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1. 发明授权

US08113866B2 Aircraft electrical connector with differential engagement and operational retention forces 有权
标题翻译：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：US08113866B2
公开(公告)日：2012-02-14
申请号：US13185489
申请日：2011-07-18
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： H01R13/62
CPC分类号： H01R13/639 , H01R4/48 , H01R4/489 , H01R13/18 , H01R13/193 , H01R13/62933 , H01R2201/26
摘要： An aircraft powering system is provided which includes an aircraft electrical connector is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft powering 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.
摘要翻译：提供了一种飞机供电系统，其包括飞行器电连接器，其具有允许与飞机轻松接合并具有强保持力的特征。飞机供电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，其中偏置机构构造成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。

2. 发明申请

US20110269325A1 AIRCRAFT ELECTRICAL CONNECTOR WITH DIFFERENTIAL ENGAGEMENT AND OPERATIONAL RETENTION FORCES 有权
标题翻译：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：US20110269325A1
公开(公告)日：2011-11-03
申请号：US13185489
申请日：2011-07-18
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 powering system is provided which includes an aircraft electrical connector is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft powering 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.
摘要翻译：提供了一种飞机供电系统，其包括飞行器电连接器，其具有允许与飞机轻松接合并具有强保持力的特征。飞机供电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，其中偏置机构构造成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。

3. 发明授权

US07980875B2 Aircraft electrical connector with differential engagement and operational retention forces 有权
标题翻译：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。

4. 发明申请

US20100197159A1 AIRCRAFT ELECTRICAL CONNECTOR WITH DIFFERENTIAL ENGAGEMENT AND OPERATIONAL RETENTION FORCES 有权
标题翻译：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：US20100197159A1
公开(公告)日：2010-08-05
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： H01R13/62
CPC分类号： H01R13/639 , H01R4/48 , H01R4/489 , H01R13/18 , H01R13/193 , H01R13/62933 , H01R2201/26
摘要： An aircraft powering system is provided which includes an aircraft electrical connector is provided with features to allow facile engagement with an aircraft and strong retention forces. The aircraft powering 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.
摘要翻译：提供了一种飞机供电系统，其包括飞行器电连接器，其具有允许与飞机轻松接合并具有强保持力的特征。飞机供电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，其中偏置机构构造成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。

5. 发明申请

US20100029123A1 AIRCRAFT POWER CONNECTOR WITH DIFFERENTIAL ENGAGEMENT AND OPERATIONAL RETENTION FORCES 有权
标题翻译：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。

6. 发明授权

US07789109B2 Expansible and collapsible pre-conditioned air supply hose conduit 有权
标题翻译：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。

7. 发明申请

US20080054631A1 Self-Positioning Adapting System Between Aircraft and Preconditioned-Air Supply Hose 有权
标题翻译：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。

8. 发明申请

US20090032652A1 SYSTEM FOR MOVING AND STORING A CONDUIT FOR SUPPLYING AIR TO AN AIRCRAFT 审中-公开
标题翻译：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。

9. 发明授权

US08631830B2 Semi-disposable pre-conditioned air supply hose conduit and connectors for attaching end portions of the same 有权
标题翻译：半一次性预处理空气供应软管导管和连接器，用于连接其端部
公开(公告)号：US08631830B2
公开(公告)日：2014-01-21
申请号：US11681644
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： F16L9/00
CPC分类号： F16L25/14 , F16L47/265
摘要： A tubular fluid conduit which is especially adapted for use in supplying pre-conditioned air to an aircraft being serviced, wherein the tubular conduit may be fabricated as a thermoplastic extrusion having a constant diameter dimension, whereby a first end portion may be fluidically connected to a large diameter supply conduit while a second end portion may be fluidically connected to a small diameter use conduit as a result of spiral wrapping the second end portion around the use conduit. Alternatively, the tubular conduit may be fabricated as a thermoplastic extrusion having repetitive sections with each section comprising relatively large diameter and relatively small diameter portions.
摘要翻译：一种管状流体导管，其特别适于用于向被维修的飞行器供应预调节的空气，其中管状导管可以制造成具有恒定直径尺寸的热塑性挤压件，由此第一端部部分可以流体地连接到大直径供应管道，而第二端部部分可以通过将第二端部部分围绕使用管道螺旋缠绕而流体连接到小直径使用管道。或者，管状管道可以制造成具有重复部分的热塑性挤出物，每个部分包括相对大的直径和相对小的直径部分。

10. 发明授权

US08016325B2 Self-positioning adapting system between aircraft and preconditioned-air supply hose 有权
标题翻译：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。

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