGLE-ACTUATOR ROTATIONAL DEPLOYMENT MECHANISM FOR MULTIPLE OBJECTS 审中-公开
公开(公告)号：WO2020251649A1
公开(公告)日：2020-12-17
申请号：PCT/US2020/025259
申请日：2020-03-27
申请人： RAYTHEON COMPANY
发明人： TRAVIS, Robert D.
IPC分类号： B64C3/56 , F42B15/10
摘要： A deployment system, such as for deploying wings (14, 16), includes a pair of hub assemblies (34, 36) that transmit linear motion provided by an actuator (40) into a combination of rotational and axial motion. The actuator (40) works on both hub assemblies, rotating (for each wing) a slew ring (162, 164) that is coupled to a lift bar (121) that acts as a follower, following a pair of cam slots (90), to allow the wings to follow their desired course. In one embodiment the wings (14) move axially away from a fuselage (20) at the beginning of the deployment movement, followed by a primarily rotational movement, with the wings pulling in toward the fuselage at the end of the deployment process. The actuator includes a pair of threaded shafts (threaded in opposite directions) that rotate along with a pinion gear, driven by a motor (202), to translate a pair of retractor links (206, 208) that are coupled to the slew rings.

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