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1. 发明授权

US6142404A Compliant tape guide with planar stiffness body for a data storage tape cartridge 失效
标题翻译：符合数据存储磁带盒的平面刚度体的磁带导轨
公开(公告)号：US6142404A
公开(公告)日：2000-11-07
申请号：US192828
申请日：1998-11-16
申请人： John D. Willems , Daniel C. Egan , Douglas W. Johnson , Leif O. Erickson
发明人： John D. Willems , Daniel C. Egan , Douglas W. Johnson , Leif O. Erickson
IPC分类号： G11B23/087 , G03B23/02
CPC分类号： G11B23/08757
摘要： A compliant tape guide having a compliant member with optimized planar stiffness. The compliant tape guide includes a top support plate, a bottom support plate, a bearing piece, the compliant member and a biasing member. The bearing piece extends between the top and bottom support plate in a generally perpendicular fashion. The compliant member is associated with an inner surface of the bottom support plate and includes a base, opposing legs, an edge receiving surface and a planar stiffness body. The opposing legs extend from the base. The edge receiving surface is attached to the opposing legs opposite the base to define an opening. The planar stiffness body is disposed within the opening and is configured to increase an in-plane stiffness of the compliant member in a plane substantially parallel to a plane of the base. Finally, the biasing member is associated with the compliant member to bias the edge receiving surface into engagement with a storage tape during use.
摘要翻译：具有柔性构件的柔性带引导件具有优化的平面刚度。柔性带引导件包括顶部支撑板，底部支撑板，支承件，柔性元件和偏置元件。轴承件以大致垂直的方式在顶部和底部支撑板之间延伸。柔性构件与底部支撑板的内表面相关联并且包括底座，相对的腿，边缘接收表面和平面刚度体。相对的腿从基部延伸。边缘接收表面附接到与基座相对的相对的腿以限定开口。平面刚度体设置在开口内，并且构造成在基本上平行于基部的平面的平面中增加柔顺构件的平面内刚度。最后，偏置构件与顺应构件相关联，以在使用期间将边缘接收表面偏置成与存储带接合。

2. 发明授权

US06257519B1 Three-piece tape reel assembly for a data storage tape cartridge 有权
标题翻译：用于数据存储带盒的三片磁带卷盘组件
公开(公告)号：US06257519B1
公开(公告)日：2001-07-10
申请号：US09408601
申请日：1999-09-30
申请人： John D. Willems , G. Phillip Rambosek , Peter A. Ridl
发明人： John D. Willems , G. Phillip Rambosek , Peter A. Ridl
IPC分类号： B65H7514
CPC分类号： G11B23/037
摘要： A tape reel assembly for maintaining a data storage tape. The tape reel assembly includes a first flange, a second flange and a hub ring. The first flange includes a first plate and at least one loop member extending in a generally axial fashion from an inner face of the top plate at a radius R1. The second flange includes a second plate and at least one leg extending in a generally axial fashion from an inner face of the bottom plate. The leg is positioned to selectively engage the loop member. Finally, the hub ring is provided separately and is free of material extending across an inner diameter thereof. The hub ring further defines an outer winding surface and inner surface having a minimum radius R2. The hub ring is assembled between the first plate and the second plate. In this regard, the radius R2 is greater than the radius R1 such that the loop member and the leg extend and interact within an area defined by the inner surface of the hub ring.
摘要翻译：一种用于维护数据存储带的磁带盘组件。磁带盘组件包括第一凸缘，第二凸缘和毂环。第一凸缘包括第一板和至少一个环形构件，其以大致轴向的方式从顶板的内表面以半径R1延伸。第二凸缘包括第二板和从底板的内表面以大致轴向方式延伸的至少一个支脚。腿被定位成选择性地接合环构件。最后，轮毂环分开设置，并且没有延伸穿过其内径的材料。轮毂环进一步限定外绕组表面和具有最小半径R2的内表面。轮毂环组装在第一板和第二板之间。在这方面，半径R2大于半径R1，使得环构件和腿在由毂环的内表面限定的区域内延伸和相互作用。

