公开(公告)号：US10799725B2

公开(公告)日：2020-10-13

申请号：US14214597

申请日：2014-03-14

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： B65D85/64 ,  B64D25/14 ,  A62B1/20

摘要： Containers and methods are disclosed for replacing expired or unserviceable aircraft emergency slides (“slides”) in an aircraft. The disclosed containers are configured to securely retain both unserviceable slides and serviceable slides. The containers can be placed on an aircraft through the main door of the aircraft, and are further configured to be easily transported within the aircraft from a staging area of the aircraft to a slide installation and removal point at either the main door or an emergency exit door of the aircraft. The containers can be aligned with the installation and removal point to facilitate replacing an unserviceable slide with a new, serviceable slide. The disclosed containers and methods improve personnel safety concerning lifting and handling of the slides, which are heavy. The containers and methods disclosed herein further facilitate positioning of the slides near installation and removal points and properly orienting the slides, while reducing awkward handling situations for personnel.

公开(公告)号：US20200047005A1

公开(公告)日：2020-02-13

申请号：US16422959

申请日：2019-05-24

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： A62B1/20

摘要： Methods are disclosed for replacing expired or unserviceable aircraft emergency slides (“slides”) in an aircraft. The disclosed methods utilize containers that are configured to securely retain both unserviceable slides and serviceable slides at different times in different configurations as installation tools. The container can be placed on an aircraft through the main door of the aircraft, and are further configured to be easily transported within the aircraft from a staging area of the aircraft to a slide installation and removal point at either the main door or an emergency exit door of the aircraft. The containers can be aligned with the installation and removal point to facilitate replacing an unserviceable slide with a new, serviceable slide. The disclosed methods and containers improve personnel safety concerning lifting and handling of the slides, which are heavy. The containers and methods disclosed herein further facilitate positioning of the slides near installation and removal points and properly orienting the slides, while reducing awkward handling situations for personnel.

公开(公告)号：US20140054188A1

公开(公告)日：2014-02-27

申请号：US13756534

申请日：2013-02-01

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： B64F5/00

CPC分类号： B64F5/40 ,  B23P6/00 ,  B64F5/50 ,  B65D85/68 ,  B65D2585/687 ,  F16D65/0043 ,  Y10T29/4973 ,  Y10T29/49826 ,  Y10T29/49998

摘要： An aircraft brake assembly container having a base or container portion with feet extending therefrom. A further base portion is provided and mounted atop the base portion. A spacing is provided between the base and further base portions and this spacing is filled by a spacing container portion or member. The spacing container portion allows for lower profile base and further base portions while accommodating larger diameter new and used brake assemblies. A method of using same is also provided.

摘要翻译： 一种具有从其延伸的脚部的基部或容器部分的飞机制动组件容器。 另外的基部设置并安装在基部的顶部。 在基部和另外的基部之间设置间隔，并且该间隔由间隔容器部分或部件填充。 间隔容器部分允许下部轮廓基部和另外的基部，同时容纳更大直径的新的和使用过的制动器组件。 还提供了使用其的方法。

公开(公告)号：USD669836S1

公开(公告)日：2012-10-30

申请号：US29388077

申请日：2011-03-23

申请人： Jose Ordonez ,  Neil Waldron

设计人： Jose Ordonez ,  Neil Waldron

公开(公告)号：US20070261979A1

公开(公告)日：2007-11-15

申请号：US11432539

申请日：2006-05-12

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： B65D85/00

CPC分类号： B65D85/68 ,  B64F5/50 ,  B65D2585/6882 ,  F16D65/0043 ,  Y10T29/49718 ,  Y10T29/4973

摘要： A cargo container, particularly a cargo container for transporting an aircraft brake assembly and a method for using an aircraft brake assembly in servicing an aircraft, with the container having at least two identical container portions, at least one of the at least two container portions having an at least one sliding channel therein, an at least one cradle member having an at least one sliding portion engaging with said at least one sliding channel holding the cargo in a horizontal orientation, and at least one seducement device securing the at least two identical container portions. The method having the method steps of transporting an aircraft brake assembly container to said aircraft undercarriage, the container comprising at least two container portions, with a first of the at least two container portions supporting a new brake assembly; opening the container, rotating a second of the at least two container portions; aligning the second of the at least two container portions with the aircraft undercarriage and a used aircraft brake assembly; releasing the used aircraft brake assembly into the second of the at least two container portions; removing the second of the at least two container portions along with the used aircraft brake assembly; aligning the first of the at least two container portions with the aircraft undercarriage; installing the new brake assembly; and replacing the first of the at least two container portions atop the second of the at least two container portions.

