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1. 发明申请

US20100193629A1 LOCALIZED UTILITY POWER SYSTEM FOR AIRCRAFT 有权
标题翻译：用于飞机的本地化实用动力系统
公开(公告)号：US20100193629A1
公开(公告)日：2010-08-05
申请号：US12362832
申请日：2009-01-30
申请人： Joseph Sherman Breit , Michael Neil Witting , Trevor Laib , Richard L. Rankin , John Anthony Trela , Markland T. Gates , Ali Reza Mansouri
发明人： Joseph Sherman Breit , Michael Neil Witting , Trevor Laib , Richard L. Rankin , John Anthony Trela , Markland T. Gates , Ali Reza Mansouri
IPC分类号： B64D41/00 , B64D11/00 , H01M8/10 , H01M8/18 , H01M8/12
CPC分类号： B64D11/02 , B64D11/04 , B64D2041/005 , Y02T50/46 , Y02T90/36 , Y10T307/344
摘要： The disclosure provides for an aircraft galley and lavatory energy system capable of independent operation from a separate aircraft energy generating system. The galley and lavatory energy system comprises an energy source providing electrical energy, heat energy, and at least one by-product; a plurality of galley and lavatory devices for receiving the electrical energy, the heat energy, and the at least one by-product; and, a plurality of connectors for connecting the electrical energy, the heat energy, and the at least one by-product to the galley and lavatory devices. The energy source comprises a fuel cell, a fuel module, and optionally, a supplemental fuel source.
摘要翻译：本公开提供了能够从单独的飞机能量产生系统独立操作的飞机厨房和卫生间能量系统。厨房和卫生间能量系统包括提供电能，热能和至少一种副产物的能量源; 多个厨房和厕所装置，用于接收电能，热能和至少一个副产物; 以及用于将电能，热能和至少一个副产品连接到厨房和厕所装置的多个连接器。能量源包括燃料电池，燃料模块和任选的补充燃料源。

2. 发明授权

US08232670B2 Localized utility power system for aircraft 有权
标题翻译：飞机本地化电力系统
公开(公告)号：US08232670B2
公开(公告)日：2012-07-31
申请号：US12362832
申请日：2009-01-30
申请人： Joseph Sherman Breit , Michael Neil Witting , Trevor Laib , Richard L. Rankin , John Anthony Trela , Markland T. Gates , Ali Reza Mansouri
发明人： Joseph Sherman Breit , Michael Neil Witting , Trevor Laib , Richard L. Rankin , John Anthony Trela , Markland T. Gates , Ali Reza Mansouri
IPC分类号： B60L1/00
CPC分类号： B64D11/02 , B64D11/04 , B64D2041/005 , Y02T50/46 , Y02T90/36 , Y10T307/344
摘要： The disclosure provides for an aircraft galley and lavatory energy system capable of independent operation from a separate aircraft energy generating system. The galley and lavatory energy system comprises an energy source providing electrical energy, heat energy, and at least one by-product; a plurality of galley and lavatory devices for receiving the electrical energy, the heat energy, and the at least one by-product; and, a plurality of connectors for connecting the electrical energy, the heat energy, and the at least one by-product to the galley and lavatory devices. The energy source comprises a fuel cell, a fuel module, and optionally, a supplemental fuel source.
摘要翻译：本公开提供了能够从单独的飞机能量产生系统独立操作的飞机厨房和卫生间能量系统。厨房和卫生间能量系统包括提供电能，热能和至少一种副产物的能量源; 多个厨房和厕所装置，用于接收电能，热能和至少一个副产物; 以及用于将电能，热能和至少一个副产品连接到厨房和厕所装置的多个连接器。能量源包括燃料电池，燃料模块和任选的补充燃料源。