3. 发明授权

US07646562B2 Data storage tape cartridge and system including an intermediate portion having a servo pattern 有权
标题翻译：数据存储带盒和系统包括具有伺服图案的中间部分
公开(公告)号：US07646562B2
公开(公告)日：2010-01-12
申请号：US11618013
申请日：2006-12-29
申请人： William J. Vanderheyden , Robert O. Wyman , John D. Willems
发明人： William J. Vanderheyden , Robert O. Wyman , John D. Willems
IPC分类号： G11B5/584
CPC分类号： G11B23/107 , G11B5/584
摘要： A data storage tape cartridge is provided with a combination tape including a data storage tape, an intermediate portion and a leader. A servo track and media information region is provided on the intermediate portion of the tape. The servo track is read by a servo track reader of a data storage apparatus. The media information region is read by the read/write head of the data storage apparatus.
摘要翻译：数据存储带盒设置有包括数据存储带，中间部分和引导者的组合带。伺服轨道和媒体信息区域设置在磁带的中间部分。伺服磁道由数据存储装置的伺服磁道读取器读取。媒体信息区域由数据存储装置的读/写头读取。

4. 发明授权

US08686328B2 Resettable missile control fin lock assembly 有权
标题翻译：可复位导弹控制翅片锁组件
公开(公告)号：US08686328B2
公开(公告)日：2014-04-01
申请号：US13554032
申请日：2012-07-20
申请人： John F. Bugge , John D. Willems
发明人： John F. Bugge , John D. Willems
IPC分类号： F42B10/64 , F42B10/02 , F42B15/01
CPC分类号： F42B10/14 , F42B10/64
摘要： A fin lock assembly 12 for locking and unlocking missile fins 20 includes a piston 34 movable along a piston axis 44 between a locked position for preventing a fin from rotating and an unlocked position for allowing the fin to rotate. The fin lock assembly includes a camshaft 46 rotatable between a locked position and a relatively-rotated unlocked position about a cam axis 50 that is transverse the piston axis. The camshaft has an eccentric portion 66 connected to the piston such that rotation of the camshaft between the locked position and the unlocked position moves the piston between its corresponding locked and unlocked positions. The fin lock assembly includes a torsion spring 72 connected to the camshaft to bias the camshaft toward its unlocked position. A latch mechanism 100 holds a plurality of camshafts in their locked positions and simultaneously releases the camshafts to release their fins.
摘要翻译：用于锁定和解锁导弹翅片20的翼片锁组件12包括活塞34，活塞34可在锁止位置之间沿着活塞轴线44移动，以防止翅片旋转，以及用于允许翅片旋转的解锁位置。翅片锁组件包括凸轮轴46，凸轮轴46可在锁定位置和相对旋转的解锁位置之间旋转，围绕横向于活塞轴线的凸轮轴线50。凸轮轴具有连接到活塞的偏心部分66，使得凸轮轴在锁定位置和解锁位置之间的旋转使活塞在其相应的锁定位置和解锁位置之间移动。翅片锁定组件包括连接到凸轮轴的扭转弹簧72，以将凸轮轴偏压到其解锁位置。闩锁机构100将多个凸轮轴保持在其锁定位置，同时释放凸轮轴以释放它们的翅片。

5. 发明授权

US07733598B1 Tape cartridge and tape drive system with internal and external tape guides 有权
标题翻译：磁带盒和磁带驱动器系统，带有内部和外部磁带导轨
公开(公告)号：US07733598B1
公开(公告)日：2010-06-08
申请号：US11409862
申请日：2006-04-24
申请人： John D. Willems , Kathryn L. Baker
发明人： John D. Willems , Kathryn L. Baker
IPC分类号： G11B15/60
CPC分类号： G11B15/602 , G11B23/087
摘要： A data storage tape cartridge and tape drive is disclosed in which drive mounted guides are received in a cutout of a data storage cartridge. A read/write head is moved through an access opening into engagement with a data storage tape between the drive mounted guides. The drive mounted guides closely control lateral positioning of the tape as it passes across the read/write head. The read/write head and the drive mounted guides are moved relative to each other and into engagement with the tape.
摘要翻译：公开了一种数据存储带盒和磁带驱动器，其中驱动器安装的引导件被接收在数据存储盒的切口中。读/写头通过访问开口移动以与驱动器安装的引导件之间的数据存储带接合。驱动器安装的导轨在通过读/写头时密切控制磁带的横向定位。读/写头和驱动安装的引导件相对于彼此移动并与带接合。