摘要翻译： 一种货物集装箱，特别是用于运输飞机制动组件的货物集装箱和使用飞机制动组件来维修飞行器的方法，该容器具有至少两个相同的容器部分，所述至少两个容器部分中的至少一个具有 至少一个滑动通道，至少一个支架构件，其具有至少一个滑动部分，所述至少一个滑动部分与所述至少一个滑动通道接合，所述至少一个滑动通道以水平方向保持货物;以及至少一个诱导装置，其固定所述至少两个相同的容器 部分。 该方法具有将飞行器制动组件容器运输到所述飞行器底盘的方法步骤，所述容器包括至少两个容器部分，所述至少两个容器部分中的第一个支撑新的制动组件; 打开所述容器，旋转所述至少两个容器部分中的第二个; 将所述至少两个容器部分中的第二个与飞机起落架对准，并且使用二手飞机制动组件; 将所述二手飞机制动器组件释放到所述至少两个容器部分中的第二个中; 沿着所用的飞行器制动组件移除所述至少两个容器部分中的第二个; 将至少两个容器部分中的第一个与飞机起落架对准; 安装新的制动总成; 并且在所述至少两个容器部分中的第二容器部分的顶部之上替换所述至少两个容器部分中的第一个。

公开(公告)号：US20230017984A1

公开(公告)日：2023-01-19

申请号：US17740298

申请日：2022-05-09

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： B60B7/04 ,  B60B7/06 ,  B60B7/01

摘要： An aircraft wheel hub protector is adapted to engage an aircraft wheel including an aircraft tire on a rim. The aircraft wheel hub protector having two or more cover sections with a protective protrusion and coupling mechanism guide extending from the a first cover section and passing through a bearing race and internal surface within a hub of the rim of the aircraft wheel in such a fashion so as to provide a void within the protective protrusion. The second cover section is engaged with an opposed side of the aircraft wheel from the first cover section. A coupling mechanism passes through the void in the protective protrusion without having contact with the bearing race and internal surfaces within the hub of the rim and coupling the first cover section and securing the aircraft wheel hub protector to the aircraft wheel.

公开(公告)号：US5516412A

公开(公告)日：1996-05-14

申请号：US441853

申请日：1995-05-16

申请人： Panayotis C. Andricacos ,  Kirk G. Berridge ,  John O. Dukovic ,  Matteo Flotta ,  Jose Ordonez ,  Helmut R. Poweleit ,  Jeffrey S. Richter ,  Lubomyr T. Romankiw ,  Otto P. Schick ,  Frank Spera ,  Kwong-Hon Wong

发明人： Panayotis C. Andricacos ,  Kirk G. Berridge ,  John O. Dukovic ,  Matteo Flotta ,  Jose Ordonez ,  Helmut R. Poweleit ,  Jeffrey S. Richter ,  Lubomyr T. Romankiw ,  Otto P. Schick ,  Frank Spera ,  Kwong-Hon Wong

IPC分类号： C25D17/00 ,  C25D21/10 ,  C25F7/00 ,  C25D17/06

CPC分类号： C25D17/001 ,  C25D17/00 ,  C25D17/007 ,  C25D17/02 ,  C25D17/08 ,  C25D21/10 ,  C25F7/00 ,  Y10S204/07

摘要： An electroplating cell includes a floor, ceiling, front wall, and back wall forming a box having first and second opposite open ends. A rack for supporting an article to be electroplated is removably positioned vertically to close the first open end and includes a thief laterally surrounding the article to define a cathode. An anode is positioned vertically to close the second open end, with the assembly defining a substantially closed, six-sided inner chamber for receiving an electrolyte therein for electroplating the article. The article and surrounding thief are coextensively aligned with the anode, with the floor, ceiling, front and back walls being effective for guiding electrical current flux between the cathode and the anode. In a preferred embodiment, the cell is disposed as an inner cell inside an outer cell substantially filled with the electrolyte, and a paddle is disposed inside the inner cell for agitating the electrolyte therein. The rack is removable and installable vertically upwardly which allows for automated handling thereof.

