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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。

4. 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。

5. 发明授权

US07572981B2 Parked aircraft power cable protection system and method 有权
标题翻译：停放飞机电力电缆保护系统及方法
公开(公告)号：US07572981B2
公开(公告)日：2009-08-11
申请号：US11227330
申请日：2005-09-14
申请人： Scott Takayuki Koizumi , Brian Michael Piety , Folkert Fred Koch , Wolfgang Ott , Dale Arnold Miller , Denise Marie Frazier , Mark David Resendes
发明人： Scott Takayuki Koizumi , Brian Michael Piety , Folkert Fred Koch , Wolfgang Ott , Dale Arnold Miller , Denise Marie Frazier , Mark David Resendes
IPC分类号： H01B7/00
CPC分类号： B64F1/36
摘要： A power delivery system for parked aircraft includes protective rings on the power cords. These protective rings protect the power cord jackets from wear and facilitate movement of the power cords across the ground. The rings may be configured for securement to the cable so as to compress the insulative jacket of the cable somewhat, thereby firmly maintaining the rings in place on the cable. The rings may be formed of two identical elements that are joined to envelope the cable. The rings may accommodate both round insulated cable, as well as bundled cable.
摘要翻译：停放飞机的供电系统包括电源线上的保护环。这些保护环保护电源线外套不受磨损，并方便电源线穿过地面。环可以被配置为固定到电缆，以便稍微压缩电缆的绝缘护套，从而将环牢固地保持在电缆上的适当位置。环可以由两个相同的元件形成，这些元件被连接以包围电缆。环可以容纳圆形绝缘电缆以及捆扎电缆。

6. 发明申请

US20100207383A1 PRECONDITIONED AIR CONNECTOR ASSEMBLY FOR AIRCRAFT 有权
公开(公告)号：US20100207383A1
公开(公告)日：2010-08-19
申请号：US12770452
申请日：2010-04-29
申请人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
发明人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
IPC分类号： F16L37/20
CPC分类号： F16L37/127 , B64F1/362
摘要： In certain embodiments, a PCA connector has a nylon body, wherein the nylon is durable, corrosion resistant, and exhibits excellent strength over a large range of temperature and moisture conditions. The nylon body may be described as a single structure with integral features, such as a bearing portion, a latch housing portion, a latch guide portion, and so forth. Thus, the number of parts is significantly reduced by the one-piece design of the body. In addition, the PCA connector may include a latching mechanism configured to secure the PCA connector to an aircraft. For example, the latching mechanism may include a pair of levers, which engage a pair of latches on opposite sides of the nylon body. In some embodiments, the levers may be rotated in opposite directions relative to one another to impart movement of the latches in the same direction, e.g., an axial direction. Also, some embodiments of the latching mechanism include a cam between the levers and the latches, respectively.

7. 发明授权

US08857859B2 Preconditioned air connector assembly for aircraft 有权
标题翻译：飞机前置空气连接器总成
公开(公告)号：US08857859B2
公开(公告)日：2014-10-14
申请号：US13420512
申请日：2012-03-14
申请人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
发明人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
IPC分类号： F16L37/20 , F16L37/127 , B64F1/36
CPC分类号： F16L37/127 , B64F1/362
摘要： A preconditioned air connector (PCA) may be provided with a hollow body configured to pass a fluid flow, and a first mount assembly coupled to the hollow body. The first mount assembly may include a first cam joint with a first arcuate path of motion in a first plane generally tangential to the hollow body, a first mount coupled to the first cam joint, and a first lever coupled to the first cam joint. The first lever may be configured to actuate the first mount via a first transfer of motion through the first cam joint to draw the first mount inwardly toward the hollow body. In addition, the first mount may be configured to draw the hollow body and a mating component inwardly toward one another to pass the fluid flow between the hollow body and the mating component.
摘要翻译：预调节空气连接器（PCA）可以设置有被配置为使流体流动通过的中空主体，以及联接到中空本体的第一安装组件。第一安装组件可以包括第一凸轮接头，第一凸轮接头在与中空本体大致相切的第一平面中具有第一弧形运动路径，联接到第一凸轮接头的第一安装件和联接到第一凸轮接头的第一杆。第一杠杆可经配置以经由第一凸轮接头的第一运动传递来致动第一安装座，以将第一安装件向内朝向中空本体拉出。此外，第一安装件可以被配置为将中空体和配合部件朝向彼此向内拉动，以使中空体和配合部件之间的流体流动通过。