6. 发明授权

US08975566B2 Fin buzz system and method for assisting in unlocking a missile fin lock mechanism 有权
标题翻译：鳍式蜂鸣器系统和辅助解锁导弹翅片锁定机构的方法
公开(公告)号：US08975566B2
公开(公告)日：2015-03-10
申请号：US13570280
申请日：2012-08-09
申请人： Thomas A. Black , David J. Reyes , Robert W. Von Mayr , Erik A. Fjerstad , John D. Willems
发明人： Thomas A. Black , David J. Reyes , Robert W. Von Mayr , Erik A. Fjerstad , John D. Willems
IPC分类号： F42B15/01 , F42B10/64
CPC分类号： F42B10/64
摘要： By removing the aerodynamic fin forces from the fin lock mechanism, achieved by actuating the fin control system to apply a controlled force that counters the aerodynamic forces acting on the control fins, the system can reduce the transmission of aerodynamic forces onto the fin lock mechanism, which makes the fin lock mechanism easier to unlock with less force. Accordingly, a method for unlocking a fin lock mechanism that releasably holds one or more missile control fins in a locked position, where the control fins are prevented from rotating, includes the steps of (i) applying an alternating positive and negative rotational force to a control fin; (ii) monitoring the position of the control fin during the applying step; and (iii) while the position of the control fin does not exceed a predetermined value, repeating the applying step for a predetermined number of times or for a predetermined period.
摘要翻译：通过从翅片锁定机构去除空气动力学翅片力，通过致动翅片控制系统来施加对受到作用在控制翼片上的空气动力的受控力的系统可以减小空气动力对翅片锁定机构的传递，这使得翅片锁定机构在较小的力下更容易解锁。因此，用于解锁锁定机构的方法，该锁定机构可释放地将一个或多个导弹控制翼片保持在控制翼片被防止转动的锁定位置，包括以下步骤：（i）将正交和负转动的交替正转向控制鳍（ii）在施加步骤期间监测控制翅片的位置; 和（iii）当控制翅片的位置不超过预定值时，重复施加步骤预定次数或预定时段。

7. 发明申请

US20140021289A1 RESETTABLE MISSILE CONTROL FIN LOCK ASSEMBLY 有权
标题翻译：可重置的MISSILE CONTROL FIN锁定组件
公开(公告)号：US20140021289A1
公开(公告)日：2014-01-23
申请号：US13554032
申请日：2012-07-20
申请人： John F. Bugge , John D. Willems
发明人： John F. Bugge , John D. Willems
IPC分类号： F42B10/00
CPC分类号： F42B10/14 , F42B10/64
摘要： A fin lock assembly 12 for locking and unlocking missile fins 20 includes a piston 34 movable along a piston axis 44 between a locked position for preventing a fin from rotating and an unlocked position for allowing the fin to rotate. The fin lock assembly includes a camshaft 46 rotatable between a locked position and a relatively-rotated unlocked position about a cam axis 50 that is transverse the piston axis. The camshaft has an eccentric portion 66 connected to the piston such that rotation of the camshaft between the locked position and the unlocked position moves the piston between its corresponding locked and unlocked positions. The fin lock assembly includes a torsion spring 72 connected to the camshaft to bias the camshaft toward its unlocked position. A latch mechanism 100 holds a plurality of camshafts in their locked positions and simultaneously releases the camshafts to release their fins.
摘要翻译：用于锁定和解锁导弹翅片20的翼片锁组件12包括活塞34，活塞34可在锁止位置之间沿着活塞轴线44移动，以防止翅片旋转，以及用于允许翅片旋转的解锁位置。翅片锁组件包括凸轮轴46，凸轮轴46可在锁定位置和相对旋转的解锁位置之间旋转，围绕横向于活塞轴线的凸轮轴线50。凸轮轴具有连接到活塞的偏心部分66，使得凸轮轴在锁定位置和解锁位置之间的旋转使活塞在其相应的锁定位置和解锁位置之间移动。翅片锁定组件包括连接到凸轮轴的扭转弹簧72，以将凸轮轴偏压到其解锁位置。闩锁机构100将多个凸轮轴保持在其锁定位置，同时释放凸轮轴以释放它们的翅片。

