公开(公告)号：US20170334562A1

公开(公告)日：2017-11-23

申请号：US15674342

申请日：2017-08-10

Applicant: C&D ZODIAC, INC.

Inventor： Eric Long ,  Stephen Kearsey ,  Scott Savian

IPC: B64D11/00 ,  E05B5/00 ,  E05C19/00 ,  E05B41/00 ,  E05C3/24 ,  E05C1/12 ,  E05B65/00 ,  E05B53/00 ,  E05C9/00

CPC classification number: B64D11/003 ,  B64D11/0015 ,  B64D2011/0038 ,  E05B1/0038 ,  E05B5/00 ,  E05B7/00 ,  E05B41/00 ,  E05B53/00 ,  E05B53/003 ,  E05B53/005 ,  E05B65/006 ,  E05C1/12 ,  E05C3/24 ,  E05C9/00 ,  E05C9/002 ,  E05C9/046 ,  E05C19/00 ,  Y10S292/37

Abstract: A latch system that includes a paddle button assembly having a button that is movable between home and actuation positions, a latch assembly that includes a striker assembly with a striker and a hook assembly, and a cable that extends between the paddle button and latch assemblies. The hook assembly includes a hook, a pivotal trigger arm, and a manual override switch that is movable between first and second positions when the trigger arm is moved from an engaged position to a disengaged position. Movement of the button from the home position to the actuation position pushes or pulls the cable, thereby pivoting the trigger arm from the engaged to the disengaged position and disengaging the hook from the striker. Pivotal movement of the trigger arm from the engaged to the disengaged position results in linear movement of the manual override switch from the first to the second position.

公开(公告)号：US09731827B2

公开(公告)日：2017-08-15

申请号：US15356178

申请日：2016-11-18

Applicant: C&D ZODIAC, INC.

Inventor： Eric Long ,  Stephen Kearsey ,  Scott Savian

IPC: B64D11/00 ,  E05B53/00 ,  E05C9/00 ,  E05C3/24 ,  E05B41/00 ,  E05B5/00 ,  E05B65/00 ,  E05C1/12 ,  E05C19/00

CPC classification number: B64D11/003 ,  B64D11/0015 ,  B64D2011/0038 ,  E05B1/0038 ,  E05B5/00 ,  E05B7/00 ,  E05B41/00 ,  E05B53/00 ,  E05B53/003 ,  E05B53/005 ,  E05B65/006 ,  E05C1/12 ,  E05C3/24 ,  E05C9/00 ,  E05C9/002 ,  E05C9/046 ,  E05C19/00 ,  Y10S292/37

Abstract: A aircraft storage bin latch system that includes a paddle button assembly having a button that is movable between home and actuation positions, a latch assembly that includes a striker assembly with a striker and a hook assembly, and a cable that extends between the paddle button assembly and the latch assembly. The hook assembly includes a hook, a pivotal trigger arm, and an indicator that is movable between first and second positions when the trigger arm is moved from an engaged position to a disengaged position. Movement of the button from the home position to the actuation position pushes or pulls the cable, thereby pivoting the trigger arm from the engaged position to the disengaged position and disengaging the hook from the striker. Pivotal movement of the trigger arm from the engaged position to the disengaged position results in linear movement of the indicator from the first position to the second position.

公开(公告)号：US09499272B2

公开(公告)日：2016-11-22

申请号：US14923905

申请日：2015-10-27

Applicant: C&D ZODIAC, INC.

Inventor： Stephen Kearsey ,  Eric Long ,  Scott Savian

IPC: E05C9/10 ,  E05C9/00 ,  B64D11/00 ,  A47B46/00 ,  E05C19/00 ,  E05C1/12 ,  E05B53/00 ,  B60Q3/02

CPC classification number: B64D11/003 ,  A47B46/005 ,  B64D11/0015 ,  B64D2011/0038 ,  E05B41/00 ,  E05B53/00 ,  E05B53/003 ,  E05B53/005 ,  E05C1/12 ,  E05C3/24 ,  E05C9/00 ,  E05C19/00 ,  Y02T50/46 ,  Y10S292/37

Abstract: A latch system that includes a paddle button assembly having a button that is movable between a home position and an actuation position, a first latch assembly that includes a first striker assembly and a first hook assembly, and a first cable that extends between the paddle button assembly and the first latch assembly. Movement of the button from the home position to the actuation position moves the first cable, thereby disengaging the first hook assembly and the first striker assembly.