3. 发明申请

US20070068520A1 Self-donning supplemental oxygen 有权
标题翻译：自助补充氧气
公开(公告)号：US20070068520A1
公开(公告)日：2007-03-29
申请号：US11196604
申请日：2005-08-03
申请人： Trevor Laib , Bradley Mitchell
发明人： Trevor Laib , Bradley Mitchell
IPC分类号： A62B18/08
CPC分类号： A62B17/04 , A62B18/00 , A62B25/005
摘要： A supplemental oxygen system and method is set forth for providing oxygen to an occupant of a pressurized aircraft. A flexible hood may be adapted to be stowed in a small volume when the flexible hood is deflated and may be further adapted to cover at least a portion of the head of the occupant and to provide a flow of oxygen to the occupant when the flexible hood is inflated. A source of oxygen may be adapted to rapidly inflate and deploy the flexible hood.
摘要翻译：提出了补充氧气系统和方法，用于向加压飞行器的乘员提供氧气。柔性罩可以适于在柔性罩被放气时以小体积收纳，并且可以进一步适于覆盖乘员头部的至少一部分并且当柔性罩时向乘客提供氧气流充气氧气源可以适于快速膨胀和展开柔性罩。

4. 发明申请

US20070057121A1 Simplified power system for a cabin services system for an aircraft 有权
标题翻译：用于飞机的客舱服务系统的简化电力系统
公开(公告)号：US20070057121A1
公开(公告)日：2007-03-15
申请号：US11303498
申请日：2005-12-16
申请人： Kevin Callahan , Trevor Laib , Donald Lee , Bradley Mitchell , William Sanford
发明人： Kevin Callahan , Trevor Laib , Donald Lee , Bradley Mitchell , William Sanford
IPC分类号： B64D11/00
CPC分类号： H02G3/00 , B64D2221/00 , H02G3/32
摘要： A mounting rail system for a cabin services system of an aircraft is disclosed. The mounting rail system comprises a mounting rail for providing power, and at least one circuit coupled to the mounting rail for allowing for operation of functionalities of a passenger services unit.
摘要翻译：公开了一种用于飞机的客舱服务系统的安装轨道系统。安装轨道系统包括用于提供动力的安装轨道，以及耦合到安装轨道的至少一个电路，用于允许乘客服务单元的功能的操作。

5. 发明申请

US20060102784A1 Cut to fit powered seat track cover 有权
标题翻译：切割适合动力座椅履带盖
公开(公告)号：US20060102784A1
公开(公告)日：2006-05-18
申请号：US10943035
申请日：2004-09-16
申请人： Kevin Callahan , Bradley Mitchell , Trevor Laib
发明人： Kevin Callahan , Bradley Mitchell , Trevor Laib
IPC分类号： B64D11/06
CPC分类号： B60N2/0725 , B60N2002/0264 , B64C1/20 , B64D11/0624 , B64D11/0696 , H02G3/0418 , H02G3/383
摘要： A seat track cover for transferring at least one of electrical power and data between two seats. The cover has a housing and a cable. The housing is sized to extend between a first seat leg assembly of a first seat and a second seat leg assembly of a second seat. The housing comprises a channel forming a first aperture at one end and a second aperture at a second end opposite the first aperture. The cable is seated within the housing and has a length at least equal to the length of the housing. The cable comprises a first connector and a second connector. The cable is seated within the housing such that the first connector is at the first aperture of the housing and the second connector is at the second aperture of the housing. The first connector couples with the first seat leg assembly and the second connector couples with the second seat leg assembly when the housing is positioned between the first seat leg and the second seat leg. In this manner, the cover provides a simple and economical connection between two seats using a cable having a standard length.
摘要翻译：座椅轨道盖，用于在两个座位之间传送电力和数据中的至少一个。盖子有一个外壳和一根电缆。壳体的尺寸设置成在第一座椅的第一座椅支腿组件和第二座椅的第二座椅支腿组件之间延伸。壳体包括在一端形成第一孔的通道和在与第一孔相对的第二端处的第二孔。电缆位于外壳内，其长度至少等于外壳的长度。电缆包括第一连接器和第二连接器。电缆位于壳体内，使得第一连接器位于壳体的第一孔口处，并且第二连接器位于壳体的第二孔口处。当壳体位于第一座椅腿部和第二座椅腿部之间时，第一连接器与第一座椅腿部组件耦接，并且第二连接器与第二座椅腿部组件耦合。以这种方式，盖使用具有标准长度的电缆在两个座之间提供简单和经济的连接。