8. 发明申请

US20140042266A1 FIN BUZZ SYSTEM AND METHOD FOR ASSISTING IN UNLOCKING A MISSILE FIN LOCK MECHANISM 有权
标题翻译： FIN BUZZ系统和方法，用于辅助解锁困难的锁定机制
公开(公告)号：US20140042266A1
公开(公告)日：2014-02-13
申请号：US13570280
申请日：2012-08-09
申请人： Thomas A. Black , David J. Reyes , Robert W. Von Mayr , Erik A. Fjerstad , John D. Willems
发明人： Thomas A. Black , David J. Reyes , Robert W. Von Mayr , Erik A. Fjerstad , John D. Willems
IPC分类号： F42B10/64
CPC分类号： F42B10/64
摘要： By removing the aerodynamic fin forces from the fin lock mechanism, achieved by actuating the fin control system to apply a controlled force that counters the aerodynamic forces acting on the control fins, the system can reduce the transmission of aerodynamic forces onto the fin lock mechanism, which makes the fin lock mechanism easier to unlock with less force. Accordingly, a method for unlocking a fin lock mechanism that releasably holds one or more missile control fins in a locked position, where the control fins are prevented from rotating, includes the steps of (i) applying an alternating positive and negative rotational force to a control fin; (ii) monitoring the position of the control fin during the applying step; and (iii) while the position of the control fin does not exceed a predetermined value, repeating the applying step for a predetermined number of times or for a predetermined period.
摘要翻译：通过从翅片锁定机构去除空气动力学翅片力，通过致动翅片控制系统来施加对受到作用在控制翼片上的空气动力的受控力的系统可以减小空气动力对翅片锁定机构的传递，这使得翅片锁定机构在较小的力下更容易解锁。因此，用于解锁锁定机构的方法，该锁定机构可释放地将一个或多个导弹控制翼片保持在控制翼片被防止转动的锁定位置，包括以下步骤：（i）将正交和负转动的交替正转向控制鳍（ii）在施加步骤期间监测控制翅片的位置; 和（iii）当控制翅片的位置不超过预定值时，重复施加步骤预定次数或预定时段。

9. 发明申请

US20080156920A1 Data Storage Tape Cartridge and System Including an Intermediate Portion Having a Servo Pattern 有权
标题翻译：数据存储盒式磁带和包括具有伺服模式的中间部分的系统
公开(公告)号：US20080156920A1
公开(公告)日：2008-07-03
申请号：US11618013
申请日：2006-12-29
申请人： William J. Vanderheyden , Robert O. Wyman , John D. Willems
发明人： William J. Vanderheyden , Robert O. Wyman , John D. Willems
IPC分类号： G11B23/107
CPC分类号： G11B23/107 , G11B5/584
摘要： A data storage tape cartridge is provided with a combination tape including a data storage tape, an intermediate portion and a leader. A servo track and media information region is provided on the intermediate portion of the tape. The servo track is read by a servo track reader of a data storage apparatus. The media information region is read by the read/write head of the data storage apparatus.
摘要翻译：数据存储带盒设置有包括数据存储带，中间部分和引导者的组合带。伺服轨道和媒体信息区域设置在磁带的中间部分。伺服磁道由数据存储装置的伺服磁道读取器读取。媒体信息区域由数据存储装置的读/写头读取。

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