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1. 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。

2. 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。

3. 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。

4. 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。

5. 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。

6. 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。

7. 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.

8. 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。

9. 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。

10. 发明授权

US08146957B2 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：US08146957B2
公开(公告)日：2012-04-03
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 , B65B1/04
CPC分类号： F16L37/127 , B64F1/362
摘要： In certain embodiments, a PCA connector has a polyethylene body, wherein the polyethylene is durable, corrosion resistant, and exhibits excellent strength over a large range of temperature and moisture conditions. The polyethylene 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 polyethylene 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.
摘要翻译：在某些实施方案中，PCA连接器具有聚乙烯体，其中聚乙烯具有耐久性，耐腐蚀性，并且在大范围的温度和湿度条件下表现出优异的强度。聚乙烯体可以被描述为具有整体特征的单一结构，例如轴承部分，闩锁壳体部分，闩锁引导部分等。因此，通过身体的一体式设计，部件的数量显着减少。此外，PCA连接器可以包括被配置为将PCA连接器固定到飞行器的闭锁机构。例如，闩锁机构可以包括一对杠杆，其与聚乙烯主体的相对侧上的一对闩锁接合。在一些实施例中，杠杆可以相对于彼此沿相反方向旋转，以使得闩锁沿相同的方向（例如轴向）移动。而且，闩锁机构的一些实施例分别包括杠杆和闩锁之间的凸轮。

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