6. 发明申请

US20060097109A1 Telescoping powered seat track cover 有权
标题翻译：伸缩式动力座椅轨道盖
公开(公告)号：US20060097109A1
公开(公告)日：2006-05-11
申请号：US10983906
申请日：2004-11-08
申请人： Trevor Laib , Bradley Mitchell , Samuel Feist
发明人： Trevor Laib , Bradley Mitchell , Samuel Feist
IPC分类号： B64D11/06
CPC分类号： B64D11/0696
摘要： A seat track cover having telescopically engaged first and second portions that enables an overall length of the seat track cover to be adjusted as needed to cover a portion of a seat track that separates two adjacent seats mounted to the seat tracks. A cable can be routed within the first and second portions to enable electrical or optical signals to be conducted between data/power connection ports on the seats. One embodiment includes mating conductive elements formed along the lengths of each of the first and second portions.
摘要翻译：具有可伸缩接合的第一和第二部分的座椅轨道盖，其能够根据需要调整座椅轨道盖的整个长度，以覆盖安装到座椅轨道的两个相邻座椅分隔的座椅轨道的一部分。电缆可以在第一和第二部分内布线，以使电或光信号能够在座椅上的数据/电源连接端口之间传导。一个实施例包括沿着第一和第二部分中的每一个的长度形成的配合导电元件。

7. 发明申请

US20050230543A1 Power strip for seats 有权
标题翻译：座椅电源板
公开(公告)号：US20050230543A1
公开(公告)日：2005-10-20
申请号：US11090875
申请日：2005-03-25
申请人： Trevor Laib , Bradley Mitchell , Kevin Callahan
发明人： Trevor Laib , Bradley Mitchell , Kevin Callahan
IPC分类号： B64C1/18 , B64D11/06
CPC分类号： B64D11/0696 , B64C1/18 , B64D11/0624
摘要： A system for distributing signals between a first seat and a second seat of a platform. The system generally includes an elongated bus and a connector operable to provide a connection between the bus and the passenger seats. Signals can be transmitted between the bus and the passenger seats, via the connector, at any point along the power bus, thus eliminating the need to run separate connections between the signal source and each seat. The bus is connected to the connector by depressing the bus upon the connector. This system and method significantly reduces the amount of time, energy, and expense necessary to individually wire each passenger seat to receive signals, such as power and/or data.
摘要翻译：一种用于在平台的第一座椅和第二座椅之间分配信号的系统。该系统通常包括细长总线和可操作以提供总线和乘客座椅之间的连接的连接器。信号可以在总线和乘客座椅之间通过连接器沿着电源总线的任何点传输，因此不需要在信号源和每个座位之间运行单独的连接。总线通过按压连接器上的总线连接到连接器。该系统和方法显着地减少了将每个乘客座位单独接线以接收诸如电力和/或数据的信号所需的时间，能量和费用。

