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    Self-Positioning Adapting System Between Aircraft and Preconditioned-Air Supply Hose
    2.
    发明申请
    Self-Positioning Adapting System Between Aircraft and Preconditioned-Air Supply Hose 有权
    飞机与预管供气软管之间的自定位适应系统

    公开(公告)号：US20080054631A1

    公开(公告)日：2008-03-06

    申请号：US11753382

    申请日：2007-05-24

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Brian Michael Piety ,  Mark David Resendes ,  Dale Arnold Miller

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Brian Michael Piety ,  Mark David Resendes ,  Dale Arnold Miller

    IPC分类号： F16L27/00

    CPC分类号： F16L27/026 ,  B64F1/362 ,  F16L27/125 ,  F24F13/0209 ,  F24F13/0218

    摘要： A system and method for connecting a traditional air chute to an air hose delivering preconditioned air to an aircraft includes an adapter system. The adapter system includes a flexible stage having an exterior surrounding a hollow interior configured to receive air from the air hose and deliver the air to the air chute. The adapter system also includes a rotational stage coupled to the flexible stage and having an exterior surrounding a hollow interior configured to receive air from the air hose and deliver the air to the air chute. The flexible stage is adjustable relative to the rotational stage to selectively move the hollow interior of the flexible stage between extending along a common axis through the air chute and the rotational stage and not extending along the common axis.

    摘要翻译： 用于将传统空气滑槽连接到向飞机提供预调节空气的空气软管的系统和方法包括适配器系统。 适配器系统包括柔性台，其具有围绕中空内部的外部，该中空内部构造成从空气软管接收空气并将空气输送到空气槽。 适配器系统还包括旋转台，其联接到柔性台，并且具有围绕中空内部的外部，该外部构造成从空气软管接收空气并将空气输送到空气槽。 柔性台架相对于旋转台可调，以选择性地移动柔性台的中空内部，其沿公共轴线延伸通过空气滑槽和旋转台，并且不沿公共轴线延伸。

    Self-positioning adapting system between aircraft and preconditioned-air supply hose
    3.
    发明授权
    Self-positioning adapting system between aircraft and preconditioned-air supply hose 有权
    飞机与预处理供气软管之间的自适应调整系统

    公开(公告)号：US08016325B2

    公开(公告)日：2011-09-13

    申请号：US11753382

    申请日：2007-05-24

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Brian Michael Piety ,  Mark David Resendes ,  Dale Arnold Miller

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Brian Michael Piety ,  Mark David Resendes ,  Dale Arnold Miller

    IPC分类号： F16L27/00

    CPC分类号： F16L27/026 ,  B64F1/362 ,  F16L27/125 ,  F24F13/0209 ,  F24F13/0218

    摘要： A system and method for connecting a traditional air chute to an air hose delivering preconditioned air to an aircraft includes an adapter system. The adapter system includes a flexible stage having an exterior surrounding a hollow interior configured to receive air from the air hose and deliver the air to the air chute. The adapter system also includes a rotational stage coupled to the flexible stage and having an exterior surrounding a hollow interior configured to receive air from the air hose and deliver the air to the air chute. The flexible stage is adjustable relative to the rotational stage to selectively move the hollow interior of the flexible stage between extending along a common axis through the air chute and the rotational stage and not extending along the common axis.

    摘要翻译： 用于将传统空气滑槽连接到向飞机提供预调节空气的空气软管的系统和方法包括适配器系统。 适配器系统包括柔性台，其具有围绕中空内部的外部，该中空内部构造成从空气软管接收空气并将空气输送到空气槽。 适配器系统还包括旋转台，其联接到柔性台，并且具有围绕中空内部的外部，该外部构造成从空气软管接收空气并将空气输送到空气槽。 柔性台架相对于旋转台可调，以选择性地移动柔性台的中空内部，其沿公共轴线延伸通过空气滑槽和旋转台，并且不沿公共轴线延伸。

    SYSTEM FOR MOVING AND STORING A CONDUIT FOR SUPPLYING AIR TO AN AIRCRAFT
    4.
    发明申请
    SYSTEM FOR MOVING AND STORING A CONDUIT FOR SUPPLYING AIR TO AN AIRCRAFT 审中-公开
    移动和存储用于向飞机提供空气的通道的系统

    公开(公告)号：US20090032652A1

    公开(公告)日：2009-02-05

    申请号：US12140788

    申请日：2008-06-17

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Brian Michael Piety ,  Dennis Bednarz

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Brian Michael Piety ,  Dennis Bednarz

    IPC分类号： B05B15/06

    CPC分类号： B64F1/362

    摘要： A system for supporting a hose configured to deliver preconditioned air from a source to an aircraft is disclosed. The system includes a base support and a stationary bearing assembly connected to the base support proximate a first end of the stationary bearing assembly. The stationary bearing assembly is configured to engage the hose to support the hose. The system also includes a frame assembly connected to the stationary bearing assembly proximate a second end of the stationary bearing assembly. The frame assembly has a support extending away from the frame assembly that is configured to engage the hose.