8. 发明授权

US07152886B2 Preconditioned air connector assembly for aircraft 有权
标题翻译：飞机前置空气连接器总成
公开(公告)号：US07152886B2
公开(公告)日：2006-12-26
申请号：US10602310
申请日：2003-06-24
申请人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
发明人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
IPC分类号： F16L37/20 , F16L39/00 , F16L17/00
CPC分类号： F16L37/127 , B64F1/362
摘要： A connector for coupling a preconditioned air source to an aircraft is provided. The connector comprises actuating members rotatably secured to a body. In one embodiment, the actuating members are supported, at least partially, by an integrated bearing assembly. The connector also comprises securing members that are positionably coupled to the actuating members. Accordingly, rotation of the actuating members displaces the securing members. Moreover, the actuating members comprise respective camming surfaces, wherein the camming surfaces define the axial position of the corresponding securing members.
摘要翻译：提供了用于将预调节空气源耦合到飞行器的连接器。连接器包括可旋转地固定到主体的致动构件。在一个实施例中，致动构件至少部分由一体的轴承组件支撑。连接器还包括可定位地联接到致动构件的固定构件。因此，致动构件的旋转使固定构件移位。此外，致动构件包括相应的凸轮表面，其中凸轮表面限定对应的固定构件的轴向位置。

9. 发明授权

US08146958B2 Preconditioned air connector assembly for aircraft 有权
标题翻译：飞机前置空气连接器总成
公开(公告)号：US08146958B2
公开(公告)日：2012-04-03
申请号：US12770456
申请日：2010-04-29
申请人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
发明人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
IPC分类号： F16L37/20 , B65B1/04
CPC分类号： F16L37/127 , B64F1/362
摘要： In certain embodiments, a preconditioned air connector has a hollow body configured to route a fluid therethrough and a hook member configured to mate with a cooperating element to draw the hollow body into fluid communication with a mating component. The preconditioned air connector also has a pivotable member actuatable along an arc tangential to the hollow body to direct axial translation of the hook member from a first position to a second position to draw the hollow body into fluid communication with the mating component. The pivotable member has an arcuate camming surface having a locking portion that secures the connector in a fully engaged position with respect to the mating component.
摘要翻译：在某些实施例中，预调节的空气连接器具有构造成使流体穿过其中的中空本体，以及构造成与配合元件配合以将中空本体与配合部件流体连通的钩构件。预调节的空气连接器还具有可沿着与中空本体相切的弧线致动的可枢转构件，以将钩构件的轴向平移从第一位置引导到第二位置，以将中空本体与配合部件流体连通。可枢转构件具有弓形凸轮表面，其具有锁定部分，该锁定部分将连接器相对于配合部件固定在完全接合位置。

10. 发明申请

US20120235402A1 PRECONDITIONED AIR CONNECTOR ASSEMBLY FOR AIRCRAFT 有权
标题翻译：用于飞机的预先配置的空气连接器总成
公开(公告)号：US20120235402A1
公开(公告)日：2012-09-20
申请号：US13420512
申请日：2012-03-14
申请人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
发明人： Alan J. Janis , Folkert Fred Koch , Wolfgang Ott , Christopher Robin Drake , Brian Michael Piety , Mark David Resendes
IPC分类号： F16L37/18
CPC分类号： F16L37/127 , B64F1/362
摘要： A preconditioned air connector (PCA) may be provided with a hollow body configured to pass a fluid flow, and a first mount assembly coupled to the hollow body. The first mount assembly may include a first cam joint with a first arcuate path of motion in a first plane generally tangential to the hollow body, a first mount coupled to the first cam joint, and a first lever coupled to the first cam joint. The first lever may be configured to actuate the first mount via a first transfer of motion through the first cam joint to draw the first mount inwardly toward the hollow body. In addition, the first mount may be configured to draw the hollow body and a mating component inwardly toward one another to pass the fluid flow between the hollow body and the mating component.
摘要翻译：预调节空气连接器（PCA）可以设置有被配置为使流体流动通过的中空主体，以及联接到中空本体的第一安装组件。第一安装组件可以包括第一凸轮接头，第一凸轮接头在与中空本体大致相切的第一平面中具有第一弧形运动路径，联接到第一凸轮接头的第一安装件和联接到第一凸轮接头的第一杆。第一杠杆可经配置以经由第一凸轮接头的第一运动传递来致动第一安装座，以将第一安装件向内朝向中空本体拉出。此外，第一安装件可以被配置为将中空体和配合部件朝向彼此向内拉动，以使中空体和配合部件之间的流体流动通过。

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