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1. 发明授权

US07732741B1 Folding articulating wing mechanism 有权
标题翻译：折叠式铰接机构
公开(公告)号：US07732741B1
公开(公告)日：2010-06-08
申请号：US11518734
申请日：2006-08-31
申请人： Kent G. Whitham
发明人： Kent G. Whitham
IPC分类号： F42B13/32
CPC分类号： F42B10/14 , F42B10/64
摘要： A locking mechanism for securing an articulated folding wing assembly in a fully extended position by means of a tapered locking plunger urged by a coiled compression spring to contact a complementary mating surface formed on the wing assembly. The spring urged locking plunger is released from a retracted position by rotation of the wing assembly from the folded position to the extended position. A folding mechanism for rotating the wing assembly through a compound angle from the folded position to a rigid and positively locked fully extended position is provided wherein the extended wing may be rotated about its longitudinal axis to provide directional control to the vehicle.
摘要翻译：一种锁定机构，用于通过由螺旋压缩弹簧推动的锥形锁定柱塞将铰接的折叠翼组件固定在完全伸出的位置，以接触形成在翼组件上的互补配合表面。弹簧推动的锁定柱塞通过翼组件从折叠位置旋转到延伸位置而从缩回位置释放。提供了一种折叠机构，用于将翼组件从折叠位置旋转到刚性并且正向锁定的完全伸出位置的复合角度，其中延伸机翼可围绕其纵向轴线旋转以向车辆提供方向控制。

2. 发明授权

US4878695A Expanding ring joint 失效
标题翻译：膨胀环接头
公开(公告)号：US4878695A
公开(公告)日：1989-11-07
申请号：US280056
申请日：1988-12-05
申请人： Kent G. Whitham
发明人： Kent G. Whitham
IPC分类号： F16L37/252
CPC分类号： F16L37/252 , Y10T29/49963 , Y10T403/7005
摘要： A joint having no external protrusions consisting of the mating cylindricalnds of two tubular members joined by interlocking cogs on the male and female ends of the tubular members, and a pair of facing ramp surfaced rings disposed in the joint with one ring integral with or affixed immovably to the male end of one tubular member, the other ring rotatably disposed upon that same member within the joint so that when the movable ring is rotated by means of a spanner wrench or equivalent tool relative to the stationary ring, the juxtaposed ramp surfaces ride upon each other causing the movable ring to move axially relative to but in continuing contact with the stationary ring until contact with the female end of the other tubular member in the joint is established and the joint is thereby made rigid. The spaces thus created between the ramps of the rings are filled with material that becomes solid or set screws radially disposed in the movable ring to engage an annular slot about the male end of the one tubular member and underlying the movable ring can be used to thereafter immobilize that ring.
摘要翻译：没有外部突起的接头，其由两个管状构件的配合圆柱形端部组成，该两个管状构件通过在管状构件的阳和阴端上的互锁齿轮连接，以及一对面对的斜面表面环，设置在接头中，一个环与一个或多个不可移动地连接到一个管状构件的阳端，另一个环可旋转地设置在接头内的相同构件上，使得当可动环通过扳手扳手或等效工具相对于静止环旋转时，并置的斜面表面骑彼此相对地使可动环相对于静止环轴向移动，而与固定环持续接触，直到与接头中的另一个管状构件的阴端接触，从而使接头变得刚性。这样在环的斜面之间产生的空间被填充成为固体的材料或径向设置在可移动环中的固定螺钉以与环形槽相接合，该环形槽围绕一个管状构件的阳端并且可以用于其后固定那个戒指

3. 发明授权

US4568041A Fin attachment 失效
标题翻译：翅片附件
公开(公告)号：US4568041A
公开(公告)日：1986-02-04
申请号：US591159
申请日：1984-03-19
申请人： Kent G. Whitham
发明人： Kent G. Whitham
IPC分类号： F42B10/64 , F42B15/02 , F16B13/10 , B25G3/28
CPC分类号： F42B10/64 , Y10T403/4681 , Y10T403/7039
摘要： An improved fin attachment having a socket for reception of a tang mountedn a missile fin, an element for drawing the tang into the socket, and frusto-conical concentric rings which engage the tang and the socket to connect them rigidly in a predetermined angular relation. All elements of the attachment are retained so as not to be lost when the fin is detached, and the attachment provides effective connection without the use of complex shapes or precise manufacturing tolerances.
摘要翻译：改进的翅片附件具有用于接收安装在导弹翅片上的脚的插座，用于将脚部拉入插座的元件以及与脚部和插座接合的截头圆锥形同心环，以使它们以预定的角度关系刚性地连接。附件的所有元件被保持以便当散热片脱离时不会损失，并且附件提供有效的连接而不使用复杂的形状或精确的制造公差。

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