    摘要翻译： 公开了一种用于支撑被配置为将预处理的空气从源输送到飞行器的软管的系统。 该系统包括基座支撑件和固定轴承组件，该固定轴承组件在固定轴承组件的第一端附近连接到基座支撑件。 固定轴承组件构造成与软管接合以支撑软管。 该系统还包括在静止轴承组件的第二端附近连接到固定轴承组件的框架组件。 框架组件具有远离框架组件延伸的支撑件，其构造成与软管接合。

    Aircraft electrical connector with differential engagement and operational retention forces
    5.
    发明授权
    Aircraft electrical connector with differential engagement and operational retention forces 有权
    具有差异接合和操作保持力的飞机电气连接器

    公开(公告)号：US07980875B2

    公开(公告)日：2011-07-19

    申请号：US12645451

    申请日：2009-12-22

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Wolfgang Ott ,  Christopher A. Tacklind

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Wolfgang Ott ,  Christopher A. Tacklind

    IPC分类号： H01R13/15

    CPC分类号： H01R13/639 ,  H01R4/48 ,  H01R4/489 ,  H01R13/18 ,  H01R13/193 ,  H01R13/62933 ,  H01R2201/26

    摘要： An aircraft electrical connector is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft electrical system may include the aircraft electrical connector having a unique biasing mechanism and modular construction, wherein the biasing mechanism is configured to place differential forces onto mating electrical connectors from an aircraft. The biasing mechanism may be operatively coupled to a handle or trigger, which may be easily engageable by an operator. In one embodiment, an electrical connector may include a cam plate disposed between electrical connectors. The cam plate is configured to place differential forces on mating connectors inserted into the electrical connectors. In another embodiment, an electrical connector includes a moveable shaft that is disposed between electrical connectors. The shaft is configured to bias the position of the electrical connectors to place differential engagement and retention forces on mating connectors inserted into the electrical connectors.

    摘要翻译： 飞机电连接器具有允许与飞行器轻松接合和强大的保持力的特征。 飞行器电气系统可以包括具有独特的偏置机构和模块化结构的飞行器电连接器，其中偏置机构被配置为将差分力放置在与飞机相配的电连接器上。 偏置机构可以可操作地联接到手柄或触发器，其可以容易地由操作者接合。 在一个实施例中，电连接器可以包括设置在电连接器之间的凸轮板。 凸轮板被配置为将差分力放置在插入到电连接器中的配合连接器上。 在另一个实施例中，电连接器包括设置在电连接器之间的可移动轴。 轴构造成偏置电连接器的位置，以将差动接合和保持力插入插入到电连接器中的配合连接器上。

    AIRCRAFT POWER CONNECTOR WITH DIFFERENTIAL ENGAGEMENT AND OPERATIONAL RETENTION FORCES
    9.
    发明申请
    AIRCRAFT POWER CONNECTOR WITH DIFFERENTIAL ENGAGEMENT AND OPERATIONAL RETENTION FORCES 有权
    具有差异接合和操作保持力的飞机电源连接器

    公开(公告)号：US20100029123A1

    公开(公告)日：2010-02-04

    申请号：US11681674

    申请日：2007-03-02

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Frank Otte ,  Dennis Bednarz

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch ,  Frank Otte ,  Dennis Bednarz

    IPC分类号： H01R13/62

    CPC分类号： H01R13/193 ,  H01R13/639

    摘要： A new and improved aircraft power connector, for electrical connection to an aircraft electrical connector, has incorporated thereon a dual-position mechanism which can effectively alter the engagement force level defined between the electrical connector contact pins of the aircraft power connector and the aircraft electrical connector. When the mechanism is disposed at a first position, the force level is relatively low so as to easily permit connection and disconnection, whereas when the mechanism is disposed at a second position, the force level is relatively high so as to ensure the connection of the aircraft power connector to the aircraft electrical connector and thereby prevent the inadvertent disconnection of the aircraft power connector from the aircraft electrical connector.

    摘要翻译： 用于电气连接到飞机电连接器的新的和改进的飞行器电源连接器已经结合有双位置机构，其可以有效地改变在飞行器电源连接器的电连接器接触销和飞行器电连接器之间限定的接合力水平 。 当机构设置在第一位置时，力水平相对较低，以便容易地允许连接和断开，而当机构设置在第二位置时，力水平相对较高，以确保连接 飞机电源连接器连接到飞机电连接器，从而防止飞机电源连接器与飞机电连接器的意外断开。

    Expansible and collapsible pre-conditioned air supply hose conduit
    10.
    发明授权
    Expansible and collapsible pre-conditioned air supply hose conduit 有权
    可膨胀和可折叠的预调节空气供应软管导管

    公开(公告)号：US07789109B2

    公开(公告)日：2010-09-07

    申请号：US11681657

    申请日：2007-03-02

    申请人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch

    发明人： Anatoly Gosis ,  Scott Takayuki Koizumi ,  Folkert Fred Koch

    IPC分类号： F16L11/00

    CPC分类号： F16L11/15 ,  F16L11/18 ,  F24F13/0272

    摘要： An expansible and collapsible tubular conduit, which is especially adapted for use in supplying pre-conditioned air to an aircraft while the aircraft is located upon the ground and is being serviced, comprises a plurality of annular fabric membranes which are connected to the opposite sides of a plurality of annular structural dividers or frame members in a continuously repetitive alternating manner. The structural combination or assembly comprising the fabric membranes and the structural dividers or frame members renders the tubular conduit readily expansible and contractible in the form of a spring or accordion so as to be capable of being easily and rapidly deployed and stowed, as well as to be capable of being stored in a relatively compact state or mode.

    摘要翻译： 一种可膨胀和可折叠的管状导管，其特别适用于在飞机位于地面并被维修时向飞行器供应预调节的空气，其包括多个环形织物膜，其连接到 多个环形结构分隔件或框架构件，以连续重复的交替方式。 包括织物膜和结构分隔器或框架构件的结构组合或组件使得管状导管能够以弹簧或手风琴的形式容易地膨胀和收缩，以便能够容易且快速地展开和收起，以及 能够以相对紧凑的状态或模式存储。