摘要翻译： 电镀电池包括形成具有第一和第二相对开口端的盒子的地板，天花板，前壁和后壁。 用于支撑待电镀的物品的支架可移除地垂直地定位以闭合第一开口端，并且包括围绕物品的小偷以限定阴极。 阳极被垂直定位以闭合第二开口端，其中组件限定了基本封闭的六面内腔，用于在其中容纳用于电镀物品的电解质。 物品和周围的小偷与阳极共同对准，地板，天花板，前壁和后壁对于引导阴极和阳极之间的电流通量是有效的。 在一个优选的实施方式中，将电池作为内部电池设置在基本上充满电解质的外部电池中，并且在内部电池内设置有用于搅拌电解质的电极。 机架是可拆卸的，可垂直向上安装，允许其自动处理。

公开(公告)号：US11697034B2

公开(公告)日：2023-07-11

申请号：US16422959

申请日：2019-05-24

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： B64D25/14 ,  A62B1/20 ,  B65D85/64

CPC分类号： A62B1/20 ,  B64D25/14 ,  B65D85/64 ,  Y10T29/4973

摘要： Methods are disclosed for replacing expired or unserviceable aircraft emergency slides (“slides”) in an aircraft. The disclosed methods utilize containers that are configured to securely retain both unserviceable slides and serviceable slides at different times in different configurations as installation tools. The container can be placed on an aircraft through the main door of the aircraft, and are further configured to be easily transported within the aircraft from a staging area of the aircraft to a slide installation and removal point at either the main door or an emergency exit door of the aircraft. The containers can be aligned with the installation and removal point to facilitate replacing an unserviceable slide with a new, serviceable slide. The disclosed methods and containers improve personnel safety concerning lifting and handling of the slides, which are heavy. The containers and methods disclosed herein further facilitate positioning of the slides near installation and removal points and properly orienting the slides, while reducing awkward handling situations for personnel.

公开(公告)号：US20190001746A1

公开(公告)日：2019-01-03

申请号：US15859566

申请日：2017-12-31

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： B60B7/02 ,  B60B7/06

摘要： An aircraft wheel hub protector is adapted to engage an aircraft wheel including an aircraft tire on a rim. The aircraft wheel hub protector having two or more cover sections with a protective protrusion and coupling mechanism guide extending from the a first cover section and passing through a bearing race and internal surface within a hub of the rim of the aircraft wheel in such a fashion so as to provide a void within the protective protrusion. The second cover section is engaged with an opposed side of the aircraft wheel from the first cover section. A coupling mechanism passes through the void in the protective protrusion without having contact with the bearing race and internal surfaces within the hub of the rim and coupling the first cover section and securing the aircraft wheel hub protector to the aircraft wheel.

公开(公告)号：US09278764B2

公开(公告)日：2016-03-08

申请号：US13756534

申请日：2013-02-01

申请人： Jose Ordonez ,  Neil Waldron

发明人： Jose Ordonez ,  Neil Waldron

IPC分类号： B65D85/68 ,  B64F5/00

CPC分类号： B64F5/40 ,  B23P6/00 ,  B64F5/50 ,  B65D85/68 ,  B65D2585/687 ,  F16D65/0043 ,  Y10T29/4973 ,  Y10T29/49826 ,  Y10T29/49998

摘要： An aircraft brake assembly container having a base or container portion with feet extending therefrom. A further base portion is provided and mounted atop the base portion. A spacing is provided between the base and further base portions and this spacing is filled by a spacing container portion or member. The spacing container portion allows for lower profile base and further base portions while accommodating larger diameter new and used brake assemblies. A method of using same is also provided.

摘要翻译： 一种具有从其延伸的脚部的基部或容器部分的飞机制动组件容器。 另外的基部设置并安装在基部的顶部。 在基部和另外的基部之间设置间隔，并且该间隔由间隔容器部分或部件填充。 间隔容器部分允许下部轮廓基部和另外的基部，同时容纳更大直径的新的和使用过的制动器组件。 还提供了使用其的方法。