8. 发明申请

US20050211835A1 Continuous power bus for seat power 有权
标题翻译：连续电源总线用于座椅电源
公开(公告)号：US20050211835A1
公开(公告)日：2005-09-29
申请号：US10810324
申请日：2004-03-27
申请人： James Henley , Robert Johnson , Darrel Santala , Samuel Feist , Trevor Laib , Bradley Mitchell , Kevin Callahan
发明人： James Henley , Robert Johnson , Darrel Santala , Samuel Feist , Trevor Laib , Bradley Mitchell , Kevin Callahan
IPC分类号： B64D11/06 , H01R4/26 , H01R25/14 , H02G3/00
CPC分类号： B64D11/0624 , B64D11/06 , B64D2221/00 , H01R4/26 , H01R25/14 , H02G3/00
摘要： A power distribution system having a continuous power bus to supply power and/or data to aircraft passenger seats in a mobile platform. The power distribution system generally includes a bus strip that extends along a length of the passenger cabin and a connector operable to provide a connection between the bus strip and the passenger seats. Power and/or data can be transmitted between the bus strip and the passenger seats, via the connector, at any point along the bus strip, thus eliminating the need to run separate connections between the power and/or data source and each passenger seat.
摘要翻译：一种配电系统，具有连续的电力总线，用于向移动平台中的飞机乘客座椅供电和/或数据。配电系统通常包括沿乘客舱的长度延伸的总线带和可操作以提供总线带和乘客座椅之间的连接的连接器。电源和/或数据可以在总线条和乘客座位之间通过连接器沿着总线条的任何点传输，因此不需要在电源和/或数据源与每个乘客座位之间运行单独的连接。

9. 发明申请

US20070228215A1 APPARATUS AND METHODS FOR REMOVABLY SECURING PAYLOADS IN AN AIRCRAFT 有权
标题翻译：用于在飞机上卸载货物的装置和方法
公开(公告)号：US20070228215A1
公开(公告)日：2007-10-04
申请号：US11278298
申请日：2006-03-31
申请人： Timothy Hudson , Trevor Laib , Timothy Erhardt
发明人： Timothy Hudson , Trevor Laib , Timothy Erhardt
IPC分类号： B64C1/20
CPC分类号： B64D9/003 , B64D11/0696
摘要： Apparatus and methods for removably securing payloads are disclosed. In one embodiment, a method includes coupling the payload to a body of a locking assembly, engaging an insertion portion of the body into the channel, translating the insertion portion of the body along the track from a first position to a second position, the body being substantially constrained from movement away from the track in the second position, and actuating at least one engagement member from an unsecured position to a secured position, a portion of the track being clampably engaged by the at least one engagement member and the insertion portion of the body when the at least one engagement member is positioned in the secured position such that the body is substantially constrained from movement along the track by the at least one engagement member.
摘要翻译：公开了用于可拆卸地固定有效载荷的装置和方法。在一个实施例中，一种方法包括将有效载荷联接到锁定组件的主体，将主体的插入部分接合到通道中，使身体沿着轨迹的插入部分从第一位置平移到第二位置，身体在第二位置基本上限制离开轨道的移动，并且将至少一个接合构件从不受保护的位置致动到固定位置，轨道的一部分可被夹紧地接合在至少一个接合构件和插入部分当所述至少一个接合构件位于所述固定位置时，所述主体使得所述主体基本上被所述至少一个接合构件沿着所述轨道的运动限制。

10. 发明申请

US20070089746A1 Method and apparatus for extending flight crew's time of useful consciousness after decompression 有权
标题翻译：减压后飞行机组有用意识时间延长的方法和装置
公开(公告)号：US20070089746A1
公开(公告)日：2007-04-26
申请号：US11244535
申请日：2005-10-06
申请人： Bradley Mitchell , Trevor Laib
发明人： Bradley Mitchell , Trevor Laib
IPC分类号： A61M16/00
CPC分类号： B64D25/00 , A62B99/00 , B64C1/18 , B64C2001/009 , B64D10/00
摘要： Systems and methods are provided for regulating the pressure within an aircraft flight crew area during and/or after a decompression event. For example, an aircraft may include a flight crew area, at least one pressure sensor for detecting the pressure of the atmosphere within the flight crew area, and at least one regulated decompression panel that is operatively associated with the pressure sensor, for regulating the pressure within the flight crew area during and/or after a decompression event.
摘要翻译：提供了系统和方法，用于在减压事件期间和/或之后调节飞机机组人员区域内的压力。例如，飞行器可以包括飞行机组区域，用于检测飞行机组区域内的气氛的压力的至少一个压力传感器以及与压力传感器可操作地相关联的至少一个调节减压面板，用于调节压力在减压事件期间和/或之后的飞行机组人员区域内。

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