Abstract translation: 一种闩锁系统，其包括具有可在原始位置和致动位置之间移动的按钮的桨按钮组件，包括第一撞击器组件和第一钩组件的第一闩锁组件以及在所述桨按钮之间延伸的第一线缆 组件和第一闩锁组件。 按钮从原位移动到致动位置移动第一缆线，从而使第一钩组件和第一撞针组件脱离接合。

公开(公告)号：US08955805B2

公开(公告)日：2015-02-17

申请号：US14179494

申请日：2014-02-12

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian ,  Stephen Kearsey ,  Corey Williams

IPC: B64D11/00 ,  B60Q3/02 ,  B64D13/00

CPC classification number: B64D11/003 ,  B60Q3/43 ,  B64D11/0015 ,  B64D2011/0038 ,  Y02T50/46

Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

Abstract translation: 枢轴箱组件，其构造成接收行李并定位在飞行器的内部。 所述枢轴箱组件包括上壳体，所述上壳体包括强力和第一和第二侧板，与所述上壳体配合以限定箱体内部的铲斗，与所述第一侧板和所述铲斗可操作地相关联的第一枢转机构，以及 第二枢转机构可操作地与第二侧板和铲斗相关联。 第一和第二枢转机构沿着枢转轴线轴向对齐，使得该斗围绕上部壳体的枢转轴线在打开位置和关闭位置之间枢转。

公开(公告)号：US20140197721A1

公开(公告)日：2014-07-17

申请号：US14179494

申请日：2014-02-12

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian ,  Stephen Kearsey ,  Corey Williams

IPC: B64D11/00 ,  A47B46/00

CPC classification number: B64D11/003 ,  B60Q3/43 ,  B64D11/0015 ,  B64D2011/0038 ,  Y02T50/46

Abstract: A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.

Abstract translation: 枢轴箱组件，其构造成接收行李并定位在飞行器的内部。 所述枢轴箱组件包括上壳体，所述上壳体包括强背和第一和第二侧板，与所述上壳体协作以限定仓室内部的桶，与所述第一侧板和所述桶可操作地相关联的第一枢转机构，以及 第二枢转机构可操作地与第二侧板和铲斗相关联。 第一和第二枢转机构沿着枢转轴线轴向对齐，使得该斗围绕枢转轴线相对于上壳体在打开位置和关闭位置之间枢转。

公开(公告)号：US20130207529A1

公开(公告)日：2013-08-15

申请号：US13765358

申请日：2013-02-12

Applicant: C&D ZODIAC, INC.

Inventor： Stephen Kearsey ,  Richard McClure

IPC: F16F9/32 ,  A47B46/00

CPC classification number: F16F9/3207 ,  A47B46/00 ,  B64D11/003 ,  F16F9/145

Abstract: A damping mechanism that includes a housing with an inner circumferential surface defined by an assembly outer race, an axle shaft that is rotatable with respect to the housing, and a transmission assembly operatively associated with the axle shaft and disposed within the housing. The transmission assembly includes an assembly intermediate race. A fluid space that includes fluid therein is defined between the assembly intermediate race and the inner circumferential surface of the assembly outer race. A vane is disposed between the assembly intermediate race and the inner circumferential surface of the assembly outer race. The vane includes a restriction space defined therein. When the axle shaft rotates in the first direction, the transmission assembly transmits rotation from the axle shaft to the vane, and when the axle shaft rotates in the second direction, the transmission assembly transmits less rotation to the first vane than when the axle shaft rotates in the first direction.

Abstract translation: 一种阻尼机构，包括具有由组件外座圈限定的内圆周表面的壳体，可相对于所述壳体旋转的车轴;以及传动组件，其可操作地与所述车轴相关联并且设置在所述壳体内。 传动组件包括组合中间座圈。 在组件中间座圈和组件外圈的内圆周表面之间限定包括流体的流体空间。 叶片设置在组装中间座圈和组件外圈的内周面之间。 叶片包括其中限定的限制空间。 当车轴沿第一方向旋转时，传动组件将转轴从轴轴传递到叶片，并且当车轴沿第二方向旋转时，传动组件相对于第一叶片的旋转少于当车轴旋转时 在第一个方向。